+++ DISCLAIMER +++

Nothing you see here is real, even though the model, the conversion or the presented background story might be based on historical facts. BEWARE!

  

Some background:

Operated by the Islamic Revolutionary Guards Corps, Iran's small Bell AH-1J fleet has seen a fair share of indigenous modernization in recent years. In 1971, Iran purchased 202 examples of an improved AH-1J, named "AH-1J International", from the United States. This improved Cobra featured an uprated P&WC T400-WV-402 engine and a stronger drivetrain, so that it would have a better performance under “hot & high” conditions. Recoil damping gear was fitted to the 20 mm M197 gun turret, and the gunner was given a stabilized sight and a stabilized seat, too. Of the AH-1Js delivered to the Shah's Imperial Iranian Army Aviation, 62 were TOW-capable.

Iranian AH-1Js participated in the Iran–Iraq War—which saw the most intensive use of helicopters in any conventional war. Iranian AH-1Js (particularly the TOW-capable ones) were "exceptionally effective" in anti-armor warfare, inflicting heavy losses on Iraqi armored and vehicle formations. In operations over the barren terrain in Khuzestan and later in southern Iraq, beside the standard tactics, Iranian pilots developed special, effective tactics, often in the same manner as the Soviets did with their Mi-24s. Due to the post-Revolution weapons sanctions, Iranians had to make do with what was at hand: lacking other guided ordnance they equipped the AH-1Js with AGM-65 Maverick missiles and used them with some success in several operations. About half of the AH-1Js were lost during the conflict to combat, accidents, and simple wear and tear –the rest of the fleet was kept operational and busy during the following years.

 

However, time and use took their toll on the Iranian Cobras, for which no replacement could be found. In 2001, Brigadier General Ahmad Kazemi, the then-commander in chief of the IRGC Air Force (from 2009, it became known as the IRGC Aerospace Force, or IRGCASF), requested Ali Khamenei, leader of the Islamic Republic, to permit the IRGC to procure two former army AH-1J Cobra helicopters that had been restored by the Iranian Helicopters Support and Renewal Company (IHSRC, called ‘Panha’ in Iran). They belonged to the Iranian Army Aviation Force (IRIAA, as it was then known), which lacked the funds to pay for the necessary restoration and renewal of parts and fuselage sections.

The first of these refurbished AH-1Js was a TOW Cobra capable of using the Iranian-made clone of the BGM-71A TOW anti-tank missile, the “Towfan”, while the second helicopter was a Non-TOW version capable of using only the 2¾-inch Hydra unguided rockets. They entered IRGCAF service at Fat'h helicopter base, Karaj, to the west of Tehran, in 2001. This marked the start of an ongoing but slow modernization program for the remaining Iranian Cobra fleet.

 

IHSRC also worked on the restoration of two more battle-damaged AH-1J TOW Cobras, in a project known as “Panha-2091”. The front sections of their fuselages had been destroyed by cannon rounds from Iraqi tanks during the Iran-Iraq war and the extensive restoration work required manufacture of new fuselage panels and structural parts. Panha engineers also co-operated with their colleagues from IAMI (Iranian Aircraft Manufacturing Industries, also known as HESA in Iran) and designed a new canopy for the helicopters equipped with a flat, bulletproof windshield instead of the former oval, non-bulletproof version. Under a project named HESA-2091, both helicopters were thoroughly modernized and equipped with multifunction displays and a new weapon control system with a head-up display for the pilot. Internal avionics were revamped with the addition of a GPS system in the nose, and a warning radar with four antennae providing 360 degrees coverage was integrated, too. Design and production of the new digital systems and their components was carried out by the Iranian Electronics Industries Company (IEI) with the assistance of Isfahan University of Technology and a Chinese-connected company, Safa Electronic Component Industries. Installation was performed by IAMI in Shahin-Shahr.

 

These two helicopters were ultimately named ‘Tiztak-2091’ and became prototypes for a larger modernization project for 102 remaining AH-1J Cobra attack helicopters for the Iranian Army Aviation Force. However, in total, the cost of this bold conversion projects exceeded the whole IRIAA budget for 2001, and this resulted in the cancellation of the wider modernization program just a year later. Step forward the IRGC which procured the two Tiztak-2091 prototypes alongside four more former IRIAA AH-1J Non-TOW Cobra helicopters from the Iranian Defence Ministry. These were revamped and delivered to frontline units between 2003 and 2005. However, further conversions have only be done sparingly since then, due to the lack of funds and material.

Despite these limitations, the IAAF immediately began working on upgrade projects to further increase combat capability of the small but busy fleet of Cobra helicopters. The Tiztak helicopters had been equipped with new targeting/surveillance turrets instead of their M-65 Telescopic Sight Units under a IAMI project named Towfan-2 back in 2012. The first helicopters were equipped with the Oqab EO/IR targeting turret produced by IOI (Iranian Optics Industries) in 2012, while others received an RU-290 thermal camera, a product of Rayan Roshd-Afzar.

 

After the formation of the Army Aviation Force of the Islamic Revolutionary Guard Corps (IRGCAA) on February 23, 2016, the IRGCASF helicopter base at Fat’h was transferred to the IRGCGF (IRGC Ground Force), of which the IRGCAA was now a part. IRGCAA today operates more than 80 helicopters including nine Bell AH-1J International Cobras, with three examples modernized by Iranian Aircraft Manufacturing Industries (IAMI). IRGCAA had also been trying to equip its small fleet of AH-1Js with a new air-to-surface missile and an anti-tank missile, the Qaem-114 (outwardly almost identical to the American AGM-119 Hellfire), but this did not proceed beyond prototype stage.

 

Despite the active Iranian AH-1J fleet’s relatively small size after 2001, the Cobras were extremely active during counter-terrorism and counter-insurgency operations in the southeast and northwest of Iran. Both the IAAF and now the IRGCAA had always had two fire support teams, each formed with two to three AH-1Js in Orumiyeh and Zahedan, to be used against the PKK/PJAK and Jaish ul-Adl terrorist groups. The fire-support team at the IRGCGF Hamzeh Garrison in the northwest of Iran had two Bell 214A utility helicopters for SAR operations to accompany the Cobras while the team in Zahedan International Airport had two to three Mi-171Sh helicopters; usually, one armed with B8M1 rocket pods as a heavy fire support gunship.

The most notable use of the AH-1Js in combat by the IRGC took place in spring and summer 2008 when two AH-1Js stationed in Zahedan were extensively used in close-air-support missions during a counter-terrorism operation by IRGC Ground Forces against the Jondollah group (later to be rebranded as Jaish ul-Adl after being listed as a terrorist organization by the US State Department). After the arrest and execution of its leader, Abdolmalek Reigi by Iran, the group stopped its activities in 2009. It resumed again a few years later resulting in the launch of new anti-terror operations involving the AH-1Js in 2013, which continued periodically until 2020.

  

General characteristics:

Crew: 2

Length: 53 ft 5 in (16.28 m) with both rotors turning

45 ft 9 in (14 m) for fuselage only

Width: 10 ft 9 in (3.28 m) for stub wings only

Height: 13 ft 5 in (4.09 m)

Main rotor diameter: 43 ft 11 in (13.39 m)

Main rotor area: 1,514.97 sq ft (140.745 m²)

Empty weight: 2,802 kg (6,177 lb)

Max takeoff weight: 4,530 kg (9,987 lb)

 

Powerplant:

2× P&W Canada T400-CP-400 (PT6T-3 Twin-Pac) turboshaft engines, coupled to produce 1,530 shp

(1,140 kW; de-rated from 1,800 shp (1,342 kW) for drivetrain limitations)

 

Performance:

Maximum speed: 236 km/h (147 mph, 127 kn)

Range: 600 km (370 mi, 320 nmi)

Service ceiling: 10,500 ft (3,200 m)

Rate of climb: 1,090 ft/min (5.5 m/s)

 

Armament:

1× 20 mm (0.787 in) M197 3-barreled Gatling cannon in M97 chin turret with 750 rounds

4× hardpoints under the sub wings for 2.75” (70 mm) Mk 40 or Hydra 70 rockets in 7 or 19 rounds

pods; up to 16 5” (127 mm) Zuni rockets in 4-round LAU-10D/A launchers, up to eight Toophan

ATGM in a dual or quad launcher on each wing, AIM-9 Sidewinder or Misagh-2 anti-aircraft

missiles (1 mounted on each hardpoint)

  

The kit and its assembly:

This is the counterpart to another modified Fujimi AH-1 model, actually a kit bashing of the AH-1S and the AH-1J model to produce something that comes close to the real IAMI HESA-2091 helicopter, an upgraded/re-built AH-1J International of the Iranian Army Air Force. The “leftover” parts were used to create an (Indonesian) AH-1G – even though the HESA-2091 was the “core project”.

 

To create this Iranian variant, the AH-1J was taken as the basis and the nose as well as the flat-window canopy from the AH-1S were transplanted. While the nose with the TOW sensor turret was just an optional part that fits naturally on the fuselage (even though not without some PSR), the clear parts was more challenging, because the flat canopy is shorter than the original. In this case I had to fill some triangular gaps between the hood and the engine section, and this was done with 1.5 mm styrene sheet wedges and some more PSR to blend the parts that were not meant to be combined into each other.

The cockpit was taken OOB, together with the pilot figures that come with the kit. I also retained the original all-metal main rotor because the Iranian Cobras AFAIK were never upgraded with composite material blades?

 

To set the HESA-2091 further apart from the original AH-1J I changed the sensor turret in the nose and scratched a ball-shaped fairing that resembles the indigenous RU-290 thermal camera – it’s actually the ball joint from a classic clear Matchbox kit display, with a base scratched from 0.5mm styrene sheet. The “ball” turned out to be a bit too large, but the overall look is O.K., since I wanted a non-TOW AH-1J. For a “different-than-a-stock-AH-1J” look A small radome for a missile guidance antenna was added to the nose above the sensor turret, too. Another personal addition are the small end plates on the stabilizers – inspired by similar installations on Bell’s early twin-engine AH-1s, even though these later disappeared and were technically replaced by a ventral fin extension and a longer fuselage; the Iranian AH-1Js retained the short, original fuselage of the single-engine Cobra variants, though. The end plates were cut from leftover rotor blades from the scrap box, IIRC they belong to a Matchbox Dauphin 2.

 

Being part of the historical Zahedan fire support team I gave the Cobra an armament consisting of a nineteen round 70mm Hydra unguided missile pods (OOB), a pair of AGM-65 Maverick missiles (an ordnance actually deployed by Iranian Cobras), together with their respective launch rails, and I added launch tubes for indigenous Misagh-2 anti-aircraft missiles (which are actually MANPADS) to the stub wings’ tips as a self-defense measure. These were scratched from 2mm styrene rods.

  

Painting and markings:

Finding a suitable paint scheme was not easy. A conservative choice would have been an early mid-stone/earth scheme or a tri-color scheme consisting of sand, earth and dark green. However, while doing WWW research I came across some more exotic and contemporary specimen, carrying a kind of leopard-esque mottle scheme or even a “high resolution” fractal/digital cammo consisting of three shades of beige/brown/grey – even though I am not certain if the latter was a “real” camouflage for operational helicopters or just a “show and shine” propaganda livery?

 

Re-creating the latter from scratch would have been prohibitively complex, because the pixelized mottles were really fine, maybe just 2” wide each in real life. But I used this scheme as an inspiration for a simplified variant, also kept in three shades of brown, even though the result was a kind of compromise due to the limited material options to create it.

The base became an overall coat with Tamiya XF-57 (Buff), plus very light grey (RAL 7035; Humbrol 196) undersides. A light black ink washing was applied, and panels were post-shaded to create a more vivid surface.

Then came the pixelized mottles in two contrast colors: first came a layer in RAL 1015 (Hellelfenbein/Light Ivory) and then a second in RAL 8011 (Nussbraun/Nut Brown) in a 1:1 ratio, slightly overlapping and letting the Buff base shine through. These mottles were not painted but rather created with square bits from generic decal stripe material in various widths from TL Modellbau. While not as sophisticated as the original camouflage, effect and look are quite similar, and add to the unique look of this HESA-2091(-ish) model. And even though I was sceptical, esp. because of the reddish Nussbraun, the blurring effect of the scheme is surprisingly good – esp. when you put the model in front of a dry mountain background! I’ll keep the concept in the back of my head for further what-if models. All those single pixels were a lot of work, but the result looks really good.

 

Another detail from many real late Iranian Cobras was taken over, too: a black tail rotor drive shaft cover that extends up onto the fin’s leading edge – probably a measure to hide exhaust soot stains on the tail boom? A black anti-glare panel was added in front of the windscreen, too, and the rotor blades became medium grey (Humbrol 165, Medium Sea Grey) except for the main rotor blades’ undersides, which became black. The cockpit interior was uniformly painted in a very dark grey (Revell 06, Anthracite) and the pilots received khaki jumpsuits and modern grey and olive drab “bone domes”.

 

The decals were puzzled together from various sources. The Iranian roundels came from a Begemot MiG-29 sheet, registration numbers and fin flashes from an Iranian F-5. The IAAF abbreviation was created with single black 4 mm letters.

Graphite was used to weather the model, esp. the area on top of the tail boom, and the model was finally sealed with matt acrylic varnish overall.

  

An exotic model – the Iranian home-brew HESA-2091 looks familiar, but it’s a unique combination of classic Cobra elements. More spectacular is the pixelated paint scheme, and the attempt to generate it with the help of square decal bits worked (and looks) better than expected! This might also work well in grey as a winter camouflage? Hmmm….

In space there is a need for a small vehicle capable of transporting loads of top-secret liquids and minerals at high speed. After loading the precious merchandise into its compartment, it sets off at great speed to deliver it to the Space Control Center.

The vehicle is based on the famous Italian "APE", transformed for the occasion into a very fast spedeer thanks to its powerful engines.

 

The nostalgia of the 80s and the love for Classic Space make me travel in the imagination and everything can be transformed into something spatial !!

 

This little MOC participates in the third contest for 90 years of LEGO on the LEGO Ideas platform at this link:

ideas.lego.com/challenges/8f551f3c-0554-4b9b-a1a6-8dc61e9...

My brother in law loves the donkeys that guard his herd of cattle and their calves on the Bruce Peninsula in Ontario . They are immensely strong and capable animals. Their huge ears and keen sense of smell are super detectors of intruders and they can make an incredible bawling noise, audible for miles. If that doesn't deter coyotes, the donkeys intercept them like jet fighters and dispatch the hapless predators with powerful and effective kicks and bites.

It was unnerving when one donkey butted me repeatedly while crossing a field after being spoilt by children hand feeding apples. My camera was knocked to the ground and broken and my arm bitten and bruised.

Already recognised as the most dynamically capable, performance-focused Jaguar, the F-TYPE sports car continues to evolve, with a fresh look, state-of-the-art infotainment system and world-first ReRun app that combines vehicle data with GoPro video to enhance the driving experience.

At the beginning of the Cold War, the Royal Canadian Air Force relied mostly on Canadair-built F-86 Sabres for defense of Canada. While the F-86 was a very capable aircraft, it was not suited to intercepting Soviet bombers in the extreme weather conditions of northern Canada, nor did it have the range to patrol the second-largest country in the world.

 

With this in mind, Avro Canada embarked on a crash program to design and build an interceptor with the necessary range, armament, and all-weather capability needed. The resulting CF-100 Canuck was a simple but effective design. While comparatively slow and unmanueverable compared to the Sabre—earning the CF-100 nicknames such as “Clunk,” “CF-Zero,” “Zilch,” and “Beast” for its lack of maneuverability—the Canuck was reliable and well-suited to poor weather. For awhile, the CF-100 was the only NATO fighter capable of operating in all weathers, and the USAF briefly considered adopting it for use over Korea; Belgium was to adopt the design in 1957.

 

The CF-100 was to go through several variants, though all kept the same basic straight-wing design. Initial versions of the Canuck, the Mk.3 and Mk. 4, entered service in 1953 and were armed with eight Browning M2 .50 caliber machine guns. As these were considered insufficient to bring down a heavy bomber, the Mk.4A added 58 Mighty Mouse rockets in wingtip pods; the Mk.5 deleted the machine guns entirely for rocket-only armament. The Canuck Mk.6 would have deleted the rocket pods in favor of AIM-7 Sparrow missiles, but this was cancelled as the CF-100 was scheduled to be replaced in the mid-1960s with the CF-105 Arrow. When the Arrow itself was cancelled, the Canuck was instead replaced by the CF-101 Voodoo, though a small number continued in service as trainers and electronic warfare aircraft until 1981, when it was finally withdrawn. 692 CF-100s were built, and today 26 remain in museums.

 

This CF-100, 100779, is a Mk.5, delivered in 1959 to 416 Squadron at CFB Cold Lake, Alberta. It served with 416 Squadron and 425 Squadron at CFB Bagotville, Quebec until 1970, when it was converted to an ECM training aircraft. When it was retired in 1976, it was donated to the Peterson AFB airpark (today the Peterson Air and Space Museum), which honors NORAD interceptors. It retains the knight's-helmet emblem of 414 Squadron, its last squadron assignment, based at North Bay, Ontario, and carries the earlier bilingual "Canadian Armed Forces/Forces Armees Canadiennes" used by the CAF in the late 1960s. The overall ADC gray was not used by CF-100s, but in this case is there to preserve the airframe.

 

This is the second picture I've taken of 100779; the first was taken in 1983 from the opposite angle. 40 years separate the two pictures. Here's the 1983 version: www.flickr.com/photos/31469080@N07/34567603212/in/photoli...

   

During World War II, both Great Britain and Germany had experimented with very large glider designs (the Hamlicar and Gigant, respectively) capable of carrying tanks. Though glider assaults had varied results during the war, the US Air Force briefly considered resurrecting the idea in 1948, and commissioned Chase Aircraft to build a large glider, the XCG-20 Avitruc. The XCG-20 was of all-metal construction, with a fully-equipped flight deck and a rear-mounted loading ramp for vehicles to be driven directly into the fuselage. The USAF abandoned the idea of glider assaults soon after the first XCG-20 was completed, but Chase had anticipated this: through the simple installation of two propeller-driven engines, the XCG-20 became the XC-123. This itself was considered only an interim design, as the XC-123A had four turbojet engines, becoming the first all-jet transport aircraft.

 

The USAF rejected the XC-123A, as it was found to have poor performance and short range, owing to the thirsty jets of the early 1950s. However, the piston-engined XC-123 showed promise, and the USAF ordered it into production in 1953. Production was delayed due to Chase Aircraft being acquired by Kaiser, who in turn sold the design to Fairchild Aircraft, who would produce it as the C-123B Provider.

 

The C-123 was considered a supplemental aircraft to the C-119 Flying Boxcar already in service and the soon-to-be-deployed C-130 Hercules. It had better single-engine performance than the C-119, and acquired a reputation for reliability, rugged design, simple maintenance, and the ability to land almost anywhere. A small number were converted to C-123J standard, with ski landing gear for operations in Antarctica and Greenland, and experiments were even made to convert it to an amphibian. Nevertheless, the number of C-123s in service were small compared to other types, and the C-130 began replacing it beginning in 1958.

 

As the United States involved itself more in the Vietnam War, one major advantage of its Viet Cong and North Vietnamese Army adversaries was the very jungle of Vietnam itself, which provided ready-made cover and camouflage from American air units. In an attempt to deprive the VC/NVA of jungle cover in known concentration areas, the USAF converted a number of C-123s to UC-123 standard, with spraying equipment for the pesticide Agent Orange. Under Operation Ranch Hand, UC-123s were among the first USAF aircraft deployed to Vietnam, and the first USAF aircraft lost in combat was a UC-123B. Spraying Agent Orange was very dangerous work, as it involved flying low and slow over hostile territory; it would not be until after the Vietnam War was over that it was learned that Agent Orange, used in the concentrated quantity employed in Vietnam, was also a deadly carcinogenic.

 

Besides their controversial employment as defoilant sprayers, standard C-123s were used as transports and Candlestick flareships, as the C-130 demand was exceeding supply, and the US Army’s CV-2 (later C-8) Caribous were proving the worth of a short-takeoff and landing transport. To improve the Provider’s performance in the “hot and high” conditions of Vietnam, two J85 turbojets were added beneath the wings of the C-123K variant, which became the final Provider variant and the main type used in Vietnam. CIA-flown Providers were used by Air America to clandestinely supply friendly Hmong tribes in Laos and in Cambodia. 54 C-123s were lost in Vietnam, second only to the C-130.

 

Following the end of American involvement in Vietnam, the C-123Ks were either handed over to South Vietnam or relegated to USAF Reserve and Air National Guard units, from which they were finally withdrawn around 1980. A few UC-123Ks were used to spray insecticides in Alaska and Guam as late as 1982. 11 other air forces used Providers, and the last C-123s were retired from the South Korean Air Force in 2001. 27 are preserved as museum pieces and a few remain in revenue service as “bush” aircraft in Alaska and elsewhere; remaining aircraft in storage were scrapped due to Agent Orange contamination.

 

55-4533 was delivered to the USAF's 513th Troop Carrier Group at Sewart AFB, Tennessee in 1957; after Sewart closed, the 513th moved to Pope AFB, North Carolina. In 1964, it was transferred to the 1st Air Commando Wing at Eglin AFB, Florida in anticipation of deployment to Southeast Asia--which happened in 1966, when 55-4533 was sent to the 375th Combat Support Group at Tan Son Nhut, South Vietnam. The aircraft would remain in Vietnam until 1971, serving in the transport and flareship role with the 375th and the 315th Special Operations Wing at Phan Rang. As American involvement wound down, 55-4533 returned to the United States, assigned to the 906th Tactical Airlift Group (Reserve) at Lockbourne AFB, Ohio. It was retired in 1981 and donated to the Castle Air Museum.

 

55-4533 was restored to its Vietnam appearance, with the name and nose art of "Hog Hauler"--either a commentary on the C-123's handling, or the cargo the Providers sometimes carried on Operation Mule Train missions over South Vietnam. Though its SEA camouflage has faded considerably, at least this is one Vietnam veteran C-123 that has found a honorable retirement in a museum.

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based historical facts. BEWARE!

 

Some background:

The Mikoyan-Gurevich MiG-19 (NATO reporting name: "Farmer") was a Soviet second-generation, single-seat, twin jet-engine fighter aircraft. It was the first Soviet production aircraft capable of supersonic speeds in level flight. A comparable U.S. "Century Series" fighter was the North American F-100 Super Sabre, although the MiG-19 would primarily oppose the more modern McDonnell Douglas F-4 Phantom II and Republic F-105 Thunderchief over North Vietnam. Furthermore, the North American YF-100 Super Sabre prototype appeared approximately one year after the MiG-19, making the MiG-19 the first operational supersonic jet in the world.

 

On 20 April 1951, OKB-155 was given the order to develop the MiG-17 into a new fighter called "I-340", also known as "SM-1". It was to be powered by two Mikulin AM-5 non-afterburning jet engines, a scaled-down version of the Mikulin AM-3, with 19.6 kN (4,410 lbf) of thrust. The I-340 was supposed to attain 1,160 km/h (725 mph, Mach 0.97) at 2,000 m (6,562 ft), 1,080 km/h (675 mph, Mach 1.0) at 10,000 m (32,808 ft), climb to 10,000 m (32,808 ft) in 2.9 minutes, and have a service ceiling of no less than 17,500 m (57,415 ft).

After several prototypes with many detail improvements, the ministers of the Soviet Union issued the order #286-133 to start serial production on February 17, 1954, at the factories in Gorkiy and Novosibirsk. Factory trials were completed on September 12 the same year, and government trials started on September 30.

 

Initial enthusiasm for the aircraft was dampened by several problems. The most alarming of these was the danger of a midair explosion due to overheating of the fuselage fuel tanks located between the engines. Deployment of airbrakes at high speeds caused a high-g pitch-up. Elevators lacked authority at supersonic speeds. The high landing speed of 230 km/h (145 mph), compared to 160 km/h (100 mph) for the MiG-15, combined with the lack of a two-seat trainer version, slowed pilot transition to the type. Handling problems were addressed with the second prototype, "SM-9/2", which added a third ventral airbrake and introduced all-moving tailplanes with a damper to prevent pilot-induced oscillations at subsonic speeds. It flew on 16 September 1954, and entered production as the MiG-19S.

 

Approximately 5,500 MiG-19's were produced, first in the USSR and in Czechoslovakia as the Avia S-105, but mainly in the People's Republic of China as the Shenyang J-6. The aircraft saw service with a number of other national air forces, including those of Cuba, North Vietnam, Egypt, Pakistan, and North Korea. The aircraft saw combat during the Vietnam War, the 1967 Six Day War, and the 1971 Bangladesh War.

 

However, jet fighter development made huge leaps in the 1960s, and OKB MiG was constantly trying to improve the MiG-19's performance, esp. against fast and high-flying enemies, primarily bombers but also spy planes like the U-2.

 

As the MiG-19S was brought into service with the Soviet air forces in mid-1956, the OKB MiG was continuing the refinement of the SM-1/I-340 fighter. One of these evolutionary paths was the SM-12 (literally, “SM-1, second generation”) family of prototypes, the ultimate extrapolation of the basic MiG-19 design, which eventually led to the MiG-19bis interceptor that filled the gap between the MiG-19S and the following, highly successful MiG-21.

 

The SM-12 first saw life as an exercise in drag reduction by means of new air intake configurations, since the MiG-19’s original intake with rounded lips became inefficient at supersonic speed (its Western rival, the North American F-100, featured a sharp-lipped nose air intake from the start). The first of three prototypes, the SM-12/1, was essentially a MiG-19S with an extended and straight-tapered nose with sharp-lipped orifice and a pointed, two-position shock cone on the intake splitter. The simple arrangement proved to be successful and was further refined.

 

The next evolutionary step, the SM-12/3, differed from its predecessors primarily in two new R3-26 turbojets developed from the earlier power plant by V. N. Sorokin. These each offered an afterburning thrust of 3,600kg, enabling the SM-12/3 to attain speeds ranging between 1,430km/h at sea level, or Mach=1.16, and 1,930km/h at 12,000m, or Mach=1.8, and an altitude of between 17,500 and 18,000m during its test program. This outstanding performance prompted further development with a view to production as a point defense interceptor.

 

Similarly powered by R3-26 engines, and embodying major nose redesign with a larger orifice permitting introduction of a substantial two-position conical centerbody for a TsD-30 radar, a further prototype was completed as the SM-12PM. Discarding the wing root NR-30 cannon of preceding prototypes, the SM-12PM was armed with only two K-5M (RS-2U) beam-riding missiles and entered flight test in 1957. This configuration would become the basis for the MiG-19bis interceptor that eventually was ordered into limited production (see below).

 

However, the SM-12 development line did not stop at this point. At the end of 1958, yet another prototype, the SM-12PMU, joined the experimental fighter family. This had R3M-26 turbojets uprated to 3.800kg with afterburning, but these were further augmented by a U-19D accelerator, which took the form of a permanent ventral pack containing an RU-013 rocket motor and its propellant tanks. Developed by D. D. Sevruk, the RU-013 delivered 3,000kg of additional thrust, and with the aid of this rocket motor, the SM-12PMU attained an altitude of 24,000m and a speed of Mach=1.69. But this effort was to no avail: the decision had been taken meanwhile to manufacture the Ye-7 in series as the MiG-21, and further development of the SM-12 series was therefore discontinued.

 

Nevertheless, since full operational status of the new MiG-21 was expected to remain pending for some time, production of a modified SM-12PM was ordered as a gap filler. Not only would this fighter bridge the performance gap to the Mach 2-capable MiG-21, it also had the benefit of being based on proven technologies and would not require a new basic pilot training.

 

The new aircraft received the official designation MiG-19bis. Compared with the SM-12PM prototype, the MiG-19bis differed in some details and improvements. The SM-12PM’s most significant shortfall was its short range – at full power, it had only a range of 750 km! This could be mended through an additional fuel tank in an enlarged dorsal fairing behind the cockpit. With this internal extra fuel, range could be extended by a further 200 - 250km range, but drop tanks had typically to be carried, too, in order to extend the fighter’ combat radius with two AAMs to 500 km. Specifically for the MiG-19bis, new, supersonic drop tanks (PTB-490) were designed, and these were later adapted for the MiG-21, too.

 

The air intake shock cone was re-contoured and the shifting mechanism improved: Instead of a simple, conical shape, the shock cone now had a more complex curvature with two steps and the intake orifice area was widened to allow a higher airflow rate. The air intake’s efficiency was further optimized through gradual positions of the shock cone.

As a positive side effect, the revised shock cone offered space for an enlarged radar dish, what improved detection range and resolution. The TsD-30 radar for the fighter’s missile-only armament was retained, even though the K-5’s effective range of only 2–6 km (1¼ – 3¾ mi) made it only suitable against slow and large targets like bombers. All guns were deleted in order to save weight or make room for the electronic equipment. The tail section was also changed because the R3M-26 engines and their afterburners were considerably longer than the MiG-19's original RM-5 engines. The exhausts now markedly protruded from the tail section, and the original, characteristic pen nib fairing between the two engines had been modified accordingly.

 

Production started in 1960, but only a total of roundabout 180 MiG-19bis, which received the NATO code "Farmer F", were built and the Soviet Union remained the only operator of the type. The first aircraft entered Soviet Anti-Air Defense in early 1961, and the machines were concentrated in PVO interceptor units around major sites like Moscow, Sewastopol at the Black Sea and Vladivostok in the Far East.

 

With the advent of the MiG-21, though, their career did not last long. Even though many machines were updated to carry the K-13 (the IR-guided AA-2 "Atoll") as well as the improved K-55 AAMs, with no change of the type’s designation, most MiG-19bis were already phased out towards the late 1960s and quickly replaced by 2nd generation MiG-21s as well as heavier and more capable Suchoj interceptors like the Su-9, -11 and -15. By 1972, all MiG-19bis had been retired.

  

General characteristics:

Crew: 1

Length: 13.54 m (44 ft 4 in), fuselage only with shock cone in forward position

15.48 m (50 8 ½ in) including pitot

Wingspan: 9 m (29 ft 6 in)

Height: 3.8885 m (12 ft 9 in)

Wing area: 25 m² (269 ft²)

Empty weight: 5,210 kg (11,475 lb)

Loaded weight: 7,890 kg (17,380 lb)

Max. takeoff weight: 9,050 kg (19,935 lb)

Fuel capacity: 2,450 l (556 imp gal; 647 US gal) internal;

plus 760 l (170 imp gal; 200 US gal) with 2 drop tanks

 

Powerplant:

2× Sorokin R3M-26 turbojets, rated at 37.2 kN (8,370 lbf) thrust each with afterburning

 

Performance:

Maximum speed: 1,380km/h at sea level (Mach=1.16)

1,850km/h at 12,000m (Mach=1.8)

Range: 1,250 km (775 mi; 750 nmi) at 14,000 m (45,000 ft) with 2 × 490 l drop tanks

Combat range: 500 km (312 mi; 270 nmi)

Ferry range: 2,000 km (1,242 mi; 690 nmi)

Service ceiling: 19,750 m (64,690 ft)

Rate of climb: 180 m/s (35,000 ft/min)

Wing loading: 353.3 kg/m² (72.4 lb/ft²)

Thrust/weight: 0.86

 

Armament:

No internal guns.

4× underwing pylons; typically, a pair of PTB-490 drop tanks were carried on the outer pylon pair,

plus a pair of air-to air missiles on the inner pair: initially two radar-guided Kaliningrad K-5M (RS-2US)

AAMs, later two radar-guided K-55 or IR-guided Vympel K-13 (AA-2 'Atoll') AAMs

  

The kit and its assembly:

Another submission for the 2018 Cold War Group Build at whatifmodelers.com, and again the opportunity to build a whiffy model from the project list. But it’s as fictional as one might think, since the SM-12 line of experimental “hybrid” fighters between the MiG-19 and the MiG-21 was real. But none of these aircraft ever made it into serial production, and in real life the MiG-21 showed so much potential that the attempts to improve the MiG-19 were stopped and no operational fighter entered production or service.

 

However, the SM-12, with its elongated nose and the central shock cone, makes a nice model subject, and I imagined what a service aircraft might have looked like? It would IMHO have been close, if not identical, to the SM-12PM, since this was the most refined pure jet fighter in the development family.

 

The basis for the build was a (dead cheap) Mastercraft MiG-19, which is a re-edition of the venerable Kovozávody Prostějov (KP) kit – as a tribute to modern tastes, it comes with (crudely) engraved panel, but it has a horrible fit all over. For instance, there was a 1mm gap between the fuselage and the right wing, the wing halves’ outlines did not match at all and it is questionable if the canopy actually belongs to the kit at all? PSR everywhere. I also had a Plastyk version of this kit on the table some time ago, but it was of a much better quality! O.K., the Mastercraft kit comes cheap, but it’s, to be honest, not a real bargain.

 

Even though the result would not be crisp I did some mods and changes. Internally, a cockpit tub was implanted (OOB there’s just a wacky seat hanging in mid air) plus some serious lead weight in the nose section for a proper stance.

On the outside, the new air intake is the most obvious change. I found a Su-17 intake (from a Mastercraft kit, too) and used a piece from a Matchbox B-17G’s dorsal turret to elongate the nose – it had an almost perfect diameter and a mildly conical shape. Some massive PSR work was necessary to blend the parts together, though.

The tail received new jet nozzles, scratched from steel needle protection covers, and the tail fairing was adjusted according to the real SM-12’s shape.

 

Ordnance was adapted, too: the drop tanks come from a Mastercraft MiG-21, and these supersonic PTB-490 tanks were indeed carried by the real SM-12 prototypes because the uprated engines were very thirsty and the original, teardrop-shaped MiG-19 tanks simply too draggy for the much faster SM-12. As a side note, the real SM-12’s short range was one of the serious factors that prevented the promising type’s production in real life. In order to overcome the poor range weakness I added an enlarged spine (half of a drop tank), inspired by the MiG-21 SMT, that would house an additional internal fuel tank.

 

The R2-SU/K-5 AAMs come from a vintage Mastercraft Soviet aircraft weapon set, which carries a pair of these 1st generation AAMs. While the molds seem to be a bit soft, the missiles look pretty convincing. Their pylons were taken from the kit (OOB they carry unguided AAM pods and are placed behind the main landing gear wells), just reversed and placed on the wings’ leading edges – similar to the real SM-12’s arrangement.

  

Painting and markings:

No surprises. In the Sixties, any PVO aircraft was left in bare metal, so there was hardly an alternative to a NMF finish.

 

Painting started with an all-over coat with acrylic Revell 99 (Aluminum), just the spine tank became light grey (Revell 371) for some contrast, and I painted some di-electric covers in a deep green (Revell 48).

The cockpit interior was painted with a bright mix of Revell 55 and some 48, while the landing gear wells and the back section of the cockpit were painted in a bluish grey (Revell 57).

The landing gear was painted in Steel (unpolished Modelmaster metallizer) and received classic, bright green wheel discs (Humbrol 2). As a small, unusual highlight the pitot boom under the chin received red and white stripes – seen on occasional MiG-19S fighters in Soviet service, and the anti-flutter booms on the stabilizers became bright red, too.

 

After the basic painting was done the kit received a black ink wash. Once this had dried and wiped off with a soft cotton cloth, post shading with various metallizer tones was added in order to liven up the uniform aircraft (including Humbrol’s matt and polished aluminum, and the exhaust section was treated with steel). Some panel lines were emphasized with a thin pencil.

 

Decals were puzzled together from various sources, a Guards badge and a few Russian stencils were added, too. Finally, the kit was sealed with a coat of sheen acrylic varnish (a 2:1 mix of Italeri matt and semi-gloss varnish).

 

The K-5 missiles, last but not least, were painted in aluminum, too, but their end caps (both front and tail section) became off-white.

  

The Mastercraft kit on which this conversion was based is crude, so I did not have high expectations concerning the outcome. But the new nose blends nicely into the MiG-19 fuselage, and the wide spine is a subtle detail that makes the aircraft look more “beefy” and less MiG-19-ish. The different drop tanks – even though they are authentic – visually add further speed. And despite many flaws, I am quite happy with the result of roundabout a week’s work.

Heavy Equipment Transporters (HET's) are capable of carrying a 70-ton Main Battle Tank on board. They can move their load rapidly and cost-effectively, saving wear and tear on the tracks – and the roads. The semi-trailers are equipped with a heavy-duty winch – giving an all-up weight of 104 tons.

 

The new Heavy Equipment Transporter is the most powerful tank transporter in production. It consists of an Oshkosh 1070F 8x8 tractor truck and a King Trailer GTS 100 seven axle semi-trailer.

 

The fully integrated power pack, comprises of a Caterpillar C18 after-cooled, turbocharged diesel engine developing 700hp, and is linked through to an electronically controlled X300 transmission unit.

 

The HET pictured, is seen departing Trowle Services on the M1 Motorway in Nottinghamshire. Note the multi-rear wheel steering on the semi-trailer.

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based historical facts. BEWARE!

 

Some background:

The Mikoyan-Gurevich MiG-19 (NATO reporting name: "Farmer") was a Soviet second-generation, single-seat, twin jet-engine fighter aircraft. It was the first Soviet production aircraft capable of supersonic speeds in level flight. A comparable U.S. "Century Series" fighter was the North American F-100 Super Sabre, although the MiG-19 would primarily oppose the more modern McDonnell Douglas F-4 Phantom II and Republic F-105 Thunderchief over North Vietnam. Furthermore, the North American YF-100 Super Sabre prototype appeared approximately one year after the MiG-19, making the MiG-19 the first operational supersonic jet in the world.

 

On 20 April 1951, OKB-155 was given the order to develop the MiG-17 into a new fighter called "I-340", also known as "SM-1". It was to be powered by two Mikulin AM-5 non-afterburning jet engines, a scaled-down version of the Mikulin AM-3, with 19.6 kN (4,410 lbf) of thrust. The I-340 was supposed to attain 1,160 km/h (725 mph, Mach 0.97) at 2,000 m (6,562 ft), 1,080 km/h (675 mph, Mach 1.0) at 10,000 m (32,808 ft), climb to 10,000 m (32,808 ft) in 2.9 minutes, and have a service ceiling of no less than 17,500 m (57,415 ft).

After several prototypes with many detail improvements, the ministers of the Soviet Union issued the order #286-133 to start serial production on February 17, 1954, at the factories in Gorkiy and Novosibirsk. Factory trials were completed on September 12 the same year, and government trials started on September 30.

 

Initial enthusiasm for the aircraft was dampened by several problems. The most alarming of these was the danger of a midair explosion due to overheating of the fuselage fuel tanks located between the engines. Deployment of airbrakes at high speeds caused a high-g pitch-up. Elevators lacked authority at supersonic speeds. The high landing speed of 230 km/h (145 mph), compared to 160 km/h (100 mph) for the MiG-15, combined with the lack of a two-seat trainer version, slowed pilot transition to the type. Handling problems were addressed with the second prototype, "SM-9/2", which added a third ventral airbrake and introduced all-moving tailplanes with a damper to prevent pilot-induced oscillations at subsonic speeds. It flew on 16 September 1954, and entered production as the MiG-19S.

 

Approximately 5,500 MiG-19's were produced, first in the USSR and in Czechoslovakia as the Avia S-105, but mainly in the People's Republic of China as the Shenyang J-6. The aircraft saw service with a number of other national air forces, including those of Cuba, North Vietnam, Egypt, Pakistan, and North Korea. The aircraft saw combat during the Vietnam War, the 1967 Six Day War, and the 1971 Bangladesh War.

 

However, jet fighter development made huge leaps in the 1960s, and OKB MiG was constantly trying to improve the MiG-19's performance, esp. against fast and high-flying enemies, primarily bombers but also spy planes like the U-2.

 

As the MiG-19S was brought into service with the Soviet air forces in mid-1956, the OKB MiG was continuing the refinement of the SM-1/I-340 fighter. One of these evolutionary paths was the SM-12 (literally, “SM-1, second generation”) family of prototypes, the ultimate extrapolation of the basic MiG-19 design, which eventually led to the MiG-19bis interceptor that filled the gap between the MiG-19S and the following, highly successful MiG-21.

 

The SM-12 first saw life as an exercise in drag reduction by means of new air intake configurations, since the MiG-19’s original intake with rounded lips became inefficient at supersonic speed (its Western rival, the North American F-100, featured a sharp-lipped nose air intake from the start). The first of three prototypes, the SM-12/1, was essentially a MiG-19S with an extended and straight-tapered nose with sharp-lipped orifice and a pointed, two-position shock cone on the intake splitter. The simple arrangement proved to be successful and was further refined.

 

The next evolutionary step, the SM-12/3, differed from its predecessors primarily in two new R3-26 turbojets developed from the earlier power plant by V. N. Sorokin. These each offered an afterburning thrust of 3,600kg, enabling the SM-12/3 to attain speeds ranging between 1,430km/h at sea level, or Mach=1.16, and 1,930km/h at 12,000m, or Mach=1.8, and an altitude of between 17,500 and 18,000m during its test program. This outstanding performance prompted further development with a view to production as a point defense interceptor.

 

Similarly powered by R3-26 engines, and embodying major nose redesign with a larger orifice permitting introduction of a substantial two-position conical centerbody for a TsD-30 radar, a further prototype was completed as the SM-12PM. Discarding the wing root NR-30 cannon of preceding prototypes, the SM-12PM was armed with only two K-5M (RS-2U) beam-riding missiles and entered flight test in 1957. This configuration would become the basis for the MiG-19bis interceptor that eventually was ordered into limited production (see below).

 

However, the SM-12 development line did not stop at this point. At the end of 1958, yet another prototype, the SM-12PMU, joined the experimental fighter family. This had R3M-26 turbojets uprated to 3.800kg with afterburning, but these were further augmented by a U-19D accelerator, which took the form of a permanent ventral pack containing an RU-013 rocket motor and its propellant tanks. Developed by D. D. Sevruk, the RU-013 delivered 3,000kg of additional thrust, and with the aid of this rocket motor, the SM-12PMU attained an altitude of 24,000m and a speed of Mach=1.69. But this effort was to no avail: the decision had been taken meanwhile to manufacture the Ye-7 in series as the MiG-21, and further development of the SM-12 series was therefore discontinued.

 

Nevertheless, since full operational status of the new MiG-21 was expected to remain pending for some time, production of a modified SM-12PM was ordered as a gap filler. Not only would this fighter bridge the performance gap to the Mach 2-capable MiG-21, it also had the benefit of being based on proven technologies and would not require a new basic pilot training.

 

The new aircraft received the official designation MiG-19bis. Compared with the SM-12PM prototype, the MiG-19bis differed in some details and improvements. The SM-12PM’s most significant shortfall was its short range – at full power, it had only a range of 750 km! This could be mended through an additional fuel tank in an enlarged dorsal fairing behind the cockpit. With this internal extra fuel, range could be extended by a further 200 - 250km range, but drop tanks had typically to be carried, too, in order to extend the fighter’ combat radius with two AAMs to 500 km. Specifically for the MiG-19bis, new, supersonic drop tanks (PTB-490) were designed, and these were later adapted for the MiG-21, too.

 

The air intake shock cone was re-contoured and the shifting mechanism improved: Instead of a simple, conical shape, the shock cone now had a more complex curvature with two steps and the intake orifice area was widened to allow a higher airflow rate. The air intake’s efficiency was further optimized through gradual positions of the shock cone.

As a positive side effect, the revised shock cone offered space for an enlarged radar dish, what improved detection range and resolution. The TsD-30 radar for the fighter’s missile-only armament was retained, even though the K-5’s effective range of only 2–6 km (1¼ – 3¾ mi) made it only suitable against slow and large targets like bombers. All guns were deleted in order to save weight or make room for the electronic equipment. The tail section was also changed because the R3M-26 engines and their afterburners were considerably longer than the MiG-19's original RM-5 engines. The exhausts now markedly protruded from the tail section, and the original, characteristic pen nib fairing between the two engines had been modified accordingly.

 

Production started in 1960, but only a total of roundabout 180 MiG-19bis, which received the NATO code "Farmer F", were built and the Soviet Union remained the only operator of the type. The first aircraft entered Soviet Anti-Air Defense in early 1961, and the machines were concentrated in PVO interceptor units around major sites like Moscow, Sewastopol at the Black Sea and Vladivostok in the Far East.

 

With the advent of the MiG-21, though, their career did not last long. Even though many machines were updated to carry the K-13 (the IR-guided AA-2 "Atoll") as well as the improved K-55 AAMs, with no change of the type’s designation, most MiG-19bis were already phased out towards the late 1960s and quickly replaced by 2nd generation MiG-21s as well as heavier and more capable Suchoj interceptors like the Su-9, -11 and -15. By 1972, all MiG-19bis had been retired.

  

General characteristics:

Crew: 1

Length: 13.54 m (44 ft 4 in), fuselage only with shock cone in forward position

15.48 m (50 8 ½ in) including pitot

Wingspan: 9 m (29 ft 6 in)

Height: 3.8885 m (12 ft 9 in)

Wing area: 25 m² (269 ft²)

Empty weight: 5,210 kg (11,475 lb)

Loaded weight: 7,890 kg (17,380 lb)

Max. takeoff weight: 9,050 kg (19,935 lb)

Fuel capacity: 2,450 l (556 imp gal; 647 US gal) internal;

plus 760 l (170 imp gal; 200 US gal) with 2 drop tanks

 

Powerplant:

2× Sorokin R3M-26 turbojets, rated at 37.2 kN (8,370 lbf) thrust each with afterburning

 

Performance:

Maximum speed: 1,380km/h at sea level (Mach=1.16)

1,850km/h at 12,000m (Mach=1.8)

Range: 1,250 km (775 mi; 750 nmi) at 14,000 m (45,000 ft) with 2 × 490 l drop tanks

Combat range: 500 km (312 mi; 270 nmi)

Ferry range: 2,000 km (1,242 mi; 690 nmi)

Service ceiling: 19,750 m (64,690 ft)

Rate of climb: 180 m/s (35,000 ft/min)

Wing loading: 353.3 kg/m² (72.4 lb/ft²)

Thrust/weight: 0.86

 

Armament:

No internal guns.

4× underwing pylons; typically, a pair of PTB-490 drop tanks were carried on the outer pylon pair,

plus a pair of air-to air missiles on the inner pair: initially two radar-guided Kaliningrad K-5M (RS-2US)

AAMs, later two radar-guided K-55 or IR-guided Vympel K-13 (AA-2 'Atoll') AAMs

  

The kit and its assembly:

Another submission for the 2018 Cold War Group Build at whatifmodelers.com, and again the opportunity to build a whiffy model from the project list. But it’s as fictional as one might think, since the SM-12 line of experimental “hybrid” fighters between the MiG-19 and the MiG-21 was real. But none of these aircraft ever made it into serial production, and in real life the MiG-21 showed so much potential that the attempts to improve the MiG-19 were stopped and no operational fighter entered production or service.

 

However, the SM-12, with its elongated nose and the central shock cone, makes a nice model subject, and I imagined what a service aircraft might have looked like? It would IMHO have been close, if not identical, to the SM-12PM, since this was the most refined pure jet fighter in the development family.

 

The basis for the build was a (dead cheap) Mastercraft MiG-19, which is a re-edition of the venerable Kovozávody Prostějov (KP) kit – as a tribute to modern tastes, it comes with (crudely) engraved panel, but it has a horrible fit all over. For instance, there was a 1mm gap between the fuselage and the right wing, the wing halves’ outlines did not match at all and it is questionable if the canopy actually belongs to the kit at all? PSR everywhere. I also had a Plastyk version of this kit on the table some time ago, but it was of a much better quality! O.K., the Mastercraft kit comes cheap, but it’s, to be honest, not a real bargain.

 

Even though the result would not be crisp I did some mods and changes. Internally, a cockpit tub was implanted (OOB there’s just a wacky seat hanging in mid air) plus some serious lead weight in the nose section for a proper stance.

On the outside, the new air intake is the most obvious change. I found a Su-17 intake (from a Mastercraft kit, too) and used a piece from a Matchbox B-17G’s dorsal turret to elongate the nose – it had an almost perfect diameter and a mildly conical shape. Some massive PSR work was necessary to blend the parts together, though.

The tail received new jet nozzles, scratched from steel needle protection covers, and the tail fairing was adjusted according to the real SM-12’s shape.

 

Ordnance was adapted, too: the drop tanks come from a Mastercraft MiG-21, and these supersonic PTB-490 tanks were indeed carried by the real SM-12 prototypes because the uprated engines were very thirsty and the original, teardrop-shaped MiG-19 tanks simply too draggy for the much faster SM-12. As a side note, the real SM-12’s short range was one of the serious factors that prevented the promising type’s production in real life. In order to overcome the poor range weakness I added an enlarged spine (half of a drop tank), inspired by the MiG-21 SMT, that would house an additional internal fuel tank.

 

The R2-SU/K-5 AAMs come from a vintage Mastercraft Soviet aircraft weapon set, which carries a pair of these 1st generation AAMs. While the molds seem to be a bit soft, the missiles look pretty convincing. Their pylons were taken from the kit (OOB they carry unguided AAM pods and are placed behind the main landing gear wells), just reversed and placed on the wings’ leading edges – similar to the real SM-12’s arrangement.

  

Painting and markings:

No surprises. In the Sixties, any PVO aircraft was left in bare metal, so there was hardly an alternative to a NMF finish.

 

Painting started with an all-over coat with acrylic Revell 99 (Aluminum), just the spine tank became light grey (Revell 371) for some contrast, and I painted some di-electric covers in a deep green (Revell 48).

The cockpit interior was painted with a bright mix of Revell 55 and some 48, while the landing gear wells and the back section of the cockpit were painted in a bluish grey (Revell 57).

The landing gear was painted in Steel (unpolished Modelmaster metallizer) and received classic, bright green wheel discs (Humbrol 2). As a small, unusual highlight the pitot boom under the chin received red and white stripes – seen on occasional MiG-19S fighters in Soviet service, and the anti-flutter booms on the stabilizers became bright red, too.

 

After the basic painting was done the kit received a black ink wash. Once this had dried and wiped off with a soft cotton cloth, post shading with various metallizer tones was added in order to liven up the uniform aircraft (including Humbrol’s matt and polished aluminum, and the exhaust section was treated with steel). Some panel lines were emphasized with a thin pencil.

 

Decals were puzzled together from various sources, a Guards badge and a few Russian stencils were added, too. Finally, the kit was sealed with a coat of sheen acrylic varnish (a 2:1 mix of Italeri matt and semi-gloss varnish).

 

The K-5 missiles, last but not least, were painted in aluminum, too, but their end caps (both front and tail section) became off-white.

  

The Mastercraft kit on which this conversion was based is crude, so I did not have high expectations concerning the outcome. But the new nose blends nicely into the MiG-19 fuselage, and the wide spine is a subtle detail that makes the aircraft look more “beefy” and less MiG-19-ish. The different drop tanks – even though they are authentic – visually add further speed. And despite many flaws, I am quite happy with the result of roundabout a week’s work.

Colosseum

Following, a text, in english, from the Wikipedia the Free Encyclopedia:

The Colosseum, or the Coliseum, originally the Flavian Amphitheatre (Latin: Amphitheatrum Flavium, Italian Anfiteatro Flavio or Colosseo), is an elliptical amphitheatre in the centre of the city of Rome, Italy, the largest ever built in the Roman Empire. It is considered one of the greatest works of Roman architecture and Roman engineering.

Occupying a site just east of the Roman Forum, its construction started between 70 and 72 AD[1] under the emperor Vespasian and was completed in 80 AD under Titus,[2] with further modifications being made during Domitian's reign (81–96).[3] The name "Amphitheatrum Flavium" derives from both Vespasian's and Titus's family name (Flavius, from the gens Flavia).

Capable of seating 50,000 spectators,[1][4][5] the Colosseum was used for gladiatorial contests and public spectacles such as mock sea battles, animal hunts, executions, re-enactments of famous battles, and dramas based on Classical mythology. The building ceased to be used for entertainment in the early medieval era. It was later reused for such purposes as housing, workshops, quarters for a religious order, a fortress, a quarry, and a Christian shrine.

Although in the 21st century it stays partially ruined because of damage caused by devastating earthquakes and stone-robbers, the Colosseum is an iconic symbol of Imperial Rome. It is one of Rome's most popular tourist attractions and still has close connections with the Roman Catholic Church, as each Good Friday the Pope leads a torchlit "Way of the Cross" procession that starts in the area around the Colosseum.[6]

The Colosseum is also depicted on the Italian version of the five-cent euro coin.

The Colosseum's original Latin name was Amphitheatrum Flavium, often anglicized as Flavian Amphitheater. The building was constructed by emperors of the Flavian dynasty, hence its original name, after the reign of Emperor Nero.[7] This name is still used in modern English, but generally the structure is better known as the Colosseum. In antiquity, Romans may have referred to the Colosseum by the unofficial name Amphitheatrum Caesareum; this name could have been strictly poetic.[8][9] This name was not exclusive to the Colosseum; Vespasian and Titus, builders of the Colosseum, also constructed an amphitheater of the same name in Puteoli (modern Pozzuoli).[10]

The name Colosseum has long been believed to be derived from a colossal statue of Nero nearby.[3] (the statue of Nero itself being named after one of the original ancient wonders, the Colossus of Rhodes[citation needed]. This statue was later remodeled by Nero's successors into the likeness of Helios (Sol) or Apollo, the sun god, by adding the appropriate solar crown. Nero's head was also replaced several times with the heads of succeeding emperors. Despite its pagan links, the statue remained standing well into the medieval era and was credited with magical powers. It came to be seen as an iconic symbol of the permanence of Rome.

In the 8th century, a famous epigram attributed to the Venerable Bede celebrated the symbolic significance of the statue in a prophecy that is variously quoted: Quamdiu stat Colisæus, stat et Roma; quando cadet colisæus, cadet et Roma; quando cadet Roma, cadet et mundus ("as long as the Colossus stands, so shall Rome; when the Colossus falls, Rome shall fall; when Rome falls, so falls the world").[11] This is often mistranslated to refer to the Colosseum rather than the Colossus (as in, for instance, Byron's poem Childe Harold's Pilgrimage). However, at the time that the Pseudo-Bede wrote, the masculine noun coliseus was applied to the statue rather than to what was still known as the Flavian amphitheatre.

The Colossus did eventually fall, possibly being pulled down to reuse its bronze. By the year 1000 the name "Colosseum" had been coined to refer to the amphitheatre. The statue itself was largely forgotten and only its base survives, situated between the Colosseum and the nearby Temple of Venus and Roma.[12]

The name further evolved to Coliseum during the Middle Ages. In Italy, the amphitheatre is still known as il Colosseo, and other Romance languages have come to use similar forms such as le Colisée (French), el Coliseo (Spanish) and o Coliseu (Portuguese).

Construction of the Colosseum began under the rule of the Emperor Vespasian[3] in around 70–72AD. The site chosen was a flat area on the floor of a low valley between the Caelian, Esquiline and Palatine Hills, through which a canalised stream ran. By the 2nd century BC the area was densely inhabited. It was devastated by the Great Fire of Rome in AD 64, following which Nero seized much of the area to add to his personal domain. He built the grandiose Domus Aurea on the site, in front of which he created an artificial lake surrounded by pavilions, gardens and porticoes. The existing Aqua Claudia aqueduct was extended to supply water to the area and the gigantic bronze Colossus of Nero was set up nearby at the entrance to the Domus Aurea.[12]

Although the Colossus was preserved, much of the Domus Aurea was torn down. The lake was filled in and the land reused as the location for the new Flavian Amphitheatre. Gladiatorial schools and other support buildings were constructed nearby within the former grounds of the Domus Aurea. According to a reconstructed inscription found on the site, "the emperor Vespasian ordered this new amphitheatre to be erected from his general's share of the booty." This is thought to refer to the vast quantity of treasure seized by the Romans following their victory in the Great Jewish Revolt in 70AD. The Colosseum can be thus interpreted as a great triumphal monument built in the Roman tradition of celebrating great victories[12], placating the Roman people instead of returning soldiers. Vespasian's decision to build the Colosseum on the site of Nero's lake can also be seen as a populist gesture of returning to the people an area of the city which Nero had appropriated for his own use. In contrast to many other amphitheatres, which were located on the outskirts of a city, the Colosseum was constructed in the city centre; in effect, placing it both literally and symbolically at the heart of Rome.

The Colosseum had been completed up to the third story by the time of Vespasian's death in 79. The top level was finished and the building inaugurated by his son, Titus, in 80.[3] Dio Cassius recounts that over 9,000 wild animals were killed during the inaugural games of the amphitheatre. The building was remodelled further under Vespasian's younger son, the newly designated Emperor Domitian, who constructed the hypogeum, a series of underground tunnels used to house animals and slaves. He also added a gallery to the top of the Colosseum to increase its seating capacity.

In 217, the Colosseum was badly damaged by a major fire (caused by lightning, according to Dio Cassius[13]) which destroyed the wooden upper levels of the amphitheatre's interior. It was not fully repaired until about 240 and underwent further repairs in 250 or 252 and again in 320. An inscription records the restoration of various parts of the Colosseum under Theodosius II and Valentinian III (reigned 425–455), possibly to repair damage caused by a major earthquake in 443; more work followed in 484[14] and 508. The arena continued to be used for contests well into the 6th century, with gladiatorial fights last mentioned around 435. Animal hunts continued until at least 523, when Anicius Maximus celebrated his consulship with some venationes, criticised by King Theodoric the Great for their high cost.

The Colosseum underwent several radical changes of use during the medieval period. By the late 6th century a small church had been built into the structure of the amphitheatre, though this apparently did not confer any particular religious significance on the building as a whole. The arena was converted into a cemetery. The numerous vaulted spaces in the arcades under the seating were converted into housing and workshops, and are recorded as still being rented out as late as the 12th century. Around 1200 the Frangipani family took over the Colosseum and fortified it, apparently using it as a castle.

Severe damage was inflicted on the Colosseum by the great earthquake in 1349, causing the outer south side, lying on a less stable alluvional terrain, to collapse. Much of the tumbled stone was reused to build palaces, churches, hospitals and other buildings elsewhere in Rome. A religious order moved into the northern third of the Colosseum in the mid-14th century and continued to inhabit it until as late as the early 19th century. The interior of the amphitheatre was extensively stripped of stone, which was reused elsewhere, or (in the case of the marble façade) was burned to make quicklime.[12] The bronze clamps which held the stonework together were pried or hacked out of the walls, leaving numerous pockmarks which still scar the building today.

During the 16th and 17th century, Church officials sought a productive role for the vast derelict hulk of the Colosseum. Pope Sixtus V (1585–1590) planned to turn the building into a wool factory to provide employment for Rome's prostitutes, though this proposal fell through with his premature death.[15] In 1671 Cardinal Altieri authorized its use for bullfights; a public outcry caused the idea to be hastily abandoned.

In 1749, Pope Benedict XIV endorsed as official Church policy the view that the Colosseum was a sacred site where early Christians had been martyred. He forbade the use of the Colosseum as a quarry and consecrated the building to the Passion of Christ and installed Stations of the Cross, declaring it sanctified by the blood of the Christian martyrs who perished there (see Christians and the Colosseum). However there is no historical evidence to support Benedict's claim, nor is there even any evidence that anyone prior to the 16th century suggested this might be the case; the Catholic Encyclopedia concludes that there are no historical grounds for the supposition. Later popes initiated various stabilization and restoration projects, removing the extensive vegetation which had overgrown the structure and threatened to damage it further. The façade was reinforced with triangular brick wedges in 1807 and 1827, and the interior was repaired in 1831, 1846 and in the 1930s. The arena substructure was partly excavated in 1810–1814 and 1874 and was fully exposed under Benito Mussolini in the 1930s.

The Colosseum is today one of Rome's most popular tourist attractions, receiving millions of visitors annually. The effects of pollution and general deterioration over time prompted a major restoration programme carried out between 1993 and 2000, at a cost of 40 billion Italian lire ($19.3m / €20.6m at 2000 prices). In recent years it has become a symbol of the international campaign against capital punishment, which was abolished in Italy in 1948. Several anti–death penalty demonstrations took place in front of the Colosseum in 2000. Since that time, as a gesture against the death penalty, the local authorities of Rome change the color of the Colosseum's night time illumination from white to gold whenever a person condemned to the death penalty anywhere in the world gets their sentence commuted or is released,[16] or if a jurisdiction abolishes the death penalty. Most recently, the Colosseum was illuminated in gold when capital punishment was abolished in the American state of New Mexico in April 2009.

Because of the ruined state of the interior, it is impractical to use the Colosseum to host large events; only a few hundred spectators can be accommodated in temporary seating. However, much larger concerts have been held just outside, using the Colosseum as a backdrop. Performers who have played at the Colosseum in recent years have included Ray Charles (May 2002),[18] Paul McCartney (May 2003),[19] Elton John (September 2005),[20] and Billy Joel (July 2006).

Exterior

Unlike earlier Greek theatres that were built into hillsides, the Colosseum is an entirely free-standing structure. It derives its basic exterior and interior architecture from that of two Roman theatres back to back. It is elliptical in plan and is 189 meters (615 ft / 640 Roman feet) long, and 156 meters (510 ft / 528 Roman feet) wide, with a base area of 6 acres (24,000 m2). The height of the outer wall is 48 meters (157 ft / 165 Roman feet). The perimeter originally measured 545 meters (1,788 ft / 1,835 Roman feet). The central arena is an oval 87 m (287 ft) long and 55 m (180 ft) wide, surrounded by a wall 5 m (15 ft) high, above which rose tiers of seating.

The outer wall is estimated to have required over 100,000 cubic meters (131,000 cu yd) of travertine stone which were set without mortar held together by 300 tons of iron clamps.[12] However, it has suffered extensive damage over the centuries, with large segments having collapsed following earthquakes. The north side of the perimeter wall is still standing; the distinctive triangular brick wedges at each end are modern additions, having been constructed in the early 19th century to shore up the wall. The remainder of the present-day exterior of the Colosseum is in fact the original interior wall.

The surviving part of the outer wall's monumental façade comprises three stories of superimposed arcades surmounted by a podium on which stands a tall attic, both of which are pierced by windows interspersed at regular intervals. The arcades are framed by half-columns of the Tuscan, Ionic, and Corinthian orders, while the attic is decorated with Corinthian pilasters.[21] Each of the arches in the second- and third-floor arcades framed statues, probably honoring divinities and other figures from Classical mythology.

Two hundred and forty mast corbels were positioned around the top of the attic. They originally supported a retractable awning, known as the velarium, that kept the sun and rain off spectators. This consisted of a canvas-covered, net-like structure made of ropes, with a hole in the center.[3] It covered two-thirds of the arena, and sloped down towards the center to catch the wind and provide a breeze for the audience. Sailors, specially enlisted from the Roman naval headquarters at Misenum and housed in the nearby Castra Misenatium, were used to work the velarium.[22]

The Colosseum's huge crowd capacity made it essential that the venue could be filled or evacuated quickly. Its architects adopted solutions very similar to those used in modern stadiums to deal with the same problem. The amphitheatre was ringed by eighty entrances at ground level, 76 of which were used by ordinary spectators.[3] Each entrance and exit was numbered, as was each staircase. The northern main entrance was reserved for the Roman Emperor and his aides, whilst the other three axial entrances were most likely used by the elite. All four axial entrances were richly decorated with painted stucco reliefs, of which fragments survive. Many of the original outer entrances have disappeared with the collapse of the perimeter wall, but entrances XXIII (23) to LIV (54) still survive.[12]

Spectators were given tickets in the form of numbered pottery shards, which directed them to the appropriate section and row. They accessed their seats via vomitoria (singular vomitorium), passageways that opened into a tier of seats from below or behind. These quickly dispersed people into their seats and, upon conclusion of the event or in an emergency evacuation, could permit their exit within only a few minutes. The name vomitoria derived from the Latin word for a rapid discharge, from which English derives the word vomit.

Interior

According to the Codex-Calendar of 354, the Colosseum could accommodate 87,000 people, although modern estimates put the figure at around 50,000. They were seated in a tiered arrangement that reflected the rigidly stratified nature of Roman society. Special boxes were provided at the north and south ends respectively for the Emperor and the Vestal Virgins, providing the best views of the arena. Flanking them at the same level was a broad platform or podium for the senatorial class, who were allowed to bring their own chairs. The names of some 5th century senators can still be seen carved into the stonework, presumably reserving areas for their use.

The tier above the senators, known as the maenianum primum, was occupied by the non-senatorial noble class or knights (equites). The next level up, the maenianum secundum, was originally reserved for ordinary Roman citizens (plebians) and was divided into two sections. The lower part (the immum) was for wealthy citizens, while the upper part (the summum) was for poor citizens. Specific sectors were provided for other social groups: for instance, boys with their tutors, soldiers on leave, foreign dignitaries, scribes, heralds, priests and so on. Stone (and later marble) seating was provided for the citizens and nobles, who presumably would have brought their own cushions with them. Inscriptions identified the areas reserved for specific groups.

Another level, the maenianum secundum in legneis, was added at the very top of the building during the reign of Domitian. This comprised a gallery for the common poor, slaves and women. It would have been either standing room only, or would have had very steep wooden benches. Some groups were banned altogether from the Colosseum, notably gravediggers, actors and former gladiators.

Each tier was divided into sections (maeniana) by curved passages and low walls (praecinctiones or baltei), and were subdivided into cunei, or wedges, by the steps and aisles from the vomitoria. Each row (gradus) of seats was numbered, permitting each individual seat to be exactly designated by its gradus, cuneus, and number.

The arena itself was 83 meters by 48 meters (272 ft by 157 ft / 280 by 163 Roman feet).[12] It comprised a wooden floor covered by sand (the Latin word for sand is harena or arena), covering an elaborate underground structure called the hypogeum (literally meaning "underground"). Little now remains of the original arena floor, but the hypogeum is still clearly visible. It consisted of a two-level subterranean network of tunnels and cages beneath the arena where gladiators and animals were held before contests began. Eighty vertical shafts provided instant access to the arena for caged animals and scenery pieces concealed underneath; larger hinged platforms, called hegmata, provided access for elephants and the like. It was restructured on numerous occasions; at least twelve different phases of construction can be seen.[12]

The hypogeum was connected by underground tunnels to a number of points outside the Colosseum. Animals and performers were brought through the tunnel from nearby stables, with the gladiators' barracks at the Ludus Magnus to the east also being connected by tunnels. Separate tunnels were provided for the Emperor and the Vestal Virgins to permit them to enter and exit the Colosseum without needing to pass through the crowds.[12]

Substantial quantities of machinery also existed in the hypogeum. Elevators and pulleys raised and lowered scenery and props, as well as lifting caged animals to the surface for release. There is evidence for the existence of major hydraulic mechanisms[12] and according to ancient accounts, it was possible to flood the arena rapidly, presumably via a connection to a nearby aqueduct.

The Colosseum and its activities supported a substantial industry in the area. In addition to the amphitheatre itself, many other buildings nearby were linked to the games. Immediately to the east is the remains of the Ludus Magnus, a training school for gladiators. This was connected to the Colosseum by an underground passage, to allow easy access for the gladiators. The Ludus Magnus had its own miniature training arena, which was itself a popular attraction for Roman spectators. Other training schools were in the same area, including the Ludus Matutinus (Morning School), where fighters of animals were trained, plus the Dacian and Gallic Schools.

Also nearby were the Armamentarium, comprising an armory to store weapons; the Summum Choragium, where machinery was stored; the Sanitarium, which had facilities to treat wounded gladiators; and the Spoliarium, where bodies of dead gladiators were stripped of their armor and disposed of.

Around the perimeter of the Colosseum, at a distance of 18 m (59 ft) from the perimeter, was a series of tall stone posts, with five remaining on the eastern side. Various explanations have been advanced for their presence; they may have been a religious boundary, or an outer boundary for ticket checks, or an anchor for the velarium or awning.

Right next to the Colosseum is also the Arch of Constantine.

he Colosseum was used to host gladiatorial shows as well as a variety of other events. The shows, called munera, were always given by private individuals rather than the state. They had a strong religious element but were also demonstrations of power and family prestige, and were immensely popular with the population. Another popular type of show was the animal hunt, or venatio. This utilized a great variety of wild beasts, mainly imported from Africa and the Middle East, and included creatures such as rhinoceros, hippopotamuses, elephants, giraffes, aurochs, wisents, barbary lions, panthers, leopards, bears, caspian tigers, crocodiles and ostriches. Battles and hunts were often staged amid elaborate sets with movable trees and buildings. Such events were occasionally on a huge scale; Trajan is said to have celebrated his victories in Dacia in 107 with contests involving 11,000 animals and 10,000 gladiators over the course of 123 days.

During the early days of the Colosseum, ancient writers recorded that the building was used for naumachiae (more properly known as navalia proelia) or simulated sea battles. Accounts of the inaugural games held by Titus in AD 80 describe it being filled with water for a display of specially trained swimming horses and bulls. There is also an account of a re-enactment of a famous sea battle between the Corcyrean (Corfiot) Greeks and the Corinthians. This has been the subject of some debate among historians; although providing the water would not have been a problem, it is unclear how the arena could have been waterproofed, nor would there have been enough space in the arena for the warships to move around. It has been suggested that the reports either have the location wrong, or that the Colosseum originally featured a wide floodable channel down its central axis (which would later have been replaced by the hypogeum).[12]

Sylvae or recreations of natural scenes were also held in the arena. Painters, technicians and architects would construct a simulation of a forest with real trees and bushes planted in the arena's floor. Animals would be introduced to populate the scene for the delight of the crowd. Such scenes might be used simply to display a natural environment for the urban population, or could otherwise be used as the backdrop for hunts or dramas depicting episodes from mythology. They were also occasionally used for executions in which the hero of the story — played by a condemned person — was killed in one of various gruesome but mythologically authentic ways, such as being mauled by beasts or burned to death.

The Colosseum today is now a major tourist attraction in Rome with thousands of tourists each year paying to view the interior arena, though entrance for EU citizens is partially subsidised, and under-18 and over-65 EU citizens' entrances are free.[24] There is now a museum dedicated to Eros located in the upper floor of the outer wall of the building. Part of the arena floor has been re-floored. Beneath the Colosseum, a network of subterranean passageways once used to transport wild animals and gladiators to the arena opened to the public in summer 2010.[25]

The Colosseum is also the site of Roman Catholic ceremonies in the 20th and 21st centuries. For instance, Pope Benedict XVI leads the Stations of the Cross called the Scriptural Way of the Cross (which calls for more meditation) at the Colosseum[26][27] on Good Fridays.

In the Middle Ages, the Colosseum was clearly not regarded as a sacred site. Its use as a fortress and then a quarry demonstrates how little spiritual importance was attached to it, at a time when sites associated with martyrs were highly venerated. It was not included in the itineraries compiled for the use of pilgrims nor in works such as the 12th century Mirabilia Urbis Romae ("Marvels of the City of Rome"), which claims the Circus Flaminius — but not the Colosseum — as the site of martyrdoms. Part of the structure was inhabited by a Christian order, but apparently not for any particular religious reason.

It appears to have been only in the 16th and 17th centuries that the Colosseum came to be regarded as a Christian site. Pope Pius V (1566–1572) is said to have recommended that pilgrims gather sand from the arena of the Colosseum to serve as a relic, on the grounds that it was impregnated with the blood of martyrs. This seems to have been a minority view until it was popularised nearly a century later by Fioravante Martinelli, who listed the Colosseum at the head of a list of places sacred to the martyrs in his 1653 book Roma ex ethnica sacra.

Martinelli's book evidently had an effect on public opinion; in response to Cardinal Altieri's proposal some years later to turn the Colosseum into a bullring, Carlo Tomassi published a pamphlet in protest against what he regarded as an act of desecration. The ensuing controversy persuaded Pope Clement X to close the Colosseum's external arcades and declare it a sanctuary, though quarrying continued for some time.

At the instance of St. Leonard of Port Maurice, Pope Benedict XIV (1740–1758) forbade the quarrying of the Colosseum and erected Stations of the Cross around the arena, which remained until February 1874. St. Benedict Joseph Labre spent the later years of his life within the walls of the Colosseum, living on alms, prior to his death in 1783. Several 19th century popes funded repair and restoration work on the Colosseum, and it still retains a Christian connection today. Crosses stand in several points around the arena and every Good Friday the Pope leads a Via Crucis procession to the amphitheatre.

 

Coliseu (Colosseo)

A seguir, um texto, em português, da Wikipédia, a enciclopédia livre:

 

O Coliseu, também conhecido como Anfiteatro Flaviano, deve seu nome à expressão latina Colosseum (ou Coliseus, no latim tardio), devido à estátua colossal de Nero, que ficava perto a edificação. Localizado no centro de Roma, é uma excepção de entre os anfiteatros pelo seu volume e relevo arquitectónico. Originalmente capaz de albergar perto de 50 000 pessoas, e com 48 metros de altura, era usado para variados espetáculos. Foi construído a leste do fórum romano e demorou entre 8 a 10 anos a ser construído.

O Coliseu foi utilizado durante aproximadamente 500 anos, tendo sido o último registro efetuado no século VI da nossa era, bastante depois da queda de Roma em 476. O edifício deixou de ser usado para entretenimento no começo da era medieval, mas foi mais tarde usado como habitação, oficina, forte, pedreira, sede de ordens religiosas e templo cristão.

Embora esteja agora em ruínas devido a terremotos e pilhagens, o Coliseu sempre foi visto como símbolo do Império Romano, sendo um dos melhores exemplos da sua arquitectura. Actualmente é uma das maiores atrações turísticas em Roma e em 7 de julho de 2007 foi eleita umas das "Sete maravilhas do mundo moderno". Além disso, o Coliseu ainda tem ligações à igreja, com o Papa a liderar a procissão da Via Sacra até ao Coliseu todas as Sextas-feiras Santas.

O coliseu era um local onde seriam exibidos toda uma série de espectáculos, inseridos nos vários tipos de jogos realizados na urbe. Os combates entre gladiadores, chamados muneras, eram sempre pagos por pessoas individuais em busca de prestígio e poder em vez do estado. A arena (87,5 m por 55 m) possuía um piso de madeira, normalmente coberto de areia para absorver o sangue dos combates (certa vez foi colocada água na representação de uma batalha naval), sob o qual existia um nível subterrâneo com celas e jaulas que tinham acessos diretos para a arena; Alguns detalhes dessa construção, como a cobertura removível que poupava os espectadores do sol, são bastante interessantes, e mostram o refinamento atingido pelos construtores romanos. Formado por cinco anéis concêntricos de arcos e abóbadas, o Coliseu representa bem o avanço introduzido pelos romanos à engenharia de estruturas. Esses arcos são de concreto (de cimento natural) revestidos por alvenaria. Na verdade, a alvenaria era construída simultaneamente e já servia de forma para a concretagem. Outro tipo de espetáculos era a caça de animais, ou venatio, onde eram utilizados animais selvagens importados de África. Os animais mais utilizados eram os grandes felinos como leões, leopardos e panteras, mas animais como rinocerontes, hipopótamos, elefantes, girafas, crocodilos e avestruzes eram também utilizados. As caçadas, tal como as representações de batalhas famosas, eram efetuadas em elaborados cenários onde constavam árvores e edifícios amovíveis.

Estas últimas eram por vezes representadas numa escala gigante; Trajano celebrou a sua vitória em Dácia no ano 107 com concursos envolvendo 11 000 animais e 10 000 gladiadores no decorrer de 123 dias.

Segundo o documentário produzido pelo canal televisivo fechado, History Channel, o Coliseu também era utilizado para a realização de naumaquias, ou batalhas navais. O coliseu era inundado por dutos subterrâneos alimentados pelos aquedutos que traziam água de longe. Passada esta fase, foi construída uma estrutura, que é a que podemos ver hoje nas ruínas do Coliseu, com altura de um prédio de dois andares, onde no passado se concentravam os gladiadores, feras e todo o pessoal que organizava os duelos que ocorreriam na arena. A arena era como um grande palco, feito de madeira, e se chama arena, que em italiano significa areia, porque era jogada areia sob a estrutura de madeira para esconder as imperfeições. Os animais podiam ser inseridos nos duelos a qualquer momento por um esquema de elevadores que surgiam em alguns pontos da arena; o filme "Gladiador" retrata muito bem esta questão dos elevadores. Os estudiosos, há pouco tempo, descobriram uma rede de dutos inundados por baixo da arena do Coliseu. Acredita-se que o Coliseu foi construído onde, outrora, foi o lago do Palácio Dourado de Nero; O imperador Vespasiano escolheu o local da construção para que o mal causado por Nero fosse esquecido por uma construção gloriosa.

Sylvae, ou recreações de cenas naturais eram também realizadas no Coliseu. Pintores, técnicos e arquitectos construiriam simulações de florestas com árvores e arbustos reais plantados no chão da arena. Animais seriam então introduzidos para dar vida à simulação. Esses cenários podiam servir só para agrado do público ou como pano de fundo para caçadas ou dramas representando episódios da mitologia romana, tão autênticos quanto possível, ao ponto de pessoas condenadas fazerem o papel de heróis onde eram mortos de maneiras horríveis mas mitologicamente autênticas, como mutilados por animais ou queimados vivos.

Embora o Coliseu tenha funcionado até ao século VI da nossa Era, foram proibidos os jogos com mortes humanas desde 404, sendo apenas massacrados animais como elefantes, panteras ou leões.

O Coliseu era sobretudo um enorme instrumento de propaganda e difusão da filosofia de toda uma civilização, e tal como era já profetizado pelo monge e historiador inglês Beda na sua obra do século VII "De temporibus liber": "Enquanto o Coliseu se mantiver de pé, Roma permanecerá; quando o Coliseu ruir, Roma ruirá e quando Roma cair, o mundo cairá".

A construção do Coliseu foi iniciada por Vespasiano, nos anos 70 da nossa era. O edifício foi inaugurado por Tito, em 80, embora apenas tivesse sido finalizado poucos anos depois. Empresa colossal, este edifício, inicialmente, poderia sustentar no seu interior cerca de 50 000 espectadores, constando de três andares. Aquando do reinado de Alexandre Severo e Gordiano III, é ampliado com um quarto andar, podendo suster agora cerca de 90 000 espectadores. A grandiosidade deste monumento testemunha verdadeiramente o poder e esplendor de Roma na época dos Flávios.

Os jogos inaugurais do Coliseu tiveram lugar ano 80, sob o mandato de Tito, para celebrar a finalização da construção. Depois do curto reinado de Tito começar com vários meses de desastres, incluindo a erupção do Monte Vesúvio, um incêndio em Roma, e um surto de peste, o mesmo imperador inaugurou o edifício com uns jogos pródigos que duraram mais de cem dias, talvez para tentar apaziguar o público romano e os deuses. Nesses jogos de cem dias terão ocorrido combates de gladiadores, venationes (lutas de animais), execuções, batalhas navais, caçadas e outros divertimentos numa escala sem precedentes.

O Coliseu, como não se encontrava inserido numa zona de encosta, enterrado, tal como normalmente sucede com a generalidade dos teatros e anfiteatros romanos, possuía um “anel” artificial de rocha à sua volta, para garantir sustentação e, ao mesmo tempo, esta substrutura serve como ornamento ao edifício e como condicionador da entrada dos espectadores. Tal como foi referido anteriormente, possuía três pisos, sendo mais tarde adicionado um outro. É construído em mármore, pedra travertina, ladrilho e tufo (pedra calcária com grandes poros). A sua planta elíptica mede dois eixos que se estendem aproximadamente de 190 m por 155 m. A fachada compõe-se de arcadas decoradas com colunas dóricas, jónicas e coríntias, de acordo com o pavimento em que se encontravam. Esta subdivisão deve-se ao facto de ser uma construção essencialmente vertical, criando assim uma diversificação do espaço.

 

Os assentos eram em mármore e a cavea, escadaria ou arquibancada, dividia-se em três partes, correspondentes às diferentes classes sociais: o podium, para as classes altas; as maeniana, sector destinado à classe média; e os portici, ou pórticos, construídos em madeira, para a plebe e as mulheres. O pulvinar, a tribuna imperial, encontrava-se situada no podium e era balizada pelos assentos reservados aos senadores e magistrados. Rampas no interior do edifício facilitavam o acesso às várias zonas de onde podiam visualizar o espectáculo, sendo protegidos por uma barreira e por uma série de arqueiros posicionados numa passagem de madeira, para o caso de algum acidente. Por cima dos muros ainda são visíveis as mísulas, que sustentavam o velarium, enorme cobertura de lona destinada a proteger do sol os espectadores e, nos subterrâneos, ficavam as jaulas dos animais, bem como todas as celas e galerias necessárias aos serviços do anfiteatro.

O monumento permaneceu como sede principal dos espetáculos da urbe romana até ao período do imperador Honorius, no século V. Danificado por um terremoto no começo do mesmo século, foi alvo de uma extensiva restauração na época de Valentinianus III. Em meados do século XIII, a família Frangipani transformou-o em fortaleza e, ao longo dos séculos XV e XVI, foi por diversas vezes saqueado, perdendo grande parte dos materiais nobres com os quais tinha sido construído.

Os relatos romanos referem-se a cristãos sendo martirizados em locais de Roma descritos pouco pormenorizadamente (no anfiteatro, na arena...), quando Roma tinha numerosos anfiteatros e arenas. Apesar de muito provavelmente o Coliseu não ter sido utilizado para martírios, o Papa Bento XIV consagrou-o no século XVII à Paixão de Cristo e declarou-o lugar sagrado. Os trabalhos de consolidação e restauração parcial do monumento, já há muito em ruínas, foram feitos sobretudo pelos pontífices Gregório XVI e Pio IX, no século XIX.

Built by the Schiffswerks Rieherst company in Hamburg, the Umbria was launched on December 30th 1911 with the name of Bahia Blanca. It was a large freighter by that time, 150 meters long, with a power capable of providing a speed of 14 knots that could carry 9,000 tons of cargo and up to 2,000 passengers. In 1912 it began operating the Hamburg-America line doing different jobs between Europe and Argentina until the outbreak of World War I, when it was based in Buenos Aires. In 1918 the ship was acquired by the Argentinian government and it was not until 1935 when the ship was taken over by the Italian government and renamed again: the Umbria. From that moment its trips were to transport troops and during the following two years carried several thousand soldiers to the Italian colonies in East Africa.

  

The loss of the Umbria

 

In May 1940, when Italy was still neutral in World War II, the Umbria was secretly loaded with 360,000 bombs between 15 kg and 100 kg, 60 boxes of detonators, building materials and three Fiat Lunga cars, carrying a total 8,600 tons of weapons towards the East Africa. The explosives had destination Massawa and Assab, Eritrea, that was Italian colony by then, and the rest of the cargo was heading different locations in Asia. Italy's entry into the war was imminent and this shipment was destined to the defense of the colonies against the Allies and to the possible expansion of its African territories.

   

On 3rd June 1940 the Umbria reached Port Said, northern Egypt, where loaded with 1,000 tons of coal and water in a movement to fool the Allies, trying to look like a harmless freighter. The port, controlled by the Royal Navy, and its authorities allowed the ship enter on the Red Sea three days after arrival. The British delayed the departure of the Umbria knowing that Italy's entry into the war was imminent and that the cargo of Umbria had devastating power that sooner or later would be used against the Allies and why not, to get a great load to fight fascism. But Italy, as a neutral country that it was, had every right to transport weapons much like any other cargo to its colonies.

   

Having met the deadline to be retained, the Umbria crossed the Suez Canal on June 6th but with the escort of the HMS Grimsby. The importance and destructive capacity of the cargo required it. Three days later the Umbria entered in Sudan waters and the HMS Grimsby ordered the Umbria captain to anchor on Wingate Reef under the pretext of searching for contraband. Moments later the British warship HMS Leander arrived with a group of 20 sailors who boarded the Umbria. After thoroughly searching the ship and finding nothing, the captain ordered the British troops to remain the night aboard the Umbria.

The next morning Lorenzo Muiesan, Umbria captain, was in his cabin listening to the radio when Mussolini announced the entry of Italy into the World War II. Hostilities would begin at midnight of that day. Muiesan, a very patriotic captain with long experience, was the only one in the area who had heard the news and knew immediately that both Umbria and the burden would be used by the Allies against their own country. He had no option to disable both. In a move of extraordinary intelligence, as the hours passed retained by the British who did not yet know that Italy was officially the enemy, the captain ordered his crew conducting a rescue simulation... that was more real than the British thought. This maneuver, which the English soldiers agreed as they believed it would serve to further delay the departure of the Umbria. While the Italians occupied the lifeboats, the chief engineers, following Muiesan´s orders, opened all the valves and drown the ship to the bottom of the reef. With the crew safe, the British only had time to get on their ship and watch the freighter slid slowly.

When the captain of HMS Grimsby asked why he had done that Muiesan confirmed the declaration of war from Italy to Britain. The next day Muiesan and the rest of Umbria crew departed detainees to India, where they spent four years in prison.

  

CARGO:

The Umbria was carrying 360,000 individual aircraft bombs ranging in size from 15, 50 and 100 kg. The vessel also carried a large quantity of fuses, ammunition and detonators as well as other traditional cargo. The captain knew these bombs would be confiscated and used by the enemy against his country should they ever discover them which was why he made the call to sink the ship.

The Umbria had sailed in June 1940 with 6,000 tons of bombs, 60 boxes detonators, explosives, weapons and three Fiat 1100 Lunga from Genoa via Livorno and Naples in the Suez Canal and on the way via Massaua and Assab to Calcutta.

Working a service from Gothenburg to Copenhagen, SJ X2000 93-74-302 stands at the buffers under the incredible Malmö train station prior to reversing out and heading towards the Danish capital over the Øresund Bridge.

 

Often considered the train that saved Swedish Railways, the X2000, also known as the X2, was launched in 1990 by Kalmar Verkstad in Kalmar, Sweden (prior to the company being bought by Adtranz in 1996). The X2000, and its top speed of 130mph in service (though technically capable of 176mph), massively reduced journey times and increased service efficiency throughout the mid-1990's, its effects on Swedish Railways and its passenger numbers being similar to that of the HST here in the UK.

 

The X2000 design goes back to the mid-1980's, and, in similar fashion to the Pendolino of Italy, took much of its innovation from the failure of the British Advanced Passenger Train (APT). Following the cancellation of the APT in 1986, much of the information and technology developed was taken up by Italy, who pioneered the first revenue earning tilting-train in 1987 with the ETR 450.

 

The success of the ETR 450 meant that SJ, who at the time were suffering from very slow and somewhat unreliable services on the country's very winding railway network, could also take up their design innovation to help redress the balance. During the period of the X2000's construction, the Swedish Government desired something home-built, and were reluctant to buy Pendolino's from Italy. Thus the contract for building the X2000 sets was given to Kalmar Verkstad.

 

The X2000 was launched in 1990 as an entirely first-class train working the premier route between Stockholm and Gothenburg, and immediately had a pronounced effect on the railway services. However, all was not well with the X2000, due largely to some electrical infidelity. As such, widespread distribution of the sets was not completed until at least 1995, after which second-class was also made available so as to help recoup the lost train's lost profits.

 

Production ended in 1996 following the purchase of Kalmar Verkstad by German rail transport equipment manufacturer Adtranz. Today the sets have been distributed heavily around Sweden, even operating international services to Copenhagen. However, the X2000 became a failure of its own success in some respects, especially with the increased ridership on SJ trains. As popularity of train travel rose in the 2000's, not only did capacity aboard the trains become an issue, the capacity on the railways themselves was becoming problematic, with journey times becoming longer and delays being incurred. This issue was rectified in 2008 with the order of the Bombardier X55 Regina high-speed units that have helped compliment the X2000's on their long distance services.

 

The X2000 however has not just been limited to Sweden, they've also made ventures to international railways with mixed amounts of success.

 

The first county to take interest in the X2000 was interestingly enough the United States, as, in the 1990's, Amtrak decided to modernise the high speed Northeast Corridor service between Boston, New York, Philadelphia and Washington D.C. The option was also made for diesel variants to operate on non-electrified services around the USA, especially higher-capacity services around California or to the north of New York towards Albany and Buffalo, with the X2000 set being dragged around 48 states by pairs of F40 locomotives.

 

The set was tested between October 1992 and January 1993, together with a more traditional ICE set from Germany, with both sets being compared for their operational efficiency and increased performance. Though a good contender for Amtrak services, the X2000's electrical faults sadly put it out of the running. Eventually Amtrak would choose the Acela sets built by Bombardier in 2000.

 

In 1995, three X2000 cars were hired by Australian operator CountryLink for evaluation purposes, being one driving trailer, one bistro car and one first class car. The trains were towed in a push/pull operation by modified XPT power cars XP2000 and XP2009 with the tilt equipment deactivated. After conducting a statewide of New South Wales tour in March 1995, they were used on Canberra services from April 1995 until June 1995.

 

China also purchased a X2000 train named "Xinshisu" (New Speed). The train served as Guangzhou-Kowloon Through Train on the Guangshen Railway from 1998 until 2007. It was delivered to Sichuan Province in August 2007. However, due to the 2008 Sichuan earthquake, Chengdu Railway Bureau needed to rebuild the railway networks in Sichuan Province. Also, the authority could not carry the maintenance costs of the train. It was therefore returned to Guangshen Railway Company in late December 2008. In 2012 the train was purchased by SJ and was shipped back to Sweden.

 

Nevertheless, the X2000 has proven itself a well performing and capable set of trains, working hard and bringing the Swedish Railways back from the edge. In a similar fashion to the HST of Britain, the X2000 has become the face of SJ, and one hopes that these magnificent trains can see many years of future service.

Aeroscopia est un musée aéronautique français implanté à Blagnac (Haute-Garonne), près du site AéroConstellation, et accueille notamment deux exemplaires du Concorde, dont l'ouverture a eu lieu le 14 janvier 2015

 

Le tarmac Sud du musée n'est capable d'accueillir que trois gros appareils. L'installation des appareils fut définitivement terminée après que le premier prototype de l'A400M-180 y fut arrivé le 16 juillet 2015, en dépit de la possibilité de 360 000 euros de TVA.

 

Concorde, F-BVFC, MSN209 aux couleurs d'Air France

Caravelle 12, F-BTOE, MSN280 aux couleurs d'Air Inter, dernier exemplaire construit

A400M-180, F-WWMT, MSN001 stationné depuis le 16 juillet 2015

 

La réalisation en 2019 du nouveau tarmac au Nord du musée permet l'accueil d'appareils supplémentaires issus des entreprises locales Airbus et ATR. Le transfert des avions entre le site Airbus "Lagardère" et le musée a lieu sur une semaine, à raison d'un appareil par jour :

 

ATR 72-600, F-WWEY, MSN098 aux couleurs d'ATR, transféré sur site le 26 août 2019, premier exemplaire du 72 dans sa version 600

Airbus A340-600, F-WWCA, MSN360 aux couleurs d'Airbus, transféré sur site le 27 août 2019, premier exemplaire de l'A340 dans sa version 600

Airbus A320-111, F-WWAI, MSN001 aux anciennes couleurs d'Airbus, transféré sur site le 28 août 2019, premier exemplaire de l'A320 : inauguration le 14 février 1987 en présence de Lady Diana et du Prince Charles, premier vol le 22 février 1987

Airbus A380-800, F-WXXL, MSN002 aux couleurs d'Airbus, transféré sur site le 29 août 2019, second exemplaire de l'A380. Les deux ponts de cet appareil sont visitables, ainsi que le cockpit.

ATR 42-300, F-WEGC, MSN003 aux anciennes couleurs d'ATR, transféré sur site le 30 août 2019, troisième exemplaire du 42. Cet exemplaire est décoré aux couleurs du MSN001 et porte l'immatriculation F-WEGA

 

Concorde, F-WTSB, MSN201 (ANAE), il s'agit d'un appareil de présérie qui a servi entre autres à transporter plusieurs présidents de la République française.

Airbus A300B4-203, F-WUAB, MSN238 (Airbus Heritage), décoré aux couleurs du prototype, au lieu de MSN001 démantelé. L'intérieur est visitable. Dans la première section des vitrages transparents permettent de voir la structure et les systèmes de l'avion, tandis que dans les sections suivantes sont représentés des aménagements de première classe et VIP.

Super Guppy de l'association Ailes Anciennes Toulouse, l'appareil qui servait au transport des tronçons d'Airbus est exposé porte ouverte, et une passerelle permet l'accès à la soute où un film est projeté. L'ouverture n'a pas été une mince affaire, l'appareil n'ayant pas été ouvert pendant 15 ans. L'aide des anciens mécaniciens de l'avion a été primordiale pour permettre une ouverture en toute sécurité.

 

Corvette (Airbus)

Falcon 10 no 02, prototype ayant servi aux essais du turboréacteur Larzac (Ailes Anciennes Toulouse)

Fouga Magister (AAT)

Gazelle prototype (AAT)

Mirage III C (AAT)

Nord 1100 (AAT)

Lockheed F-104G (AAT)

MiG-15 (AAT)

MS.760 Paris (AAT)

Vought F-8E(FN) Crusader et son réacteur (AAT)

Alouette II Marine (AAT)

Cessna Skymaster (AAT)

Fairchild Metro, ancien avion de Météo-France (AAT)

HM-293, de Rodolphe Grunberg

Chagnes MicroStar, avion de construction amateur, version biréacteur de Rutan VariViggen (AAT)

Saab J35OE Draken (AAT)

 

Aeroscopia is a French aeronautical museum located in Blagnac (Haute-Garonne), near the AéroConstellation site, and notably hosts two copies of the Concorde, which opened on January 14, 2015

 

The south tarmac of the museum can only accommodate three large aircraft. The installation of the devices was definitively finished after the first prototype of the A400M-180 arrived there on July 16, 2015, despite the possibility of 360,000 euros in VAT.

 

Concorde, F-BVFC, MSN209 in Air France colors

Caravelle 12, F-BTOE, MSN280 in Air Inter colors, last model built

A400M-180, F-WWMT, MSN001 parked since July 16, 2015

 

The construction in 2019 of the new tarmac north of the museum will accommodate additional aircraft from local Airbus and ATR companies. The transfer of planes between the Airbus "Lagardère" site and the museum takes place over a week, at the rate of one aircraft per day:

 

ATR 72-600, F-WWEY, MSN098 in ATR colors, transferred to site on August 26, 2019, first copy of the 72 in its 600 version

Airbus A340-600, F-WWCA, MSN360 in Airbus colors, transferred to site on August 27, 2019, first copy of the A340 in its 600 version

Airbus A320-111, F-WWAI, MSN001 in the old Airbus colors, transferred to site on August 28, 2019, first copy of the A320: inauguration on February 14, 1987 in the presence of Lady Diana and Prince Charles, first flight on February 22, 1987

Airbus A380-800, F-WXXL, MSN002 in Airbus colors, transferred to site on August 29, 2019, second copy of the A380. The two decks of this aircraft can be visited, as well as the cockpit.

ATR 42-300, F-WEGC, MSN003 in the old ATR colors, transferred to the site on August 30, 2019, third specimen of the 42. This specimen is decorated in the colors of the MSN001 and bears the registration F-WEGA

 

Concorde, F-WTSB, MSN201 (ANAE), this is a pre-production aircraft which was used, among other things, to transport several presidents of the French Republic.

Airbus A300B4-203, F-WUAB, MSN238 (Airbus Heritage), decorated in the colors of the prototype, instead of dismantled MSN001. The interior can be visited. In the first section transparent glazing allows to see the structure and systems of the aircraft, while in the following sections are shown first class and VIP fittings.

Super Guppy from the Ailes Anciennes Toulouse association, the aircraft which was used to transport the Airbus sections is on display with the door open, and a gangway allows access to the hold where a film is shown. Opening was no small feat, as the device has not been opened for 15 years. The help of the former mechanics of the aircraft was essential to allow a safe opening.

 

Corvette (Airbus)

Falcon 10 no 02, prototype used for testing the Larzac turbojet engine (Ailes Anciennes Toulouse)

Fouga Magister (AAT)

Prototype Gazelle (AAT)

Mirage III C (AAT)

North 1100 (AAT)

Lockheed F-104G (AAT)

MiG-15 (AAT)

MS.760 Paris (AAT)

Vought F-8E (FN) Crusader and its engine (AAT)

Alouette II Marine (AAT)

Cessna Skymaster (AAT)

Fairchild Metro, former Météo-France (AAT) aircraft

HM-293, by Rodolphe Grunberg

Chagnes MicroStar, amateur-built aircraft, twin-jet version of Rutan VariViggen (AAT)

Saab J35OE Draken (AAT)

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based historical facts. BEWARE!

 

Some background:

The Mikoyan-Gurevich MiG-19 (NATO reporting name: "Farmer") was a Soviet second-generation, single-seat, twin jet-engine fighter aircraft. It was the first Soviet production aircraft capable of supersonic speeds in level flight. A comparable U.S. "Century Series" fighter was the North American F-100 Super Sabre, although the MiG-19 would primarily oppose the more modern McDonnell Douglas F-4 Phantom II and Republic F-105 Thunderchief over North Vietnam. Furthermore, the North American YF-100 Super Sabre prototype appeared approximately one year after the MiG-19, making the MiG-19 the first operational supersonic jet in the world.

 

On 20 April 1951, OKB-155 was given the order to develop the MiG-17 into a new fighter called "I-340", also known as "SM-1". It was to be powered by two Mikulin AM-5 non-afterburning jet engines, a scaled-down version of the Mikulin AM-3, with 19.6 kN (4,410 lbf) of thrust. The I-340 was supposed to attain 1,160 km/h (725 mph, Mach 0.97) at 2,000 m (6,562 ft), 1,080 km/h (675 mph, Mach 1.0) at 10,000 m (32,808 ft), climb to 10,000 m (32,808 ft) in 2.9 minutes, and have a service ceiling of no less than 17,500 m (57,415 ft).

After several prototypes with many detail improvements, the ministers of the Soviet Union issued the order #286-133 to start serial production on February 17, 1954, at the factories in Gorkiy and Novosibirsk. Factory trials were completed on September 12 the same year, and government trials started on September 30.

 

Initial enthusiasm for the aircraft was dampened by several problems. The most alarming of these was the danger of a midair explosion due to overheating of the fuselage fuel tanks located between the engines. Deployment of airbrakes at high speeds caused a high-g pitch-up. Elevators lacked authority at supersonic speeds. The high landing speed of 230 km/h (145 mph), compared to 160 km/h (100 mph) for the MiG-15, combined with the lack of a two-seat trainer version, slowed pilot transition to the type. Handling problems were addressed with the second prototype, "SM-9/2", which added a third ventral airbrake and introduced all-moving tailplanes with a damper to prevent pilot-induced oscillations at subsonic speeds. It flew on 16 September 1954, and entered production as the MiG-19S.

 

Approximately 5,500 MiG-19's were produced, first in the USSR and in Czechoslovakia as the Avia S-105, but mainly in the People's Republic of China as the Shenyang J-6. The aircraft saw service with a number of other national air forces, including those of Cuba, North Vietnam, Egypt, Pakistan, and North Korea. The aircraft saw combat during the Vietnam War, the 1967 Six Day War, and the 1971 Bangladesh War.

 

However, jet fighter development made huge leaps in the 1960s, and OKB MiG was constantly trying to improve the MiG-19's performance, esp. against fast and high-flying enemies, primarily bombers but also spy planes like the U-2.

 

As the MiG-19S was brought into service with the Soviet air forces in mid-1956, the OKB MiG was continuing the refinement of the SM-1/I-340 fighter. One of these evolutionary paths was the SM-12 (literally, “SM-1, second generation”) family of prototypes, the ultimate extrapolation of the basic MiG-19 design, which eventually led to the MiG-19bis interceptor that filled the gap between the MiG-19S and the following, highly successful MiG-21.

 

The SM-12 first saw life as an exercise in drag reduction by means of new air intake configurations, since the MiG-19’s original intake with rounded lips became inefficient at supersonic speed (its Western rival, the North American F-100, featured a sharp-lipped nose air intake from the start). The first of three prototypes, the SM-12/1, was essentially a MiG-19S with an extended and straight-tapered nose with sharp-lipped orifice and a pointed, two-position shock cone on the intake splitter. The simple arrangement proved to be successful and was further refined.

 

The next evolutionary step, the SM-12/3, differed from its predecessors primarily in two new R3-26 turbojets developed from the earlier power plant by V. N. Sorokin. These each offered an afterburning thrust of 3,600kg, enabling the SM-12/3 to attain speeds ranging between 1,430km/h at sea level, or Mach=1.16, and 1,930km/h at 12,000m, or Mach=1.8, and an altitude of between 17,500 and 18,000m during its test program. This outstanding performance prompted further development with a view to production as a point defense interceptor.

 

Similarly powered by R3-26 engines, and embodying major nose redesign with a larger orifice permitting introduction of a substantial two-position conical centerbody for a TsD-30 radar, a further prototype was completed as the SM-12PM. Discarding the wing root NR-30 cannon of preceding prototypes, the SM-12PM was armed with only two K-5M (RS-2U) beam-riding missiles and entered flight test in 1957. This configuration would become the basis for the MiG-19bis interceptor that eventually was ordered into limited production (see below).

 

However, the SM-12 development line did not stop at this point. At the end of 1958, yet another prototype, the SM-12PMU, joined the experimental fighter family. This had R3M-26 turbojets uprated to 3.800kg with afterburning, but these were further augmented by a U-19D accelerator, which took the form of a permanent ventral pack containing an RU-013 rocket motor and its propellant tanks. Developed by D. D. Sevruk, the RU-013 delivered 3,000kg of additional thrust, and with the aid of this rocket motor, the SM-12PMU attained an altitude of 24,000m and a speed of Mach=1.69. But this effort was to no avail: the decision had been taken meanwhile to manufacture the Ye-7 in series as the MiG-21, and further development of the SM-12 series was therefore discontinued.

 

Nevertheless, since full operational status of the new MiG-21 was expected to remain pending for some time, production of a modified SM-12PM was ordered as a gap filler. Not only would this fighter bridge the performance gap to the Mach 2-capable MiG-21, it also had the benefit of being based on proven technologies and would not require a new basic pilot training.

 

The new aircraft received the official designation MiG-19bis. Compared with the SM-12PM prototype, the MiG-19bis differed in some details and improvements. The SM-12PM’s most significant shortfall was its short range – at full power, it had only a range of 750 km! This could be mended through an additional fuel tank in an enlarged dorsal fairing behind the cockpit. With this internal extra fuel, range could be extended by a further 200 - 250km range, but drop tanks had typically to be carried, too, in order to extend the fighter’ combat radius with two AAMs to 500 km. Specifically for the MiG-19bis, new, supersonic drop tanks (PTB-490) were designed, and these were later adapted for the MiG-21, too.

 

The air intake shock cone was re-contoured and the shifting mechanism improved: Instead of a simple, conical shape, the shock cone now had a more complex curvature with two steps and the intake orifice area was widened to allow a higher airflow rate. The air intake’s efficiency was further optimized through gradual positions of the shock cone.

As a positive side effect, the revised shock cone offered space for an enlarged radar dish, what improved detection range and resolution. The TsD-30 radar for the fighter’s missile-only armament was retained, even though the K-5’s effective range of only 2–6 km (1¼ – 3¾ mi) made it only suitable against slow and large targets like bombers. All guns were deleted in order to save weight or make room for the electronic equipment. The tail section was also changed because the R3M-26 engines and their afterburners were considerably longer than the MiG-19's original RM-5 engines. The exhausts now markedly protruded from the tail section, and the original, characteristic pen nib fairing between the two engines had been modified accordingly.

 

Production started in 1960, but only a total of roundabout 180 MiG-19bis, which received the NATO code "Farmer F", were built and the Soviet Union remained the only operator of the type. The first aircraft entered Soviet Anti-Air Defense in early 1961, and the machines were concentrated in PVO interceptor units around major sites like Moscow, Sewastopol at the Black Sea and Vladivostok in the Far East.

 

With the advent of the MiG-21, though, their career did not last long. Even though many machines were updated to carry the K-13 (the IR-guided AA-2 "Atoll") as well as the improved K-55 AAMs, with no change of the type’s designation, most MiG-19bis were already phased out towards the late 1960s and quickly replaced by 2nd generation MiG-21s as well as heavier and more capable Suchoj interceptors like the Su-9, -11 and -15. By 1972, all MiG-19bis had been retired.

  

General characteristics:

Crew: 1

Length: 13.54 m (44 ft 4 in), fuselage only with shock cone in forward position

15.48 m (50 8 ½ in) including pitot

Wingspan: 9 m (29 ft 6 in)

Height: 3.8885 m (12 ft 9 in)

Wing area: 25 m² (269 ft²)

Empty weight: 5,210 kg (11,475 lb)

Loaded weight: 7,890 kg (17,380 lb)

Max. takeoff weight: 9,050 kg (19,935 lb)

Fuel capacity: 2,450 l (556 imp gal; 647 US gal) internal;

plus 760 l (170 imp gal; 200 US gal) with 2 drop tanks

 

Powerplant:

2× Sorokin R3M-26 turbojets, rated at 37.2 kN (8,370 lbf) thrust each with afterburning

 

Performance:

Maximum speed: 1,380km/h at sea level (Mach=1.16)

1,850km/h at 12,000m (Mach=1.8)

Range: 1,250 km (775 mi; 750 nmi) at 14,000 m (45,000 ft) with 2 × 490 l drop tanks

Combat range: 500 km (312 mi; 270 nmi)

Ferry range: 2,000 km (1,242 mi; 690 nmi)

Service ceiling: 19,750 m (64,690 ft)

Rate of climb: 180 m/s (35,000 ft/min)

Wing loading: 353.3 kg/m² (72.4 lb/ft²)

Thrust/weight: 0.86

 

Armament:

No internal guns.

4× underwing pylons; typically, a pair of PTB-490 drop tanks were carried on the outer pylon pair,

plus a pair of air-to air missiles on the inner pair: initially two radar-guided Kaliningrad K-5M (RS-2US)

AAMs, later two radar-guided K-55 or IR-guided Vympel K-13 (AA-2 'Atoll') AAMs

  

The kit and its assembly:

Another submission for the 2018 Cold War Group Build at whatifmodelers.com, and again the opportunity to build a whiffy model from the project list. But it’s as fictional as one might think, since the SM-12 line of experimental “hybrid” fighters between the MiG-19 and the MiG-21 was real. But none of these aircraft ever made it into serial production, and in real life the MiG-21 showed so much potential that the attempts to improve the MiG-19 were stopped and no operational fighter entered production or service.

 

However, the SM-12, with its elongated nose and the central shock cone, makes a nice model subject, and I imagined what a service aircraft might have looked like? It would IMHO have been close, if not identical, to the SM-12PM, since this was the most refined pure jet fighter in the development family.

 

The basis for the build was a (dead cheap) Mastercraft MiG-19, which is a re-edition of the venerable Kovozávody Prostějov (KP) kit – as a tribute to modern tastes, it comes with (crudely) engraved panel, but it has a horrible fit all over. For instance, there was a 1mm gap between the fuselage and the right wing, the wing halves’ outlines did not match at all and it is questionable if the canopy actually belongs to the kit at all? PSR everywhere. I also had a Plastyk version of this kit on the table some time ago, but it was of a much better quality! O.K., the Mastercraft kit comes cheap, but it’s, to be honest, not a real bargain.

 

Even though the result would not be crisp I did some mods and changes. Internally, a cockpit tub was implanted (OOB there’s just a wacky seat hanging in mid air) plus some serious lead weight in the nose section for a proper stance.

On the outside, the new air intake is the most obvious change. I found a Su-17 intake (from a Mastercraft kit, too) and used a piece from a Matchbox B-17G’s dorsal turret to elongate the nose – it had an almost perfect diameter and a mildly conical shape. Some massive PSR work was necessary to blend the parts together, though.

The tail received new jet nozzles, scratched from steel needle protection covers, and the tail fairing was adjusted according to the real SM-12’s shape.

 

Ordnance was adapted, too: the drop tanks come from a Mastercraft MiG-21, and these supersonic PTB-490 tanks were indeed carried by the real SM-12 prototypes because the uprated engines were very thirsty and the original, teardrop-shaped MiG-19 tanks simply too draggy for the much faster SM-12. As a side note, the real SM-12’s short range was one of the serious factors that prevented the promising type’s production in real life. In order to overcome the poor range weakness I added an enlarged spine (half of a drop tank), inspired by the MiG-21 SMT, that would house an additional internal fuel tank.

 

The R2-SU/K-5 AAMs come from a vintage Mastercraft Soviet aircraft weapon set, which carries a pair of these 1st generation AAMs. While the molds seem to be a bit soft, the missiles look pretty convincing. Their pylons were taken from the kit (OOB they carry unguided AAM pods and are placed behind the main landing gear wells), just reversed and placed on the wings’ leading edges – similar to the real SM-12’s arrangement.

  

Painting and markings:

No surprises. In the Sixties, any PVO aircraft was left in bare metal, so there was hardly an alternative to a NMF finish.

 

Painting started with an all-over coat with acrylic Revell 99 (Aluminum), just the spine tank became light grey (Revell 371) for some contrast, and I painted some di-electric covers in a deep green (Revell 48).

The cockpit interior was painted with a bright mix of Revell 55 and some 48, while the landing gear wells and the back section of the cockpit were painted in a bluish grey (Revell 57).

The landing gear was painted in Steel (unpolished Modelmaster metallizer) and received classic, bright green wheel discs (Humbrol 2). As a small, unusual highlight the pitot boom under the chin received red and white stripes – seen on occasional MiG-19S fighters in Soviet service, and the anti-flutter booms on the stabilizers became bright red, too.

 

After the basic painting was done the kit received a black ink wash. Once this had dried and wiped off with a soft cotton cloth, post shading with various metallizer tones was added in order to liven up the uniform aircraft (including Humbrol’s matt and polished aluminum, and the exhaust section was treated with steel). Some panel lines were emphasized with a thin pencil.

 

Decals were puzzled together from various sources, a Guards badge and a few Russian stencils were added, too. Finally, the kit was sealed with a coat of sheen acrylic varnish (a 2:1 mix of Italeri matt and semi-gloss varnish).

 

The K-5 missiles, last but not least, were painted in aluminum, too, but their end caps (both front and tail section) became off-white.

  

The Mastercraft kit on which this conversion was based is crude, so I did not have high expectations concerning the outcome. But the new nose blends nicely into the MiG-19 fuselage, and the wide spine is a subtle detail that makes the aircraft look more “beefy” and less MiG-19-ish. The different drop tanks – even though they are authentic – visually add further speed. And despite many flaws, I am quite happy with the result of roundabout a week’s work.

DISCLAIMER

Nothing you see here is real, even though the conversion or the presented background story might be based historical facts. BEWARE!

 

The Indian HAL HG-30 Bāja (‘Hawk’) had been designed and manufactured by Hindustan Aeronautics Ltd. in the early 60ies, when it became clear that the Indian Air Force was left without a capable and rather simple aircraft for these roles - the “jet age” had been in full development, but fast and large aircraft like the Su-7 or Hawker Hunter were just not suited for low-altitude missions against day and night visible ground targets in a broad area.

 

Indian military planners assumed that potential aggressor will first disable airfields, so the Bāja was designed to take-off from short unprepared runways, and it was readily available to be loaded with weapons and supplied through a flexible system of auxiliary airfields that required no special preparations, especially in mountainous regions.

 

The resulting HG-30 Bāja was a light, single-engine, low-wing single-seat aircraft with a metal airframe, capable of performing close air support, counter insurgency (COIN), and reconnaissance missions. The type featured a license-built Rolls Royce Dart turboprop engine and a reinforced, retractable tricycle landing gear for operations on rugged terrain. The unpressurized cockpit was placed as far forward and high as possible, offering the pilot an excellent view. The ejection seat was armored and the cockpit lined with nylon flak curtains.

The first HG-30 prototype flew in February 1962, and a total of 89 examples of the Bāja were built between 1963 and 1965, including two pre-production aircraft. These introduced some improvements like fixed wingtip tanks, a bulged canopy which improved the rear view or self-sealing and foam-filled fuselage tanks.

 

Armament consisted of four fixed 20mm cannons in the wings, plus unguided missiles, unguided bombs or napalm tanks under the wings and the fuselage on a total of 11 hardpoints. The inner pair under the wings as well as the centerline pylon were able to carry 1.000 lbs each and were ‘wet’ for optional drop tanks. The next pair could carry 500 lbs each, and the outer six attachment points were reserved for missile rails or single bombs of up to 200 lbs caliber. A total external ordnance load of up to 4.500 lbs could be carried, even though this was rarely practiced since it severely hampered handling.

 

The Bāja was exclusively used by the Indian Air Force, serving with 3rd (‘Cobras’) and 5th (‘Tuskers’) Squadrons in the Eastern and Western regions, alongside Toofani and Ajeet fighter bombers. Even though there was some foreign interest (e .g. from Israel and Yugoslavia,) no export sales came to fruition.

A tandem-seated trainer version was envisaged, but never left the drawing board, since Hindustan had already developed the HJT-16 Kiran jet trainer for the IAF which was more suitable, esp. with its side-by-side cockpit. Even a maritime version with foldable outer wings, arresting hook and structural reinforcements was considered for the Indian Navy.

 

The HG-30 did not make it in time into service for the five-week Indo-Pakistani war of 1965, but later saw serious action in the course of the Bangladesh Liberation War and the ensuing next clash between India and Pakistan in December 1971, when all aircraft (originally delivered in a natural metal finish) quickly received improvised camouflage schemes.

 

The 1971 campaign settled down to series of daylight anti-airfield, anti-radar and close-support attacks by fighters, with night attacks against airfields and strategic targets, into which the HG-30s were heavily involved. Sporadic raids by the IAF continued against Pakistan's forward air bases in the West until the end of the war, and large scale interdiction and close-support operations were maintained.

The HG-30 excelled at close air support. Its straight wings allowed it to engage targets 150 MPH slower than swept-wing jet fighters. This slower speed improved shooting and bombing accuracy, enabling pilots to achieve an average accuracy of less than 40 feet, and the turboprop engine offered a much better fuel consumption than the jet engines of that era.

While it was not a fast aircraft and its pilots were a bit looked down upon by their jet pilot colleagues, the HG-30 was well liked by its crews because of its agility, stability at low speed, ease of service under field conditions and the crucial ability to absorb a lot of punishment with its rigid and simple structure.

 

After the 1971 conflict the Bāja served with the IAF without any further warfare duty until 1993, when, after the loss of about two dozen aircraft due to enemy fire and (only three) accidents, the type was completely retired and its COIN duties taken over by Mi-25 and Mi-35 helicopters, which had been gradually introduced into IAF service since 1984.

  

General characteristics

Crew: 1

Length: 10.23 m (33 ft 6¼ in)

Wingspan: 12.38 m (40 ft 7¼ in) incl. wing tip tanks

Height: 3.95 m (12 ft 11¼ in)

Empty weight: 7,689 lb (3,488 kg)

Max. take-off weight: Loaded weight: 11,652 lb (5,285 kg)

 

Powerplant:

1× Rolls Royce Dart RDa.7 turboprop engine, with 1.815 ehp (1.354 kW)/1.630 shp (1.220 kW) at 15,000 rpm

 

Performance

Maximum speed: 469 mph (755 km/h) at sea level and in clean configuration

Stall speed: 88 km/h (48 knots 55 mph)

Service ceiling: 34,000 ft (10,363 m)

Rate of climb: 5,020 ft/min (25.5 m/s)

Range: 1,385 miles (2,228 km) at max. take-off weight

 

Armament:

4× 20mm cannons (2 per wing) with 250 RPG

A total of 11 underwing and fuselage hardpoints with a capacity of 4.500 lbs (2.034 kg); provisions to carry combinations of general purpose or cluster bombs, machine gun pods, unguided missiles, air-to-ground rocket pods, fuel drop tanks, and napalm tanks.

     

The kit and its assembly

This fictional COIN aircraft came to be when I stumbled across the vintage Heller Breguet Alizé kit in 1:100 scale. I did some math and came to the conclusion that the kit would make a pretty plausible single-seat propeller aircraft in 1:72...

 

Finding a story and a potential user was more of a challenge. I finally settled on India – not only because the country had and has a potent aircraft industry, a COIN aircraft (apart from obsolete WWII types) would have matched well into the IAF in the early 70ies. Brazil was another manufacturer candidate – but then I had the vision of Indian Su-7 and their unique camouflage scheme, and this was what the kit was to evolve to! Muahahah!

 

What started as a simple adaptation idea turned into a true Frankenstein job, because only little was left from the Heller Alizé – the kit is SO crappy…

 

What was thrown into the mix:

• Fuselage, rudder and front wheel doors from the Heller Alizé

• Horizontal stabilizers from an Airfix P-51 Mustang

• Wings are the outer parts from an Airfix Fw 189, clipped and with new landing gear wells

• Landing gear comes from a Hobby Boss F-86, the main wheels from the scrap box

• Cockpit tub comes from a Heller Alpha Jet, seat and pilot from the scrap box

• The canopy comes from a Hobby Boss F4U Corsair

• Ordnance hardpoints were cut from styrene strips

• Propeller consists of a spinner from a Matchbox Mitsubishi Zero and blades from two AH-1 tail rotors

• Ordnance was puzzled together from the scrap box; the six retarder bombs appeared appropriate, the four missile pods were built from Matchbox parts. The wingtip tanks are streamlines 1.000 lbs bombs.

 

The only major sculpting work was done around the nose, in order to make the bigger propeller fiat and to simulate an appropriate air intake for the engine. Overall this thing looks pretty goofy, rather jet-like, with the slightly swept wings. On the other side, the Bāja does not look bad at all, and it has that “Small man’s A-10” aura to it.

 

Putting the parts together only posed two trouble zones: the canopy and the wings. The Corsair canopy would more or less fit, getting it in place and shaping the spine intersection was more demanding than expected. Still not perfect, but this was a “quick and dirty” project with a poor basis, anyway, so I don’t bother much.

Another tricky thing were the wings and getting them on the fuselage. That the Fw 189 wings ended up here has a reason: the original kit provided two pairs of upper wing halves, the lower halves were lacking! Here these obsolete parts finally found a good use, even though the resulting wing is pretty thick and called for some serious putty work on the belly side… Anyway, this was still easier than trying to modify the Alizé wings into something useful, and a thick wing ain’t bad for low altitude and bigger external loads.

  

Painting and markings

As mentioned before, the garish paint scheme is inspired by IAF Su-7 fighter bombers during/after the India-Pakistani confrontation of 1971. It’s almost surreal, reason enough to use it. Since a 1:72 Su-7 takes up so much shelf space I was happy to find this smaller aircraft as a suitable placebo.

 

I used Su-7 pictures as benchmarks, and settled for the following enamels as basic tones for the upper grey, brown and green:

• Humbrol 176 (Neutral Grey, out of production), for a dull and bluish medium grey

• Testors 1583 (Rubber), a very dark, reddish brown

• Humbrol 114 (Russian Green, out of production)

 

For the lower sides I used Testors 2123 (Russian Underside Blue). The kit received a black ink wash and some dry painting for weathering/more depth. Judging real life aircraft pics of IAF Su-7 and MiG-21, the original underside tone is hardly different from the upper blue grey and it seems on some aircraft as if the upper tone had been wrapped around. The aircraft do not appear very uniform at all, anyway.

 

Together with the bright IAF roundels the result looks a bit as if that thing had been designed by 6 year old, but the livery has its charm - the thing looks VERY unique! The roundels come from a generic TL Modellbau aftermarket sheet, the tactical codes are single white letters from the same manufacturer. Other stencils, warning signs and the squadron emblem come from the scrap box – Indian aircraft tend to look rather bleak and purposeful, except when wearing war game markings...

   

In the end, a small and quick project. The model was assembled in just two days, basic painting done on the third day and decals plus some weathering and detail work on the forth – including pics. A new record, even though this one was not built for perfectionism, rather as a recycling kit with lots of stock material at hand. But overall the Bāja looks exotic and somehow quite convincing?

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based on historical facts. BEWARE!

  

Some background:

The Saab 35 Draken ('The Kite' or 'The Dragon') was a Swedish fighter-interceptor developed and manufactured by Svenska Aeroplan Aktiebolaget (SAAB) between 1955 and 1974. Development of the Saab 35 Draken started in 1948 as the Swedish air force future replacement for the then also in development Saab 29 Tunnan dayfighter and Saab 32B Lansen night fighter. It featured an innovative but unproven double delta wing, which led to the creation of a sub-scale test aircraft, the Saab 210, which was produced and flown to test this previously unexplored aerodynamic feature. The full-scale production version entered service with frontline squadrons of the Swedish Air Force on 8 March 1960. It received the designation Flygplan 35 (Fpl 35; 'Aeroplane 35') and was produced in several variants and types, most commonly as a fighter type with the prefix J (J 35), standing for Jaktflygplan (Pursuit-aircraft), the Swedish term for fighter aircraft.

 

The Saab 35 Draken was known for, among other things, its many "firsts" within aviation. It was the first Western European-built combat aircraft with true supersonic capability to enter service and the first fully supersonic aircraft to be deployed in Western Europe. Design-wise it was one of, if not the first, combat aircraft designed with double delta wings, being drawn up by early 1950. The unconventional wing design also had the side effect of making it the first known aircraft to perform and be capable of the Cobra maneuver. It was also one of the first Western-European-built aircraft to exceed Mach 2 in level flight, reaching it on 14 January 1960.

 

The Draken functioned as an effective supersonic fighter aircraft of the Cold War period. Even though the type was designed and intended as an interceptor, the Draken was considered to be a very capable dogfighter for the era, and its large wing area allowed the compact Saab 35 to carry a relatively high payload, too. In Swedish service, it underwent several upgrades, the ultimate of these being the J 35 J model which served until 1999. The Draken was also exported to several countries and remained operational in Austria until 2005.

 

In Swedish service, the Saab 35 was replaced by the Saab 37 “Viggen”. Development work on the new type was already initiated at Saab in 1952 and, following the selection of a radical canard delta wing configuration, the resulting aircraft performed its first flight on 8 February 1967 and entered service on 21 June 1971. However, being a radical and new design, the service introduction of the Viggen – esp. of its initial version, the AJ 37 fighter-bomber – was not without teething troubles, and in the late Sixties the Swedish Air Force expected an attack aircraft gap in its line-up. The former A 32 A Lansen attack aircraft were reaching the end of their airframe lifetime and were simply outdated, even though it was still needed as an anti-ship attack platform for the indigenous Rb 04 guided missile, so that Saab suggested an interim solution: the conversion of seventy of the 120 produced J 35 D fighters into dedicated attack aircraft, with the designation A 35 G (Gustav).

 

The Saab A 35 G was heavily modified to make it into a fighter bomber aircraft. Compared to the fighter versions the outer wings where completely redesigned and the aircraft featured 9 hardpoints in total. Airframe and landing gear were strengthened to cope with an increased payload of 10,000 lb (4,540 kg) vs. the fighters’ usual 6,393 lb (2,900 kg). Several airframe components were restored or replaced to extend the life of the aircraft, and the landing gear featured low-pressure tires for a better field performance on improvised/dispersed airfields.

A wide array of ordnance could be carried, such as bombs of up to 1.000 lb (454 kg) caliber, MERs with up to six 100 kg (220 lb) bombs each, pods with unguided 75 mm or 135 mm rockets, single 14.5 cm psrak m49/56 high-explosive anti-tank rockets and, as a new weapon, the indigenous guided Rb 05 air-to-ground missile. This had been developed for the AJ 37 "Viggen in 1967 and was roughly comparable with the American AGM-12 Bullpup, but had some unique features. The Rb 05’s supersonic speed was deemed necessary to reduce the threat of surface-to-air missiles, and it allowed the missile to be deployed against slow/large aerial targets, too, making it a dual-purpose weapon. Consequently, the Rb 05’s fuze could be set by the pilot to impact mode for ground targets, or proximity mode for attacking air targets such as bombers.

The missile had a maximum range of 9 km (5.6 ml) and would usually be launched after a high-speed attack run on very low altitude and a climb to 400m for launch. Since the RB 05 was roll-stabilized, the aircraft did not need to be aimed straight at the target when launching and could immediately descend into terrain cover again, and this also made it possible to attack aerial targets from unusual angles and flight paths. Tracking the flares on the missile, the pilot would then visually guide the missile (the missile's engine was smokeless as to not obscure the view) with a small manual joystick towards the target. Guidance commands were transmitted to the missile via a jam-proof radio transmission link.

 

The A 35 G kept the J 35 D’s two 30 mm ADEN cannons, and a limited air defense capability was retained, too: the Gustav could carry up to four IR-guided Rb 24 (AIM-9B Sidewinder) AAMs, in addition to the Rb 05 in air-to-air mode. However, the aircraft lacked any air intercept radar, and had instead a Ferranti LRMTS (laser rangefinder and marked target seeker) and a counterweight installed in the nose, which resembled the S 35 E photo reconnaissance version’s nose, just without the windows for the side-looking cameras. For its attack role, the A 35 G received a new inertial navigation system, new altimeters and a ballistic computer from Saab called BT-9Rm, which worked with both bombs and rockets and even allowed for toss bombing. The Gustav Draken was furthermore fitted with electronic countermeasure (ECM) systems, a RHAWS and chaff and flare dispensers in their tail cones to improve its survivability over the battlefield.

 

The Gustav conversion program was accepted by the Swedish government in 1968. Work started in early 1969, the first revamped aircraft reached the operational units in late 1971. However, since production of the AJ 37 was starting at the same time, only 61 aircraft were eventually re-built from existing J 35 D airframes (one prototype and sixty production aircraft). Västgöta Wing (F 6) at Karlsborg was the first squadron to receive the A 35 G, replacing its A 32 A fighter bombers, the other unit to operate the type was Skaraborg Wing (F 7) at Såtenäs.

 

Among Sweden’s Draken fleet the Gustav was easy to recognize because it was the only version that carried the new “Fields & Meadows” splinter camouflage as standard livery. Service of the A 35 G lasted only until the early Eighties, though: as more and more AJ 37 all-weather fighter bombers reached the Swedish frontline units during the Seventies, the interim attack Draken, which was only effective under daylight and more or less good weather conditions, was withdrawn and either used for spares in the running J 35 J modernization program or directly scrapped, because many airframes had, suffering from the special stress of low-level flight operations, reached the end of their lifespan.

 

Another factor for the quick withdrawal was the disappointing performance of the type’s primary weapon, the Rb 05 missile: Its manual joystick steering in the cramped Draken cockpit (to be operated while the pilot was expected to fly at low altitude and evade enemy fire!) presented a number of problems, and the Rb 05’s ultimate accuracy was, even under ideal conditions, on the order of just 10 meters (33 ft), greater than desired. Targets like tanks or even ships were hard to hit with this level of scattering, combined with imminent danger for the pilot, and the air-to-air mode was even less effective. On the more modern Saab 37 the Rb 05 was therefore replaced by the Rb 75, a license-produced version of the American TV-guided AGM-65 Maverick “fire and forget” weapon. TV and laser seeker heads for the Rb 05 to improve the weapon’s accuracy and handling had been planned since the early Seventies, but were never realized.

  

General characteristics:

Crew: 1

Length: 15.35 m (50 ft 4 in)

Wingspan: 9.42 m (30 ft 11 in)

Height: 3.89 m (12 ft 9 in)

Wing area: 49.2 m² (530 ft²)

Airfoil: 5%

Empty weight: 8,175 kg (18,006 lb)

Gross weight: 11,500 kg (25,330 lb)

Max takeoff weight: 13,554 kg (29,845 lb)

 

Powerplant:

1× Svenska Flygmotor RM6C (license-built Rolls Royce Avon with Swedish EBK67 afterburner)

turbojet engine, 56.5 kN (12,700 lbf) thrust dry, 77.3 kN (17,240 lbf) with afterburner

 

Performance:

Maximum speed: 2,150 km/h (1,335 mph, 1,168 kn) at 11,000 m (36,089 ft), clean

1,430 km/h (888 mph, 777 kn) w. two dop tanks and two 454 kg (1.00 lb) bombs

Range: 1.120 km (605 nmi; 696 mi); clean, internal fuel only

Ferry range: 2,750 km (1,480 nmi; 1,710 mi) with four external 500 l drop tanks

Service ceiling: 20,000 m (66,000 ft)

Rate of climb: 199 m/s (39,200 ft/min)

Wing loading: 231.6 kg/m² (47.4 lb/ft²)

Thrust/weight: 0.7

Takeoff roll: 800 m (2,625 ft)

 

Armament:

2× 30 mm akan m/55 ADEN cannon with 100 rounds per gun

9× hardpoints with a total capacity of 4,500 kg (10.000 lb)

  

The kit and its assembly:

Even though the model depicts a what-if aircraft, the Draken’s proposed “Gustav” attack variant based on the J 35 D interceptor was real – even though I could not find much detail information about it. So, I took some inspiration from the contemporary Danish Saab 35XD export version, which probably had similar features to the Gustav? Another inspiring factor was a pair of Rb 05 missiles (from an Airfix Viggen) that I had bought with a spare parts lot some time ago – and an attack Draken would be the perfect carrier for these exotic (and unsuccessful) missiles.

 

For a low-budget build I used one of Mistercraft’s many recent re-boxings of the vintage Revell Draken from 1957(!), and this kit is nothing for those who are faint at heart. It is horrible.

The kit probably depicts a late J 35 A (already with a long tail section), but even for this variant it lacks details like the air scoops for the afterburner or a proper landing gear. The Draken’s characteristic tail wheel is also missing completely. Worst pitfall, however: there is NO interior at all, not even a lumpy seat! The canopy, the early model with struts, is disturbingly clean and crisp, though. The overall fit is mediocre at best, too – there are only a few visible seams, but any of them calls for filling and PSR. It’s a very toyish kit, even though the general outlines are O.K.

And the Mistercraft instructions are really audacious: they show all the parts that are actually NOT there at all. Suddenly a seat appears in the cockpit, a fin fairing from a J 35 D or later, or the tail wheel… And the decal sheets only roughly meet the aircraft you see in the painting instructions - there are three sheets, totally puzzled together, including material for aircraft not mentioned in the instructions, but that’s a common feature of most Mistercraft kits. But: how much can you taunt your disappointed customers?

 

So, this leaves lots of room for improvements, and calls for a lot of scratching and improvisation, too. First measure was to open both the air intakes (which end after 2mm in vertical walls) and the exhaust, which received an afterburner dummy deep inside to create depth. Next, I implanted a complete cockpit, consisting of s scratched dashboard (styrene sheet), the tub from an Italeri Bae Hawk trainer’s rear cockpit (which comes with neat side consoles and fits quite well) plus a shallow vintage ejection seat, probably left over from an early MiG from a KP kit or one of its many later reincarnations. As an alternative, there’s a Quickboost resin aftermarket set with a complete cockpit interior (even including side walls, IIRC intended to be used with the Hasegawa Draken) available but using it on this crappy kit would have been a waste of resources – it’s more expensive than the kit itself, and even with a fine cockpit the exterior would still remain sh!t.

 

Since I could not find any detail about the Gustav Draken’s equipment I gave it a laser rangefinder in a poor-fitting S 35 E (or is it a Danish export F-35?) nose that comes as an optional part with the vintage Revell mold – which is weird, because the recce Draken was built between 1963 and 1968 in 2 series, several years after the kit’s launch? Maybe the Mistercraft kit is based on the 1989 Revell re-boxing? But that kit also features an all-in-one pilot/seat part and a two-piece canopy… Weird!

 

Once the hull was closed many surface details had to be added. The afterburner air scoops were created from plastic profiles, which are aftermarket roof rails in H0 scale. Styrene profile material was also used to create the intakes behind the cockpit, better than nothing. The OOB pitot on the fin was very robust, and since it would be wrong on a J 35 D I cut it off and added a fairing to the fin tip, a shortened/modified ACMI pod, which bears a better pitot alternative at its tip. The pitot on the nose was scratched from heated styrene, since the kit offers no part at all.

 

Under the rear fuselage the whole tail wheel arrangement had to be scratched. The shallow fairing consists of a section from a Matchbox EA-6B drop tank, the wheel and its strut were tinkered together with bits from the scrap box and profile material. Not stellar, but better than OOB (= nothing!).

The landing gear struts were taken from the kit but beefed up with some details. The main wheels had to be replaced, the new ones come from a KP MiG-21, IIRC.

 

The ordnance consists of a pair of Rb 05’s from an Airfix Viggen, a pair of OOB drop tanks and MERs from a Matchbox A-7D, together with fourteen streamlined bombs from the same kit – twelve on the MERs and single bombs on the outer pylons. AFAIK, Sweden never used MERs on their aircraft, but the bombs come pretty close to some small bombs that I have seen as AJ 37 ordnance. Most pylons are OOB, I just added a single ventral station and two outer hardpoints under the wings. The Rb 05s received a prominent place under the air intakes on Sidewinder launch rails.

  

Painting and markings:

Finally a good excuse to apply the famous and complex “Fields & Meadows” paint scheme to a Draken model! However, this “combo” actually existed in real life, but only on a single aircraft: around 1980 a J 35 B (s/n 35520), aircraft “20” of F18, was painted in this fashion, but AFAIK it was only an instructional airframe. You find some pictures of this aircraft online but getting a clear three-side view (esp. from above!) as a reliable painting benchmark is impossible. However, a complete paint scheme of this aircraft is provided with one of Mistercraft’s Revell Draken re-boxings (not the one I bought, though), even though it is mismarked as a J 35 F of F10 in the instructions. One of the common Mistercraft errors, err, “surprises” (*sigh*).

 

Finding suitable model paints for the elaborate scheme is not easy, either, and after having applied it several times I stuck to my favorites: Humbrol 150 (Forest Green, FS 34127), 75 (Bronze Green), 118 (US Light Tan, FS 30219, a bit light but RAF Dark Earth is too somber) and Revell 06 (Tar Black, RAL 9021) on the upper surfaces and Humbrol 247 (RLM76) underneath.

A large ventral section was, typical for the J 35, left in bare metal, since leaking fuel and oil would frequently eat away any paint there. The section was painted with Revell 91 (Iron) and later treated with Matt Aluminum Metallizer (Humbrol). As per usual, the model received an overall light black ink washing and some post-shading in order to emphasize the panels, correct the splinter camouflage and dramatize the surface. Some extra weathering was done around the gun ports and the jet nozzle with graphite.

 

Internal details like the cockpit and the landing gear were painted with the help of Swedish Saab 35 reference pictures. The cockpit tub was painted in a dark, bluish green (Humbrol 76) with grey-green (Revell 67) side walls.

The landing gear and its respective wells were painted in a bluish grey (Revell 57), parts of the struts were painted in a bright turquoise (a mix of Humbrol 89 and 80; looks quite weird, but I like such details!). The wheel hubs became medium grey (Revell 47). The Rb 05 missiles were painted in white as live weapons, so that they stand out well from the airframe. The drop tanks received the same blue-grey as the underside (Humbrol 247). MERs and launch rails were painted in a neutral grey (RAL 7001) and the bombs became olive drab (RAL 6014, Gelboliv) with yellow rings and golden fuzes.

 

Decals/markings were puzzled together from a Moose Republic Saab 32 sheet (unit code number and emblem) and the spares box, including the red tactical tail code from an Italeri 1:72 Gripen and roundels from a Hasegawa Draken. Stencils were taken from the kit’s OOB sheet and also from the Hasegawa Draken sheet. Finally, the model was sealed with matt acrylic varnish (Italeri).

  

What a horror trip! The paint scheme itself was/is challenging enough, but modding the crappy vintage Revell kit into something more presentable was already a fight in itself. However, I like the outcome. “Fields & Meadows” suits the Draken with its huge and flat upper surface well, and while the Gustav conversion did not take much effort the “mud mover” ordnance under this Mach 2 fighter really looks strange and makes you wonder what this is. A nice what-if model, despite its blurriness!

Monteagle TN

Airmen assigned to the 114th Civil Engineer Squadron practice shoot, move, communicate drills during October's Unit Training Assembly as part of the Multi-Capable Airman (MCA) concept. The training consisted of convoy operations, movement techniques with weapons, integrated base defense and land navigation as a way to cultivate a more self-sustaining squadron. (U.S. Air National Guard photo by Staff Sgt. Jorrie Hart)

The American MGR-1 Honest John Rocket was the first Nuclear-Capable Surface-to-Surface Rocket in their arsenal, it was originally designated ''Artillery Rocket XM31'' the first unit was tested on 29th June 1951, with the first production rounds delivered in January 1953. Its designation was changed to ''M31'' in September 1953. The first Army Units received their Rockets by year's end and Honest John Battalions were deployed in Europe in early 1954. Alternatively, the Rocket was capable of carrying an ordinary High-Explosive Warhead weighing 1,500lb.

 

Developed at Redstone Arsenal, Alabama, the Honest John was a large but simple fin-stabilised, unguided Artillery Rocket weighing 5,820lb in its initial M31 Nuclear-Armed version. Mounted on the back of a truck, the Rocket was aimed in much the same way as a Cannon and then fired up an elevated ramp, igniting four small spin rockets as it cleared the end of the ramp. The M31 had a range of 15.4 miles with a 20 kiloton Nuclear Warhead and was also capable of carrying a 1,500lb Conventional Warhead.

 

The M31 system included a truck-mounted, unguided, Solid-Fueled Rocket transported in three separate parts, the Honest John was assembled in the field before launch, mounted on an M289 Launcher, and aimed and fired in about 5 minutes. The Rocket was originally outfitted with a W7 Nuclear Warhead, with a variable yield of up to 20 kilotons of TNT in 1959, a W31 Warhead with three variants was deployed with yields of 2, 10 or 30 Kilotons. There was a W31 variant of 20 Kilotons used exclusively for the Nike Hercules Anti-Aircraft System. The M31 had a range between 3.4 and 15.4 miles.

 

Early tests exhibited more scatter on target than was acceptable when carrying conventional payloads. Development of an upgraded Honest John, M50, was undertaken to improve accuracy and extend range. The size of the fins was greatly reduced to eliminate weathercocking. Increased spin was applied to restore the positive stability margin that was lost when fin size was reduced. The improved M50, with the smaller fins and more ''rifiling'' had a maximum range of 30+ miles with a scatter on target of only 250 yards, demonstrating an accuracy approaching that of Tube Artillery. The Honest John was manufactured by the Douglas Aircraft Company of Santa Monica, California.

 

In the 1960's, Sarin Nerve Gas Cluster Munitions were also available, designed to be interchangeable for use with either the Honest John or MGM-5 Corporal. Initially the M79 (E19R1) GB Cluster Warhead, containing 356 M134 (E130R1) Bomblets for the M31A1C Honest John. The production model was the M190 (E19R2) GB Cluster Warhead, containing 356 M139 (E130R2) Bomblets when the M31A1C was phased out in favor of the XM50 Honest John. Under nominal conditions it had an mean area of effect of 0.347 square miles.

  

The two basic versions of Honest John were:-

 

**MGR-1A (M31) was 27ft 3in long, had an engine diameter of 22+7⁄8 in, a Warhead diameter of 30in, a fin span of 9ft 1in, weighed 5,820lb (nuclear) and had a range of 3.4 to 15.4 miles. The Hercules Powder Company M6 Solid-Fueled Rocket motor was 16ft 5+7⁄16 in long, weighed 3,937lb, and had 99,000 lbf thrust.

 

**MGR-1B (M50) was 26ft long, had an engine diameter of 22.8in, a Warhead diameter of 30in, a fin span of 4ft 6in, weighed 4,320lb (nuclear) and had a maximum range of 30 miles, practically twice that of the M31. An improved propellant formulation gave the Rocket motor 150,000 lbf thrust.

 

In late 1950, Major General Holger Toftoy was a Colonel overseeing the development of the Rocket. The project was in danger of cancellation "on the grounds that such a large Unguided Rocket could not possibly have had the accuracy to justify further funds." On a trip to the White Sands Missile Range, Toftoy met a Texan man who was prone to making unbelievable statements. Whenever anyone expressed doubt about the man's claims, he would respond, "Why, around these parts, I'm called ''Honest John !'" Because the project was being questioned, Toftoy felt that the nickname was appropriate for the Rocket and suggested the name to his superiors.

 

Specifications:-

 

▪︎Type: Nuclear-Capable Surface-to-Surface Rocket

▪︎Place of Origin: United States

▪︎In Service: 1953 to 1991

▪︎Used By: Belgium / Canada / Denmark / France / Germany / Greece / Italy / Netherlands / Norway / South Korea / Taiwan / Turkey / United Kingdom / United States

▪︎Conflicts: Cold War

▪︎Manufacturer: Douglas Aircraft Company

▪︎Number Built: 7000+

▪︎Variants: MGR-1A / MGR-1B / MGR-1C

▪︎Mass: MGR-1A - 5,820lb / Length: 27ft 3in / Diameter: 30in

▪︎Powerplant: Hercules M6 solid-fueled rocket, 99,000 lbf

▪︎Wingspan: 9ft 1in

▪︎Propellant: Double base solid propellant

▪︎Operational Range: 3.4 to 15.4 miles

▪︎Flight Ceiling: 30,000ft

▪︎Maximum Speed: Mach 2.3.

 

Extracts taken from Wikipedia en.m.wikipedia.org/wiki/MGR-1_Honest_John

After Adolf Hitler took power in Germany in 1933, the nation’s secret rearmament after World War I could come out into the open. The Luftwaffe quickly announced a competition for a single-seat point defense interceptor, able to reach 250 mph at 20,000 feet, be capable of reaching 15,000 feet in 17 minutes or less, and have heavy cannon armament. Production aircraft would need to use either the Junkers Jumo 210 or Daimler-Benz 600 series inline piston engines.

 

Arado, Heinkel, and the Bayerische Flugzeugwerke, headed by its chief designer Willy Messerschmitt, all submitted entries. The Ar 80 was rejected, but both Heinkel’s He 112 and BFW’s Bf 109 were highly competitive. To ensure he had enough aircraft for the competition, Messerschmitt’s first Bf 109V1s were equipped with borrowed Rolls-Royce Kestrel engines. During the competition, it looked as if the He 112 would win it: the Bf 109 was disliked by test pilots because of poor visibility forward on the ground, unreliable narrow-track landing gear, sideways-closing canopy, and heaviness on the controls. However, the Bf 109 was lighter and cheaper than the He 112, and it had better maneuverability, thanks to the then novel inclusion of leading-edge slats; it was also faster. The Reich Air Ministry chose the Bf 109, noting that Messerschmitt needed to put it in full production as soon as possible: the British were testing a similar high-performance fighter, the Supermarine Spitfire.

 

Initially, production Bf 109s (from the A through D variants) used the less powerful Jumo engine. These aircraft provided valuable experience in the type, however: several Bf 109Ds were deployed with the German “volunteer” Condor Legion during the Spanish Civil War, where it proved to be superior to anything in either the Spanish Republican or Nationalist air forces. By the beginning of World War II in September 1939, however, the majority of German fighter units had been equipped with the Daimler-Benz DB 601 powered Bf 109E, which was an even better aircraft with plenty of power. “Emils” obliterated the obsolescent air forces of Poland, Norway, and the Low Countries, and did well against more contemporary aircraft such as the Hawker Hurricane and Dewoltine D.520 over France. Only against the Spitfire, which the Bf 109 met for the first time during the Dunkirk evacuation, did it meet its match.

 

This was to continue during the Battle of Britain. German pilots such as Werner Molders and Adolf Galland learned that the Spitfire could turn inside the Bf 109, but that their fighter was better in the vertical; the only limit to the Bf 109’s performance was its lack of range, which limited it to 15 minutes combat time over England—the 109 simply was never designed as an escort fighter. Pilots liked the stable gun platform of the Bf 109, which concentrated its main armament in the nose, consisting of two machine guns in the cowl and a single cannon firing through the propeller hub.

 

Messerschmitt listened to Battle of Britain veterans and produced the Bf 109F, which was more aerodynamically clean, as it eliminated tailplane bracing and the wing cannon, which had been added before the Battle of France but impacted the 109’s manueverability. The “Fritz” was the equal of the Spitfire and superior to the P-40 Warhawk, which it began to fight in North Africa in early 1941, and far and away better than anything the Soviet Air Force could field when Hitler invaded Russia in June 1941. German veteran pilots began to rack up incredible kill ratios, with Molders and Galland topping the 100 mark in early 1941; Hans-Joachim Marseille would clear the 150 kill mark by 1942.

 

Yet the situation in Europe changed, and changed too rapidly for Messerschmitt to truly react. By 1943, when the Bf 109G was introduced, the tide was beginning to turn; by 1944, when 109 production hit its peak, the fighter was clearly outclassed by newer Allied fighters. The Bf 109 was not as manueverable as the P-51 Mustang and was outlcassed above 15,000 feet by the P-47 Thunderbolt; on the Eastern Front, the Russians began fielding the powerful Lavochkin La-5 and the nimble Yakovlev Yak-3. German pilot quality kept the Bf 109 very competitive in the East, where several Luftwaffe pilots now surpassed the 200 victory mark, but in the West, where Allied pilots were every bit as good as their German counterparts, attrition began to set in. German pilot training could not keep up with losses, and German pilot quality began to degrade; worse, the Bf 109 simply could not be improved any further.

 

By 1944, the 109 was obsolete and hunted down by American fighters ranging all over the shrinking Reich: even the best pilot could do little when he was attacked the moment he took off by P-51s superior to his aircraft and in far greater numbers. The “Gustav” had introduced the more powerful DB 605 engine, which had needed so many adaptations and cooling vents that the Bf 109G was referred to by pilots as the “pickle”: the Bf 109K returned to a more aerodynamic finish, but the “Kara” was obsolete before it entered service. Luftwaffe pilots and RLM officials had wanted Messerschmitt to end Bf 109 production in favor of the jet-powered Me 262, but this was not practical due to the lack of jet engines; Willy Messerschmitt himself also distrusted the new technology and kept the 109 in production far longer than it should have been. Whatever the case, the Bf 109 was still in production when its factories were destroyed or overrun in 1945.

 

Despite its shortcomings—more 109s were destroyed in landing accidents on the Eastern Front than by Russian fighters—it had proven a deadly opponent. Over a hundred Luftwaffe pilots scored more than a hundred kills in the aircraft; a few, such as Molders, Galland, and Marseille had done so against Allied pilots their equal in skill and training. On the Eastern Front, the numbers became truly ridiculous: between the two of them, Gerhard Barkhorn and Erich Hartmann destroyed 653 Soviet aircraft alone. Kill ratios against the Soviets were as high as 25 to 1. Bf 109s were also flown by the top ace of Finland, Ilmari Juutilainen, and Romania, Alexandru Serbanescu; it was also briefly flown by Italy’s top ace, Adriano Visconti.

 

After the end of World War II, most surviving Bf 109s were scrapped by the victorious Allies, but it remained in limited production in Czechslovakia, as the Avia S.199, and in Spain, as the Hispano HA-1112 Buchon. Due to a lack of Daimler-Benz engines, the S.199 was equipped with later model Jumo engines, which impacted their performance, leading Czech pilots to call them “Mules.” Ironically, they would be supplied to the nascent Israeli Air Force as the Sherut Avir’s first operational fighter, where they were used effectively. Buchons, refitted with Rolls-Royce Merlin engines, those used by the Bf 109’s principal foes, would stay in Spanish service until 1967. 33,984 Bf 109s were produced during World War II, making it the most widely produced fighter in history. Today, only 70 remain, with a mere seven original or restored examples airworthy.

 

This Bf 109E-3 at the Museum of Flight in Seattle, Washington was originally built as a Bf 109 in Germany, supplied to Spain before the end of the war, then rebuilt as a Rolls-Royce Merlin Hispano HA.1112. It was bought by warbird collector Douglas Champlin in 1972 and rebuilt again, back to more or less Bf 109E standard, though it uses a later Daimler-Benz engine, as the originals were unavailable by that time. Like the rest of Champlin's collection, it went to the Museum of Flight around 2006. Today, it is displayed as Hans "Assi" Hahn's Bf 109E-3, as it appeared during the Battle of Britain. Hahn, who finished the war with 108 kills (58 of them Spitfires), flew with JG 2 ("Richthofen"); the yellow cowling and tail stripe were for recognition purposes, but it led to several Luftwaffe units being nicknamed "Yellow-Nosed Bastards" or the "Boys from Abbeville" from their base in France.

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based historical facts. BEWARE!

  

Some background:

The Sondergerät SG104 "Münchhausen" was a German airborne recoillless 355.6 mm (14-inch) caliber gun, intended to engage even the roughest enemy battleships, primarily those of the Royal Navy. The design of this unusual and massive weapon began in 1939. The rationale behind it was that a battleship’s most vulnerable part was the deck – a flat surface, with relatively thin armor (as typical hits were expected on the flanks) and ideally with vital targets underneath, so that a single, good hit would cripple of even destroy a ship. The purpose of such a high angle of attack was likely to allow the projectile to penetrate the target ship's deck, where the ship's armor, if there was any, would have been much thinner than the armor on its sidesHowever, hitting the deck properly with another ship’s main gun was not easy, since it could only be affected through indirect hits and the typical angle of the attack from aballistic shot would not necessarily be ideal for deep penetration, esp. at long range.

The solution to this problem: ensure that the heavy projectile would hit its target directly from above, ideally at a very steep angle. To achieve this, the gun with battleship caliber was “relocated” from a carrier ship or a coastal battery onto an aircraft – specifically to a type that was capable of dive-bombing, a feature that almost any German bomber model of the time offered.

 

Firing such a heavy weapon caused a lot fo problems, which were severe even if the gun was mounted on a ship or on land. To compensate for such a large-caliber gun’s recoil and to make firing a 14 in shell (which alone weighed around almost 700 kg/1.550 lb, plus the charge) from a relatively light airframe feasible, the respective gun had to be as light as possible and avoid any recoil, which would easily tear an aircraft – even a bomber – apart upon firing. Therefore, the Gerät 104 was designed as a recoilless cannon. Its firing system involved venting the same amount of the weapon's propellant gas for its round to the rear of the launch tube (which was open at both ends), in the same fashion as a rocket launcher. This created a forward directed momentum which was nearly equal to the rearward momentum (recoil) imparted to the system by accelerating the projectile itself. The balance thus created did not leave much net momentum to be imparted to the weapon's mounting or the carrying airframe in the form of felt recoil. A further share of the recoil induced by the moving round itself could be compensated by a muzzle brake which re-directed a part of the firing gases backwards. Since recoil had been mostly negated, a heavy and complex recoil damping mechanism was not necessary – even though the weapon itself was huge and heavy.

 

Work on the "Münchhausen" device (a secret project handle after a fictional German nobleman created by the German writer Rudolf Erich Raspe in the late 18th century who reputedly had ridden on a cannonball between enemy frontlines), was done by Rheinmetall-Borsig and lasted until 1941. The first test of a prototype weapon was conducted on 9th of September 1940 in Unterlüss with a satisfactory result, even though the weapon was only mounted onto an open rack and not integrated into an airframe yet. At that time, potential carriers were the Ju 88, the Dornier Do 217 and the new Junkers Ju 288. Even though the system’s efficacy was doubted, the prospect of delivering a single, fatal blow to an important , armored arget superseded any doubts at the RLM, and the project was greenlit in early 1942 for the next stage: the integration of the Sondergerät 104 into an existing airframe. The Ju 88 and its successor, the Ju 188, turned out to be too light and lacked carrying capacity for the complete, loaded weapon, and the favored Ju 288 was never produced, so that only the Dornier Do 217 or the bigger He 177 remained as a suitable carriers. The Do 217 was eventually chosen because it had the biggest payload and the airframe was proven and readily available.

 

After calculations had verified that the designed 14 in rifle would have effectively no recoil, preliminary tests with dumm airframes were carried out. After ground trials with a Do 217 E day bomber to check recoil and blast effects on the airframe, the development and production of a limited Nullserie (pre-production series) of the dedicated Do 217 F variant for field tests and eventual operational use against British sea and land targets was ordered in April 1942.

 

The resulting Do 217 F-0 was based on the late “E” bomber variant and powered by a pair of BMW 801 radial engines. It was, however, heavily modified for its unique weapon and the highly specialized mission profile: upon arriving at the zone of operation at high altitude, the aircraft would initiate a dive with an angle of attack between 50° and 80° from the horizontal, firing the SG 104 at an altitude between 6,000 and 2,000 meters. The flight time of the projectile could range from 16.0 seconds for a shot from an altitude of 6,000 meters at a 50° angle to just 4.4 seconds for a shot from 2.000 meters at an almost vertical 80° angle. Muzzle velocity of the SG 104 was only 300 m/s, but, prior to impact, the effective velocity of the projectile was projected to range between 449 and 468 m/s (1,616 to 1,674 km/h). Together with the round's weight of roughly 700 kg (1.550 lb) and a hardened tip, this would still ensure a high penetration potential.

 

The operational Sondergerät 104 had an empty mass of 2.780 kg (6,123 lb) and its complete 14 inch double cartridge weighed around 1.600 kg (3,525 lb). The loaded mass of the weapon was 4,237 kg, stretching the limits of the Do 217’s load capacity to the maximum, so that some armor and less vital pieces of equipment were deleted. Crew and defensive armament were reduced to a minimum.

Even though there had been plans to integrate the wepaon into the airframe (on the Ju 288), the Gerät 104 was on the Do 217 F-0 mounted externally and occupied the whole space under the aircraft, precluding any use of the bomb bay. The latter was occupied by the Gerät 104’s complex mount, which extended to the outside under a streamlined fairing and held the weapon at a distance from the airframe. Between the mount’s struts inside of the fuselage, an additional fuel tank for balance reasons was added, too.

The gun’s center, where the heavy round was carried, was positioned under the aircraft’s center of gravity, so that the gun barrel markedly protruded from under the aircraft’s nose. To make enough space, the Do 217 Es bomb aimer’s ventral gondola and his rearward-facing defensive position under the cockpit were omitted and faired over. The nose section was also totally different: the original extensive glazing (the so-called “Kampfkopf”) was replaced by a smaller, conventional canopy, similar to the later Do 217 J and N night fighter versions, together with a solid nose - the original glass panels would have easily shattered upon firing the gun, esp. in a steep high-speed dive. A "Lotfernrohr" bomb aiming device was still installed in a streamlined and protected fairing, though, so that the navigator could guide the pilot during the approach to the target and during the attack run.

To stabilize the heavy aircraft during its attack and to time- and safely pull out of the dive, a massive mechanical dive brake was mounted at the extended tail tip, which unfolded with four "petals". A charecteristic stabilizing dorsal strake was added between the twin fins, too.

 

The ventral area behind the gun’s rear-facing muzzle received additional metal plating and blast guiding vanes, after trials in late 1940 had revealed that firing the SG 104 could easily damage the Do 217’s tail structure, esp. all of the tail surfaces’ rudders and the fins’ lower ends in particular. Due to all this extra weight, the Do 217 F-0’s defensive armament consisted only of a single 13 mm MG 131 machine gun in a manually operated dorsal position behind the cockpit cabin, which offered space for a crew of three. A fixed 15 mm MG 151 autocannon was mounted in the nose, too, a weapon with a long barrel for extended range and accuracy. It was not an offensive weapon, though, rather intended as an aiming aid for the SG 104 because it was loaded with tracer bullets: during the final phase of the attack dive, the pilot kept firing the MG 151, and the bullet trail showed if he was on target to fire the SG 104 when the right altitude/range had been reached.

 

The first Do 217 F-0 was flown and tested in late 1943, and after some detail changes the type was cleared for a limited production run of ten aircraft in January 1944. The first operational machine was delivered to a dedicated testing commando, the Erprobungskommando 104 “Münchhausen”, also known as “Sonderkommando Münchhausen” or simply “E-Staffel 104”. The unit was based at Bordeaux/Merignac and directly attached to the KG 40's as a staff flight. At that time, KG 40 operated Do 217 and He 177 bombers and frequently flew reconnaissance and anti-shipping missions over the Atlantic west of France, up to the British west and southern coast, equipped with experimental Henschel Hs 293 glide bombs.

 

Initial flights confirmed that the Do 217 airframe was burdened with the SG 104 to its limits, the already rather sluggish aircraft (the Do 217 had generally a high wing loading and was not easy to fly) lost anything that was left of what could be called agility. It needed an experienced pilot to handle it safely, esp. during start and landing. It is no wonder that two Do 217 F-0s suffered ground accidents during the first two weeks of operations, but the machines could be repaired, resume the test program and carry out attack missions.

However, during one of the first test shots with the weapon, one Do 217 F-0 lost its complete tail section though the gun blast, and the aircraft crashed into the Bay of Biscay, killing the complete crew.

 

On 4th or April 1944 the first "hot" attack against an enemy ship was executed in the Celtic Sea off of Brest, against a convoy of 20 ships homeward bound from Gibraltar. The attack was not successful, though, the shot missing its target, and the German bomber was attacked and heavily damaged by British Bristol Beaufighters that had been deployed to protect the ships. The Do 217F-0 eventually crashed and sank into the Atlantic before it could reach land again.

 

A couple of days later, on 10th of April, the first attempt to attack and destroy a land target was undertaken: two Do 217 F-0s took off to attack Bouldnor Battery, an armored British artillery position located on the Isle of Wight. One machine had to abort the attack due to oil leakages, the second Do 217 F-0 eventually reached its target and made a shallow attack run, but heavy fog obscured the location and the otherwise successful shot missed the fortification. Upon return to its home base the aircraft was intercepted by RAF fighters over the Channel and heavily damaged, even though German fighters deployed from France came to the rescue, fought the British attackers off and escorted the limping Do 217 F-0 back to its home base.

 

These events revealed that the overall SG 104 concept was generally feasible, but also showed that the Do 217 F-0 was very vulnerable without air superiority or a suitable escort, so that new tactics had to be developed. One consequence was that further Do 217 F-0 deployments were now supported by V/KG 40, the Luftwaffe's only long range maritime fighter unit. These escorts consisted of Junkers Ju 88C-6s, which were capable of keeping up with the Do 217 F-0 and fend of intercepting RAF Coastal Command’s Beaufighters and later also Mosquitos.

 

In the meantime, tests with the SG 104 progressed and several modifications were tested on different EKdo 104's Do 217 F-0s. One major upgrade was a further strengthening of the tail section, which added another 200 kg (440 lb) to the aircraft's dry weight. Furthermore, at least three aircraft were outfitted with additional dive brakes under the outer wings, so that the dive could be better controlled and intercepted. these aircraft, however, lost their plumbed underwing hardpoints, but these were only ever used for drop tanks during transfer flights - a loaded SG 104 precluded any other ordnance. On two other aircraft the SG 104 was modified to test different muzzle brakes and deflectors for the rear-facing opening, so that the gun blast was more effectively guided away from the airframe to prevent instability and structural damage. For instance, one machine was equipped with a bifurcated blast deflector that directed the rearward gasses partly sideways, away from the fuselage.

 

These tests did not last long, though. During the Allied Normandy landings in June 1944 E-Staffel 104 was hastily thrown into action and made several poorly-prepared attack runs against Allied support ships. The biggest success was a full hit and the resulting sinking of the Norwegian destroyer HNoMS Svenner (G03) by "1A+BA" at dawn on 6th of June, off Sword, one of the Allied landing zones. Other targets were engaged, too, but only with little effect. This involvement, however, led to the loss of three Do 217 F-0s within just two days and four more heavily damaged aircraft – leaving only two of EKdo 104's Do 217 F-0s operational.

 

With the Allied invasion of France and a worsening war condition, the SG 104 program was stopped in August 1944 and the idea of an airborne anti-ship gun axed in favor of more flexible guided weapons like the Hs 293 missile and the Fritz-X glide bomb. Plans for a further developed weapon with a three-round drum magazine were immediately stopped, also because there was no carrier aircraft in sight that could carry and deploy this complex 6.5 tons weapon. However, work on the SG 104 and the experience gained from EKdo 104's field tests were not in vain. The knowledge gathered from the Münchhausen program was directly used for the design of a wide range of other, smaller recoilless aircraft weapons, including the magnetically-triggered SG 113 "Förstersonde" anti-tank weapon or the lightweight SG 118 "Rohrblock" unguided air-to-air missile battery for the Heinkel He 162 "Volksjäger".

  

General characteristics:

Crew: 3 (pilot, navigator, radio operator/gunner)

Length: 20,73 m (67 ft 11 in) overall

18,93 m (62 ft 3/4 in) hull only

Wingspan: 19 m (62 ft 4 in)

Height: 4.97 m (16 ft 4 in)

Wing area: 57 m² (610 sq ft)

Empty weight: 9,065 kg (19,985 lb)

Empty equipped weight:10,950 kg (24,140 lb)

Max takeoff weight: 16,700 kg (36,817 lb)

Fuel capacity: 2,960 l (780 US gal; 650 imp gal) in fuselage tank and four wing tanks

 

Powerplant:

2× BMW 801D-2 14-cylinder air-cooled radial piston engines, delivering

1,300 kW (1,700 hp) each for take-off and 1,070 kW (1,440 hp) at 5,700 m (18,700 ft),

driving 3-bladed VDM constant-speed propellers

 

Performance:

Maximum speed: 475 km/h (295 mph, 256 kn) at sea level

560 km/h (350 mph; 300 kn) at 5,700 m (18,700 ft)

Cruise speed: 400 km/h (250 mph, 220 kn) with loaded Gerät 104 at optimum altitude

Range: 2,180 km (1,350 mi, 1,180 nmi) with maximum internal fuel

Ferry range: 2,500 km (1,600 mi, 1,300 nmi); unarmed, with auxiliary fuel tanks

Service ceiling: 7,370 m (24,180 ft) with loaded Gerät 104,

9,500 m (31,200 ft) after firing

Rate of climb: 3.5 m/s (690 ft/min)

Time to altitude: 1,000 m (3,300 ft) in 4 minutes 10 seconds

2,000 m (6,600 ft) in 8 minutes 20 seconds

6,100 m (20,000 ft) in 24 minutes 40 seconds

 

Armament:

1x 355.6 mm (14-inch) Sondergerät 104 recoilless gun with a single round in ventral position

1x 15 mm (0.787 in) MG 151 machine cannon with 200 rounds, fixed in the nose

1x 13 mm (0.512 in) MG 131 machine gun with 500 rounds, movable in dorsal position

Two underwing hardpoints for a 900 l drop tank each, but only used during unarmed ferry flights

  

The kit and its assembly:

This was another submission to the "Gunships" group build at whatifmodellers.com in late 2021, and inspiration struck when I realized that I had two Italeri Do 217 in The Stash - a bomber and a night fighter - that could be combined into a suitable (fictional) carrier for a Sondergerät 104. This mighty weapon actually existed and even reached the hardware/test stage - but it was never integrated into an airframe and tested in flight. But that's what this model is supposed to depict.

 

On the Do 217, the Sg 104 would have been carried externally under the fuselage, even though there had been plans to integrate this recoilless rifle into airframes, esp. into the Ju 288. Since the latter never made it into production, the Do 217 would have been the most logical alternative, also because it had the highest payload of all German bombers during WWII and probably the only aircraft capable of carrying and deploying the Münchhausen device, as the SG 104 was also known.

 

The fictional Do 217 F-0 is a kitbashing, using a Do 217 N fuselage, combined with the wings from a Do 217 K bomber, plus some modifications. What initially sounded like a simple plan soon turned into a improvisation mess: it took some time to realize that I had already donated the Do 217 K's BMW 801 engines to another project, an upgraded He 115... I did not want to use the nightfighter's more powerful DB 603s, and I was lucky to have an Italeri Ju 188 kit at hand which comes with optional BMW 801s and Jumo 211s. Transplanting these engines onto the Do 217's wings took some tailoring of the adapter plates, but was feasible. However, the BMW 801s from the Ju 188 kit have a flaw: they lack the engine's characteristic cooling fans... Another lucky find: I found two such parts in the scrap box, even though from different kits - one left over from another Italeri Do 217 K, the other one from what I assume is/was an Italeri 1:72 Fw 190 A/F. To make matters worse, one propeller from the Ju 188 kit was missing, so that I had to find a(nother) replacement. :-/

I eventually used something that looked like an 1:72 F6F Hellcat propeller, but I an not certain about this because I have never built this model...? With some trimming on the blades' trailing edges and other mods, the donor's overall look could be adapted to the Ju 188 benchmark. Both propellers were mounted on metal axis' so that they could also carry the cooling fans. Lots of work, but the result looks quite good.

 

The Do 217 N's hull lost the lower rear gunner position and its ventral gondola, which was faired over with a piece of styrene sheet. The pilot was taken OOB, the gunner in the rear position was replaced by a more blob-like crew member from the scrap box. The plan to add a navigator in the seat to the lower right of the pilot did not work out due to space shortage, but this figure would probably have been invisble, anyway.

All gun openings in the nose were filled and PSRed away, and a fairing for a bomb aiming device and a single gun (the barrel is a hollow steel needle) were added.

 

The SG 104 was scratched. Starting point was a white metal replacement barrel for an 1:35 ISU-152 SPG with a brass muzzle brake. However, after dry-fitting the barrel under the hull the barrel turned out to be much too wide, so that only the muzzal brake survived and the rest of the weapon was created from a buddy refueling pod (from an Italeri 1:72 Luftwaffe Tornado, because of its two conical ends) and protective plastic caps from medical canulas. To attach this creation to the hull I abused a conformal belly tank from a Matchbox Gloster Meteor night fighter and tailored it into a streamlined fairing. While this quite a Frankenstein creation, the overall dimensions match the real SG 104 prototype and its look well.

 

Other cosmetic modifications include a pair of underwing dive brakes, translanted from an Italeri 1:72 Ju 88 A-4 kit, an extended (scratched) tail "stinger" which resembles the real dive brake arrangement that was installed on some Do 217 E bombers, and I added blast deflector vanes and a dorsal stabilizer fin.

In order to provide the aircraft with enough ground clearance, the tail wheel was slightly extended. Thanks to the long tail stinger, this is not blatantly obvious.

  

Painting and markings:

This was not an easy choice, but as a kind of prototype I decided that the paint scheme should be rather conservative. However, German aircraft operating over the Atlantic tended to carry rather pale schemes, so that the standard pattern of RLM 70/71/65 (Dunkelgrün, Schwarzgrün and Hellblau) with a low waterline - typical for experimental types - would hardly be appropriate.

I eventually found a compromise on a He 177 bomber (coded 6N+BN) from 1944 that was operated by KG 100: this particular aircraft had a lightened upper camouflage - still a standard splinter scheme but consisting of RLM 71 and 02 (Dunkelgrün and Grau; I used Modelmaster 2081 and Humbrol 240), a combination that had been used on German fighters during the Battle of Britain when the standard colors turned out to be too dark for operations over the Channel. The aircraft also carried standard RLM 65 (or maybe the new RLM76) underneath (Humbrol 65) and on the fin, but with a very high and slightly wavy waterline. As a rather unusual feature, no typical camouflage mottles were carried on the flanks or the fin, giving the aircraft a very bleak and simple look.

 

Despite my fears that this might look rather boring I adapted this scheme for the Do 217 F-0, and once basic painting was completed I was rather pleased by the aircraft's look! As an aircraft operated at the Western front, no additional markings like fuselage bands were carried.

To set the SG 104 apart from the airframe, I painted the weapon's visible parts in RLM 66 (Schwarzgrau, Humbrol 67), because this tone was frequently used for machinery (including the interior surfaces of aircraft towards 1945).

RLM 02 was also used for the interior surfaces and the landing gear, even though I used a slightly different, lighter shade in form of Revell 45 (Helloliv).

 

A light black ink washing was applied and post-shading to emphasize panel lines. Most markings/decals came from a Begemot 1:72 He 11 sheet, including the unusual green tactical code - it belongs to a staff unit, a suitable marking for such an experimental aircraft. The green (Humbrol 2) was carried over to the tips of the propeller spinners. The unit's code "1A" is fictional, AFAIK this combination had never been used by the Luftwaffe.

The small unit badge was alucky find: it actually depicts the fictional Baron von Münchhausen riding on a cannonball, and it comes from an Academy 1:72 Me 163 kit and its respective sheet. The mission markings underneath, depicting two anti-ship missions plus a successful sinking, came from a TL Modellbau 1:72 scale sheet with generic German WWII victory markings.

 

After some soot stains around the engine exhaust and weapon muzzles had been added with graphite, the model was sealed with matt acrylic varnish and final details like position lights and wire antennae (from heated black plastic sprue material) were added.

  

Well, what started as a combination of two kits of the same kind with a simple huge pipe underneath turned out to be more demanding than expected. The (incomplete) replacement engines were quite a challenge, and body work on the hull (tail stinger, fairing for the SG 104 as well as the weapon itself) turned out to be more complex and extensive than initially thought of. The result looks quite convincing, also supported by the rather simple paint scheme which IMHO just "looks right" and very convincing. And the whole thing is probably the most direct representation of the inspiring "Gunship" theme!

 

860 bhp, 6,262 cc rear-mounted longitudinal 65-degree V-12 engine with Bosch Motronic ME7 electronic fuel injection, six-speed electro-hydraulic semi-automatic transmission, front and rear independent pushrod suspension with unequal length wishbones, coil-over springs, and manually adjustable telescopic shock absorbers, and four-wheel Brembo carbon-ceramic disc brakes. Wheelbase: 104.3 in.

 

•The first customer FXX produced

•Single ownership from new; used at only three Corse Clienti events

•Upgraded with the Evoluzione package by the factory

•One of Ferrari’s rarest and most exclusive automobiles; a track-day titan

  

The performance car industry was characterized in the mid-2000s by a supercar battle royale that raged between Europe’s most prestigious automotive manufacturers. Porsche’s Carrera GT, the Mercedes-Benz SLR McLaren , and the Ferrari Enzo were all vying to be crowned king of the supercars. All three were capable of speeds over 200 mph and 0–60 times in the low three-second range, and they looked like nothing else on the road. Nevertheless, only one could be the best, and most agreed that the Enzo was the undisputed champion. As the Enzo was produced in lower numbers than both the Carrera GT and SLR McLaren and it boasted incredible looks with startling performance, many believed it to be the top dog and a car that its company simply would not be able to top for quite some time.

 

However, Ferrari was not a company to rest on its laurels, and many within the company thought that there was still much that could be improved upon with the Enzo platform. During the summer of 2005, at private, invitation-only events throughout Europe and North America, Ferrari announced to a select few that it would be producing a special track-only car that would be available in limited production to its best customers. The purpose of this car would be to give Ferrari’s most loyal clients the opportunity to develop the next generation of road cars through unprecedented access to Ferrari’s newest automotive technology and engineers. This new car, based on the already-incredible Ferrari Enzo, would provide an insane amount of performance, with a top speed stated at 214 mph.

 

The FXX was formally announced a few months later in December 2005 at the Bologna Motor Show, and it garnered an incredible amount of attention from both the world’s motoring press and automotive enthusiasts alike. Only 38 examples would be produced, making it one of the rarest cars in the history of the company. For the lucky enthusiasts given a chance to own an FXX, it was almost considered to be a blessing, as they would be given the opportunity to work directly with the factory to help develop future cars bearing the Cavallino Rampante.

 

Unlike Ferrari’s successful and very well run Challenge Series, the FXX would be run under the Corse Clienti program. This program, equally successful in its own right, was responsible for providing factory support to clients with Formula One Ferraris, and it would play a similar role in the FXX Programme. This would be a non-competitive program, in which owners would be invited, along with their cars, to select events, where they would be able to drive their cars on the track at speed. Like the F1 Clienti program, the factory would provide owners with a team of technicians and engineers for mechanical support and to advise the drivers on how to achieve the best results with their car. These events allowed the owners to improve their driving abilities in a controlled environment through feedback from the industry’s best factory drivers and support staff. The cars would be serviced and maintained by the factory, and owners were even given the opportunity to store their cars at Ferraris facilities in Maranello if they so desired, leaving the company in charge of transporting the cars to and from events.

 

The FXX presented here, chassis number 145369, was the very first FXX produced. It was ordered new by its first and current owner at the announcement of the program, and at that time, it was established that he would receive the first example built by the factory. Following its delivery, the car has only been used in three Corse Clienti events, at the inaugural FXX event at Homestead-Miami Speedway in April 2006, at the same venue once more in March of 2007, and at Laguna Seca in August 2008. This totals to only six heats over the three Corse Clienti events, with the car logging perhaps three to four hours of track time since new. The color scheme of pearl white with red trim is unique amongst the 37 other FXXs produced, and it is incredibly attractive both at speed and at a standstill.

 

In early 2008, before it was used at the Laguna Seca Corse Clienti event in August, FXX number 1 was converted to Evoluzione specifications by the factory. Thanks to data, telemetry, and feedback gathered from owners over the first two years of the program, the factory was able to perform a series of upgrades to the car in order to increase every parameter of its performance. The “Evo” upgrades included gear ratios being changed to accommodate the extra 1,000 rpm produced by the engine, which resulted in the gearshifts now taking place in 60 milliseconds and the FXX’s lap time around Fiorano being cut down by two seconds. The upgrades also included modified aerodynamics, an improved and more complex traction-control system, a braking system upgraded with better cooling and ductwork and more durable brake pads, and a rear-camera upgraded in order to provide the driver with increased rearward visibility.

 

Ownership of a FXX provides its possessor not only with a car of incredible performance but also a once-in-a-lifetime opportunity to work directly with the company that created it through a wholly unique racing experience. There is no doubt that data gained during the FXX program contributed to the development of the revolutionary LaFerrari, as well as numerous other cars in the marque’s current lineup and perhaps future models in the years to come. Despite the unveiling of the LaFerrari and its Corse Clienti sibling, the FXX K, the FXX Programme will continue for the 2015 season, with a calendar of events already announced. Both the car and program showcase Ferrari’s unwavering commitment to their customers to produce not only the finest motor cars in the world but to also furnish an entire motoring experience based around an automobile.

 

With only three Corse Clienti events under its belt, FXX number 1 is ready for many more track days, and it will forever remain a symbol of Ferrari’s ever-evolving performance, technology, and steadfast commitment to its clientele.

 

This Ferrari FXX Evoluzione (chassis ZFFHX62X000145369) sold for $1,622,500.

 

[Text from RM Auctions]

 

www.rmsothebys.com/lots/lot.cfm?lot_id=1072254

 

This Lego miniland scale Ferrari FXX Evoluzione (2005) has been created for Flickr LUGNuts' 96th Build Challenge - The 8th Birthday, titled - 'Happy Crazy Eight Birthday, LUGNuts' - where all previous build challenges are available to build to. This model is built to the LUGNuts 89th Build Challenge, - "Over a Million, Under a Thousand" - a challenge to build a vehicle which costs over one million dollars, or under on thousand dollars.

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based historical facts. BEWARE!

  

Some background:

The North American FJ-4 Fury was a swept-wing carrier-capable fighter-bomber, originally developed for the United States Navy and Marine Corps. It was the final development in a lineage that included the Air Force's F-86 Sabre. The FJ-4 shared its general layout and engine with the earlier FJ-3, but featured an entirely new wing design. And it was, as a kind of final embodiment with the FJ-4B, a very different aircraft from the F-86 .

 

The first FJ-4 flew on 28 October 1954 and delivery began in February 1955. Of the original order for 221 FJ-4 fighters, the last 71 were modified into the FJ-4B fighter-bomber version, of which the Netherlands received 16 aircraft under the designation FJ-4B from the USA in the course of NATO support. Even though the main roles of the MLD were maritime patrol, anti-submarine warfare and search and rescue, the FJ-4B was a dedicated fighter-bomber, and these aircraft were to be used with the Dutch Navy’s Colossus-Class carrier HNLMS Karel Doorman (R81).

 

Compared to the lighter FJ-4 interceptor, the FJ-4B had a stronger wing with six instead of four underwing stations, a stronger landing gear and additional aerodynamic brakes under the aft fuselage. The latter made landing safer by allowing pilots to use higher thrust settings, and were also useful for dive attacks. Compared to the FJ-4, external load was doubled, and the US FJ-4Bs were capable of carrying a nuclear weapon on the inboard port station, a feature the MLD Furies lacked. The MLD aircraft were still equipped with the corresponding LABS or Low-Altitude Bombing System for accurate delivery of ordnance.

The Dutch Furies were primarily intended for anti-ship missions (toting up to five of the newly developed ASM-N-7 missiles - renamed in AGM-12B Bullpup after 1962 - plus a guidance pod) and CAS duties against coastal targets, as well as for precision strikes. In a secondary role, the FJ-4B could carry Sidewinder AAMs for interception purposes.

 

The MLD's FJ-4B became operational in 1956, just in time to enhance the firepower of the Karel Doorman, which just had its 24 WW-II era propeller driven Fairey Firefly strike fighters and Hawker Sea Fury fighter/anti-ship aircraft backed up with 14 TBF Avenger ASW/torpedo bombers and 10 Hawker Sea Hawk fighters (the MLD owned 22 of these) for an ASW/Strike profile. The Furies joined the carrier in late 1957 and replaced the piston-engined attack aircraft.

 

In 1960, during the Dutch decolonization and planned independence of Western New Guinea, a territory which was also claimed by Indonesia, the Karel Doorman set sail along with two destroyers and a modified oil tanker to 'show the flag'. In order to avoid possible problems with Indonesia's ally Egypt at the Suez Canal, the carrier instead sailed around the horn of Africa. She arrived in Fremantle, Australia, where the local seamen's union struck in sympathy with Indonesia; the crew used the propeller thrust of aircraft chained down on deck to nudge the carrier into dock without tugs! In addition to her air wing, she was ferrying twelve Hawker Hunter fighters to bolster the local Dutch defense forces, which the Karel Doorman delivered when she arrived at Hollandia, New Guinea.

 

During the 1960 crisis, Indonesia prepared for a military action named Operation Trikora (in the Indonesian language, "Tri Komando Rakyat" means "The Three Commands of the People"). In addition to planning for an invasion, the TNI-AU (Indonesian Air Forces) hoped to sink the Karel Doorman with Soviet-supplied Tupolev Tu-16KS-1 Badger naval bombers using AS-1 Kennel/KS-1 Kometa anti-ship missiles. This bomber-launched missile strike mission was cancelled on short notice, though, because of the implementation of the cease-fire between Indonesia and the Netherlands. This led to a Dutch withdrawal and temporary UN peacekeeping administration, followed by occupation and annexation through Indonesia. While the Dutch aircraft served actively during this conflict, flying patrols and demonstrating presence, visibly armed and in alert condition, no 'hot' sortie or casualty occured, even though one aircraft, 10-18, was lost in a start accident. The pilot ejected safely.

 

The MLD FJ-4Bs only served on the carrier until its overhaul in 1964, after which the carrier-borne attack role was eliminated and all aircraft were transferred to land bases (Valkenburg) or in reserve storage. The Seahawks were retired from service by the end of the 1960s after the sale of the Karel Doorman to Argentina, and the FJ-4Bs were returned to the United States, where they were re-integrated into the USMC until the end of the 1960ies, when all FJ-4 aircraft were phased out.

  

General characteristics:

Crew: 1

Length: 36 ft 4 in (11.1 m)

Wingspan: 39 ft 1 in (11.9 m)

Height: 13 ft 11 in (4.2 m)

Wing area: 338.66 ft² (31.46 m²)

Empty weight: 13,210 lb (6,000 kg)

Loaded weight: 20,130 lb (9,200 kg)

Max. take-off weight: 23,700 lb (10,750 kg)

Powerplant: 1 × Wright J65-W-16A turbojet, 7,700 lbf (34 kN)

 

Performance:

Maximum speed: 680 mph (1,090 km/h) at 35,000 ft (10,670 m)

Range: 2,020 mi (3,250 km) with 2× 200 gal (760 l) drop tanks and 2× AIM-9 missiles

Service ceiling: 46,800 ft (14,300 m)

Rate of climb: 7,660 ft/min (38.9 m/s)

Wing loading: 69.9 lb/ft² (341.7 kg/m²)

Thrust/weight: .325

 

Armament:

4× 20 mm (0.787 in) cannon

6× pylons under the wings for 3,000 lb (1,400 kg) external ordnance, including up to 6× AIM-9 Sidewinder AAMs, bombs and guided/unguided ASM, e .g. ASM-N-7 (AGM-12B Bullpup) missiles.

  

The kit and its assembly

Originally, this model project was inspired by a (whiffy) Dutch F3H Demon profile, designed by fellow user Darth Panda at whatifmodelers.com. I found the idea of a foreign/NATO user of one of these early carrier-borne jet fighters very inspiring – not only because of the strange design of many of these aircraft, but also since the USN and USMC had been the only real world users of many of these types.

 

Initially, I planned to convert a F3H accordingly. But with limited storage/display space at home I decided to apply the MLD idea to another smaller, but maybe even more exotic, type: the North American FJ-4B Fury, which was in 1962 recoded into AF-1E.

I like the beefy Sabre cousin very much. It’s one of those aircraft that received little attention, even from model kit manufacturers. In fact, in 1:72 scale there are only vintage vacu kits or the very basic Emhar kit available. Th Emhar kit, which I used here and which is a kind donation of a fellow modeler (Thanks a lot, André!), a rather rough thing with raised panel lines and much room for improvements. As a side note, there's also a FJ-4B from Revell, but it's just a 1996 re-issue with no improvements, whatsoever.

 

Another facet of the model: When I did legwork concerning a possible background story, I was surprised to find out that the Netherlands actually operated aircraft carriers in the 1950s, including carrier-borne, fixed-wing aircraft, even jets in the form of Hawker Sea Hawks. The real life FJ-4Bs service introduction, the naissance of NATO and the Indonesian conflict as well as the corresponding intervention of the Karel Doorman carrier all fell into a very plausible time frame – and so there’s a very good and plausible story why the MLD could actually have used the Fury fighter bomber!

 

The Emhar kit was not modified structurally, but saw some changes in detail. These include a scratch-built cockpit with side walls, side consoles and a new ejection seat, plus a Matchbox pilot figure, a new front wheel (from a Kangnam Yak-38, I believe), plus a lot of added blade aerials and a finer pitot.

The flaps were lowered, for a more lively look- Another new feature is the opened air intake, which features a central splitter - in fact a vertically placed piece of a Vicker Wellesley bomb container from Matchbox. At the rear end, the exhaust pipe was opened and lengthened internally.

 

The six weapon hardpoints were taken from the original kit, but I did not use the four Sidewinder AAMs and the rather bulky drop tanks. So, all ordnance is new: the Bullpups come from the Hasegawa air-to-ground missile set, the drop tanks are leftover pieces from a Hobby Boss F-86. They are much more 'delicate', and make the Fury look less stout and cumbersome. The guidance pod for the Bullpups (a typical FJ-4B feature with these weapons) is a WWII drop tank, shaped with the help of benchmark pictures. Certainly not perfect, but, hey - it's just a MODEL!

  

Painting and markings

I used mid-1950ies MLD Sea Furys and Sea Hawks as a design benchmark, but this Fury is placed just into the time frame around 1960 when the MLD introduced a new 3-digit code system. Before that, a code "6-XX" with the XX somewhere in the 70 region would have been appropriate, and I actually painted the fuselage sides a bit darker so as if the old code had recently been painted over.

 

Dutch MLD aircraft tended to keep their former users’ liveries, but in the FJ-4B’s case I thought that a light grey and white aircraft (USN style) with Dutch roundels would look a bit odd. So I settled for early NATO style with Extra Dark Sea Grey upper sides (Humbrol 123) and Sky from below (Testors 2049 from their Authentic Line).

 

I also went for an early design style with a low waterline - early Hawker Sea Furies were painted this way, and a high waterline would probably be more typical. But in the face of potential seriosu action, who knows...? Things tend to be toned down quickly, just remember the RN Harriers during the Falkland conflict. I'll admit that the aircraft looks a bit simple and dull now, but this IMHO just adds to the plausible look of this whif. I prefer such subtleties to garish designs.

 

The surfaces were weathered with dry-brushed lighter shades of the basic tones (mostly Humbrol 79, but also some 140 and 67, and Humbrol 90 and 166 below), including overpainted old codes in a slightly darker tone of EDSG, done with Revell 77. A light wash with black ink emphasizes edges and some details - the machine was not to look worn.

 

The interior was painted in medium grey (Humbrol 140), the landing gear is white (Humbrol 130), and some details like the air intake rim, the edges of the landing gear covers, the flaps or the tips of the wing fences were painted in bright red (Humbrol 174), for some contrast to the overall grey upper sides.

 

The MLD markings were puzzled together. The roundels come from an Xtradecal sheet for various Hawker Sea Furies, the '202' code comes, among others, from a Grumman Bearcat aftermarket sheet. The 'KON. MARINE' line is hand-made, letter by letter, from a TL Modellbau aftremarket sheet.

Most stencils and warning sign decals come from the original decal sheet, as well as from a FJ-4 Xtradecal aftermarket sheet, from F-86 kits and the scrap box. I wanted these details to provide the color to the aircraft, so that it would not look too uniform, but still without flashy decorations and like a rather utilarian military item.

 

finally, the model received a coat of semi-matt varnish (Tamiya Acryllic), since MLD aircraft had a pretty glossy finish. No dirt or soot stains were added - the Dutch kept their (few) shipborne aircraft very clean and tidy!

  

So, all in all, a simple looking aircraft, but this Dutch Fury has IMHO a certain, subtle charm - probably also because it is a rather rare and unpopular aircraft, which in itself has a certain whiffy aura.

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based historical facts. BEWARE!

  

Some background:

The Sondergerät SG104 "Münchhausen" was a German airborne recoillless 355.6 mm (14-inch) caliber gun, intended to engage even the roughest enemy battleships, primarily those of the Royal Navy. The design of this unusual and massive weapon began in 1939. The rationale behind it was that a battleship’s most vulnerable part was the deck – a flat surface, with relatively thin armor (as typical hits were expected on the flanks) and ideally with vital targets underneath, so that a single, good hit would cripple of even destroy a ship. The purpose of such a high angle of attack was likely to allow the projectile to penetrate the target ship's deck, where the ship's armor, if there was any, would have been much thinner than the armor on its sidesHowever, hitting the deck properly with another ship’s main gun was not easy, since it could only be affected through indirect hits and the typical angle of the attack from aballistic shot would not necessarily be ideal for deep penetration, esp. at long range.

The solution to this problem: ensure that the heavy projectile would hit its target directly from above, ideally at a very steep angle. To achieve this, the gun with battleship caliber was “relocated” from a carrier ship or a coastal battery onto an aircraft – specifically to a type that was capable of dive-bombing, a feature that almost any German bomber model of the time offered.

 

Firing such a heavy weapon caused a lot fo problems, which were severe even if the gun was mounted on a ship or on land. To compensate for such a large-caliber gun’s recoil and to make firing a 14 in shell (which alone weighed around almost 700 kg/1.550 lb, plus the charge) from a relatively light airframe feasible, the respective gun had to be as light as possible and avoid any recoil, which would easily tear an aircraft – even a bomber – apart upon firing. Therefore, the Gerät 104 was designed as a recoilless cannon. Its firing system involved venting the same amount of the weapon's propellant gas for its round to the rear of the launch tube (which was open at both ends), in the same fashion as a rocket launcher. This created a forward directed momentum which was nearly equal to the rearward momentum (recoil) imparted to the system by accelerating the projectile itself. The balance thus created did not leave much net momentum to be imparted to the weapon's mounting or the carrying airframe in the form of felt recoil. A further share of the recoil induced by the moving round itself could be compensated by a muzzle brake which re-directed a part of the firing gases backwards. Since recoil had been mostly negated, a heavy and complex recoil damping mechanism was not necessary – even though the weapon itself was huge and heavy.

 

Work on the "Münchhausen" device (a secret project handle after a fictional German nobleman created by the German writer Rudolf Erich Raspe in the late 18th century who reputedly had ridden on a cannonball between enemy frontlines), was done by Rheinmetall-Borsig and lasted until 1941. The first test of a prototype weapon was conducted on 9th of September 1940 in Unterlüss with a satisfactory result, even though the weapon was only mounted onto an open rack and not integrated into an airframe yet. At that time, potential carriers were the Ju 88, the Dornier Do 217 and the new Junkers Ju 288. Even though the system’s efficacy was doubted, the prospect of delivering a single, fatal blow to an important , armored arget superseded any doubts at the RLM, and the project was greenlit in early 1942 for the next stage: the integration of the Sondergerät 104 into an existing airframe. The Ju 88 and its successor, the Ju 188, turned out to be too light and lacked carrying capacity for the complete, loaded weapon, and the favored Ju 288 was never produced, so that only the Dornier Do 217 or the bigger He 177 remained as a suitable carriers. The Do 217 was eventually chosen because it had the biggest payload and the airframe was proven and readily available.

 

After calculations had verified that the designed 14 in rifle would have effectively no recoil, preliminary tests with dumm airframes were carried out. After ground trials with a Do 217 E day bomber to check recoil and blast effects on the airframe, the development and production of a limited Nullserie (pre-production series) of the dedicated Do 217 F variant for field tests and eventual operational use against British sea and land targets was ordered in April 1942.

 

The resulting Do 217 F-0 was based on the late “E” bomber variant and powered by a pair of BMW 801 radial engines. It was, however, heavily modified for its unique weapon and the highly specialized mission profile: upon arriving at the zone of operation at high altitude, the aircraft would initiate a dive with an angle of attack between 50° and 80° from the horizontal, firing the SG 104 at an altitude between 6,000 and 2,000 meters. The flight time of the projectile could range from 16.0 seconds for a shot from an altitude of 6,000 meters at a 50° angle to just 4.4 seconds for a shot from 2.000 meters at an almost vertical 80° angle. Muzzle velocity of the SG 104 was only 300 m/s, but, prior to impact, the effective velocity of the projectile was projected to range between 449 and 468 m/s (1,616 to 1,674 km/h). Together with the round's weight of roughly 700 kg (1.550 lb) and a hardened tip, this would still ensure a high penetration potential.

 

The operational Sondergerät 104 had an empty mass of 2.780 kg (6,123 lb) and its complete 14 inch double cartridge weighed around 1.600 kg (3,525 lb). The loaded mass of the weapon was 4,237 kg, stretching the limits of the Do 217’s load capacity to the maximum, so that some armor and less vital pieces of equipment were deleted. Crew and defensive armament were reduced to a minimum.

Even though there had been plans to integrate the wepaon into the airframe (on the Ju 288), the Gerät 104 was on the Do 217 F-0 mounted externally and occupied the whole space under the aircraft, precluding any use of the bomb bay. The latter was occupied by the Gerät 104’s complex mount, which extended to the outside under a streamlined fairing and held the weapon at a distance from the airframe. Between the mount’s struts inside of the fuselage, an additional fuel tank for balance reasons was added, too.

The gun’s center, where the heavy round was carried, was positioned under the aircraft’s center of gravity, so that the gun barrel markedly protruded from under the aircraft’s nose. To make enough space, the Do 217 Es bomb aimer’s ventral gondola and his rearward-facing defensive position under the cockpit were omitted and faired over. The nose section was also totally different: the original extensive glazing (the so-called “Kampfkopf”) was replaced by a smaller, conventional canopy, similar to the later Do 217 J and N night fighter versions, together with a solid nose - the original glass panels would have easily shattered upon firing the gun, esp. in a steep high-speed dive. A "Lotfernrohr" bomb aiming device was still installed in a streamlined and protected fairing, though, so that the navigator could guide the pilot during the approach to the target and during the attack run.

To stabilize the heavy aircraft during its attack and to time- and safely pull out of the dive, a massive mechanical dive brake was mounted at the extended tail tip, which unfolded with four "petals". A charecteristic stabilizing dorsal strake was added between the twin fins, too.

 

The ventral area behind the gun’s rear-facing muzzle received additional metal plating and blast guiding vanes, after trials in late 1940 had revealed that firing the SG 104 could easily damage the Do 217’s tail structure, esp. all of the tail surfaces’ rudders and the fins’ lower ends in particular. Due to all this extra weight, the Do 217 F-0’s defensive armament consisted only of a single 13 mm MG 131 machine gun in a manually operated dorsal position behind the cockpit cabin, which offered space for a crew of three. A fixed 15 mm MG 151 autocannon was mounted in the nose, too, a weapon with a long barrel for extended range and accuracy. It was not an offensive weapon, though, rather intended as an aiming aid for the SG 104 because it was loaded with tracer bullets: during the final phase of the attack dive, the pilot kept firing the MG 151, and the bullet trail showed if he was on target to fire the SG 104 when the right altitude/range had been reached.

 

The first Do 217 F-0 was flown and tested in late 1943, and after some detail changes the type was cleared for a limited production run of ten aircraft in January 1944. The first operational machine was delivered to a dedicated testing commando, the Erprobungskommando 104 “Münchhausen”, also known as “Sonderkommando Münchhausen” or simply “E-Staffel 104”. The unit was based at Bordeaux/Merignac and directly attached to the KG 40's as a staff flight. At that time, KG 40 operated Do 217 and He 177 bombers and frequently flew reconnaissance and anti-shipping missions over the Atlantic west of France, up to the British west and southern coast, equipped with experimental Henschel Hs 293 glide bombs.

 

Initial flights confirmed that the Do 217 airframe was burdened with the SG 104 to its limits, the already rather sluggish aircraft (the Do 217 had generally a high wing loading and was not easy to fly) lost anything that was left of what could be called agility. It needed an experienced pilot to handle it safely, esp. during start and landing. It is no wonder that two Do 217 F-0s suffered ground accidents during the first two weeks of operations, but the machines could be repaired, resume the test program and carry out attack missions.

However, during one of the first test shots with the weapon, one Do 217 F-0 lost its complete tail section though the gun blast, and the aircraft crashed into the Bay of Biscay, killing the complete crew.

 

On 4th or April 1944 the first "hot" attack against an enemy ship was executed in the Celtic Sea off of Brest, against a convoy of 20 ships homeward bound from Gibraltar. The attack was not successful, though, the shot missing its target, and the German bomber was attacked and heavily damaged by British Bristol Beaufighters that had been deployed to protect the ships. The Do 217F-0 eventually crashed and sank into the Atlantic before it could reach land again.

 

A couple of days later, on 10th of April, the first attempt to attack and destroy a land target was undertaken: two Do 217 F-0s took off to attack Bouldnor Battery, an armored British artillery position located on the Isle of Wight. One machine had to abort the attack due to oil leakages, the second Do 217 F-0 eventually reached its target and made a shallow attack run, but heavy fog obscured the location and the otherwise successful shot missed the fortification. Upon return to its home base the aircraft was intercepted by RAF fighters over the Channel and heavily damaged, even though German fighters deployed from France came to the rescue, fought the British attackers off and escorted the limping Do 217 F-0 back to its home base.

 

These events revealed that the overall SG 104 concept was generally feasible, but also showed that the Do 217 F-0 was very vulnerable without air superiority or a suitable escort, so that new tactics had to be developed. One consequence was that further Do 217 F-0 deployments were now supported by V/KG 40, the Luftwaffe's only long range maritime fighter unit. These escorts consisted of Junkers Ju 88C-6s, which were capable of keeping up with the Do 217 F-0 and fend of intercepting RAF Coastal Command’s Beaufighters and later also Mosquitos.

 

In the meantime, tests with the SG 104 progressed and several modifications were tested on different EKdo 104's Do 217 F-0s. One major upgrade was a further strengthening of the tail section, which added another 200 kg (440 lb) to the aircraft's dry weight. Furthermore, at least three aircraft were outfitted with additional dive brakes under the outer wings, so that the dive could be better controlled and intercepted. these aircraft, however, lost their plumbed underwing hardpoints, but these were only ever used for drop tanks during transfer flights - a loaded SG 104 precluded any other ordnance. On two other aircraft the SG 104 was modified to test different muzzle brakes and deflectors for the rear-facing opening, so that the gun blast was more effectively guided away from the airframe to prevent instability and structural damage. For instance, one machine was equipped with a bifurcated blast deflector that directed the rearward gasses partly sideways, away from the fuselage.

 

These tests did not last long, though. During the Allied Normandy landings in June 1944 E-Staffel 104 was hastily thrown into action and made several poorly-prepared attack runs against Allied support ships. The biggest success was a full hit and the resulting sinking of the Norwegian destroyer HNoMS Svenner (G03) by "1A+BA" at dawn on 6th of June, off Sword, one of the Allied landing zones. Other targets were engaged, too, but only with little effect. This involvement, however, led to the loss of three Do 217 F-0s within just two days and four more heavily damaged aircraft – leaving only two of EKdo 104's Do 217 F-0s operational.

 

With the Allied invasion of France and a worsening war condition, the SG 104 program was stopped in August 1944 and the idea of an airborne anti-ship gun axed in favor of more flexible guided weapons like the Hs 293 missile and the Fritz-X glide bomb. Plans for a further developed weapon with a three-round drum magazine were immediately stopped, also because there was no carrier aircraft in sight that could carry and deploy this complex 6.5 tons weapon. However, work on the SG 104 and the experience gained from EKdo 104's field tests were not in vain. The knowledge gathered from the Münchhausen program was directly used for the design of a wide range of other, smaller recoilless aircraft weapons, including the magnetically-triggered SG 113 "Förstersonde" anti-tank weapon or the lightweight SG 118 "Rohrblock" unguided air-to-air missile battery for the Heinkel He 162 "Volksjäger".

  

General characteristics:

Crew: 3 (pilot, navigator, radio operator/gunner)

Length: 20,73 m (67 ft 11 in) overall

18,93 m (62 ft 3/4 in) hull only

Wingspan: 19 m (62 ft 4 in)

Height: 4.97 m (16 ft 4 in)

Wing area: 57 m² (610 sq ft)

Empty weight: 9,065 kg (19,985 lb)

Empty equipped weight:10,950 kg (24,140 lb)

Max takeoff weight: 16,700 kg (36,817 lb)

Fuel capacity: 2,960 l (780 US gal; 650 imp gal) in fuselage tank and four wing tanks

 

Powerplant:

2× BMW 801D-2 14-cylinder air-cooled radial piston engines, delivering

1,300 kW (1,700 hp) each for take-off and 1,070 kW (1,440 hp) at 5,700 m (18,700 ft),

driving 3-bladed VDM constant-speed propellers

 

Performance:

Maximum speed: 475 km/h (295 mph, 256 kn) at sea level

560 km/h (350 mph; 300 kn) at 5,700 m (18,700 ft)

Cruise speed: 400 km/h (250 mph, 220 kn) with loaded Gerät 104 at optimum altitude

Range: 2,180 km (1,350 mi, 1,180 nmi) with maximum internal fuel

Ferry range: 2,500 km (1,600 mi, 1,300 nmi); unarmed, with auxiliary fuel tanks

Service ceiling: 7,370 m (24,180 ft) with loaded Gerät 104,

9,500 m (31,200 ft) after firing

Rate of climb: 3.5 m/s (690 ft/min)

Time to altitude: 1,000 m (3,300 ft) in 4 minutes 10 seconds

2,000 m (6,600 ft) in 8 minutes 20 seconds

6,100 m (20,000 ft) in 24 minutes 40 seconds

 

Armament:

1x 355.6 mm (14-inch) Sondergerät 104 recoilless gun with a single round in ventral position

1x 15 mm (0.787 in) MG 151 machine cannon with 200 rounds, fixed in the nose

1x 13 mm (0.512 in) MG 131 machine gun with 500 rounds, movable in dorsal position

Two underwing hardpoints for a 900 l drop tank each, but only used during unarmed ferry flights

  

The kit and its assembly:

This was another submission to the "Gunships" group build at whatifmodellers.com in late 2021, and inspiration struck when I realized that I had two Italeri Do 217 in The Stash - a bomber and a night fighter - that could be combined into a suitable (fictional) carrier for a Sondergerät 104. This mighty weapon actually existed and even reached the hardware/test stage - but it was never integrated into an airframe and tested in flight. But that's what this model is supposed to depict.

 

On the Do 217, the Sg 104 would have been carried externally under the fuselage, even though there had been plans to integrate this recoilless rifle into airframes, esp. into the Ju 288. Since the latter never made it into production, the Do 217 would have been the most logical alternative, also because it had the highest payload of all German bombers during WWII and probably the only aircraft capable of carrying and deploying the Münchhausen device, as the SG 104 was also known.

 

The fictional Do 217 F-0 is a kitbashing, using a Do 217 N fuselage, combined with the wings from a Do 217 K bomber, plus some modifications. What initially sounded like a simple plan soon turned into a improvisation mess: it took some time to realize that I had already donated the Do 217 K's BMW 801 engines to another project, an upgraded He 115... I did not want to use the nightfighter's more powerful DB 603s, and I was lucky to have an Italeri Ju 188 kit at hand which comes with optional BMW 801s and Jumo 211s. Transplanting these engines onto the Do 217's wings took some tailoring of the adapter plates, but was feasible. However, the BMW 801s from the Ju 188 kit have a flaw: they lack the engine's characteristic cooling fans... Another lucky find: I found two such parts in the scrap box, even though from different kits - one left over from another Italeri Do 217 K, the other one from what I assume is/was an Italeri 1:72 Fw 190 A/F. To make matters worse, one propeller from the Ju 188 kit was missing, so that I had to find a(nother) replacement. :-/

I eventually used something that looked like an 1:72 F6F Hellcat propeller, but I an not certain about this because I have never built this model...? With some trimming on the blades' trailing edges and other mods, the donor's overall look could be adapted to the Ju 188 benchmark. Both propellers were mounted on metal axis' so that they could also carry the cooling fans. Lots of work, but the result looks quite good.

 

The Do 217 N's hull lost the lower rear gunner position and its ventral gondola, which was faired over with a piece of styrene sheet. The pilot was taken OOB, the gunner in the rear position was replaced by a more blob-like crew member from the scrap box. The plan to add a navigator in the seat to the lower right of the pilot did not work out due to space shortage, but this figure would probably have been invisble, anyway.

All gun openings in the nose were filled and PSRed away, and a fairing for a bomb aiming device and a single gun (the barrel is a hollow steel needle) were added.

 

The SG 104 was scratched. Starting point was a white metal replacement barrel for an 1:35 ISU-152 SPG with a brass muzzle brake. However, after dry-fitting the barrel under the hull the barrel turned out to be much too wide, so that only the muzzal brake survived and the rest of the weapon was created from a buddy refueling pod (from an Italeri 1:72 Luftwaffe Tornado, because of its two conical ends) and protective plastic caps from medical canulas. To attach this creation to the hull I abused a conformal belly tank from a Matchbox Gloster Meteor night fighter and tailored it into a streamlined fairing. While this quite a Frankenstein creation, the overall dimensions match the real SG 104 prototype and its look well.

 

Other cosmetic modifications include a pair of underwing dive brakes, translanted from an Italeri 1:72 Ju 88 A-4 kit, an extended (scratched) tail "stinger" which resembles the real dive brake arrangement that was installed on some Do 217 E bombers, and I added blast deflector vanes and a dorsal stabilizer fin.

In order to provide the aircraft with enough ground clearance, the tail wheel was slightly extended. Thanks to the long tail stinger, this is not blatantly obvious.

  

Painting and markings:

This was not an easy choice, but as a kind of prototype I decided that the paint scheme should be rather conservative. However, German aircraft operating over the Atlantic tended to carry rather pale schemes, so that the standard pattern of RLM 70/71/65 (Dunkelgrün, Schwarzgrün and Hellblau) with a low waterline - typical for experimental types - would hardly be appropriate.

I eventually found a compromise on a He 177 bomber (coded 6N+BN) from 1944 that was operated by KG 100: this particular aircraft had a lightened upper camouflage - still a standard splinter scheme but consisting of RLM 71 and 02 (Dunkelgrün and Grau; I used Modelmaster 2081 and Humbrol 240), a combination that had been used on German fighters during the Battle of Britain when the standard colors turned out to be too dark for operations over the Channel. The aircraft also carried standard RLM 65 (or maybe the new RLM76) underneath (Humbrol 65) and on the fin, but with a very high and slightly wavy waterline. As a rather unusual feature, no typical camouflage mottles were carried on the flanks or the fin, giving the aircraft a very bleak and simple look.

 

Despite my fears that this might look rather boring I adapted this scheme for the Do 217 F-0, and once basic painting was completed I was rather pleased by the aircraft's look! As an aircraft operated at the Western front, no additional markings like fuselage bands were carried.

To set the SG 104 apart from the airframe, I painted the weapon's visible parts in RLM 66 (Schwarzgrau, Humbrol 67), because this tone was frequently used for machinery (including the interior surfaces of aircraft towards 1945).

RLM 02 was also used for the interior surfaces and the landing gear, even though I used a slightly different, lighter shade in form of Revell 45 (Helloliv).

 

A light black ink washing was applied and post-shading to emphasize panel lines. Most markings/decals came from a Begemot 1:72 He 11 sheet, including the unusual green tactical code - it belongs to a staff unit, a suitable marking for such an experimental aircraft. The green (Humbrol 2) was carried over to the tips of the propeller spinners. The unit's code "1A" is fictional, AFAIK this combination had never been used by the Luftwaffe.

The small unit badge was alucky find: it actually depicts the fictional Baron von Münchhausen riding on a cannonball, and it comes from an Academy 1:72 Me 163 kit and its respective sheet. The mission markings underneath, depicting two anti-ship missions plus a successful sinking, came from a TL Modellbau 1:72 scale sheet with generic German WWII victory markings.

 

After some soot stains around the engine exhaust and weapon muzzles had been added with graphite, the model was sealed with matt acrylic varnish and final details like position lights and wire antennae (from heated black plastic sprue material) were added.

  

Well, what started as a combination of two kits of the same kind with a simple huge pipe underneath turned out to be more demanding than expected. The (incomplete) replacement engines were quite a challenge, and body work on the hull (tail stinger, fairing for the SG 104 as well as the weapon itself) turned out to be more complex and extensive than initially thought of. The result looks quite convincing, also supported by the rather simple paint scheme which IMHO just "looks right" and very convincing. And the whole thing is probably the most direct representation of the inspiring "Gunship" theme!

 

History of St Gabriel’s

Early History of St Gabriel’s

 

A study of the 1895 Ordnance Survey map of Byker and Heaton reveals a building described as St Gabriel’s Church but this building is not where you would expect it to be on Heaton Road. It is to the east of Chillingham Road on the north side of a road that is not named but can be recognised as present day Rothbury Terrace. To the south is a cricket ground and a football ground.There is a record that states that in 1890 ‘the wooden building was replaced with a structure of corrugated iron lined with wood, costing £500, with seats for 350. It is not known whether the wooden building had also been a church. The building was known as St Gabriel’s Iron Mission Chapel and was a daughter church of St Michael’s, Byker.

 

Also in 1890 Lord Armstrong gave a new site for a permanent church to be built on the west side of Heaton Road near to its northern end and opposite a row of large villas between Simonside and Cartington Terraces. The architect appointed was Mr Frank W Rich and the Archdeacon of Northumberland recommended Mr Rich to prepare plans for a permanent church to be built in the Gothic design with a tower, a nave and one aisle, to hold 500 but capable of being enlarged to hold 600. Plans were submitted to Lord Armstrong for his approval. The site of the new church on Heaton Road was found in 1896 to be too narrow to accommodate a large church built on a cruciform shape. Lord Armstrong generously gave another sit directly north of the original site. On 1st December Bishop Edgar agreed that the architect Mr F W Rich should build a new stone church on the new site. The building contractor appointed was Mr Walter Baston, a member of St Gabriel’s congregation.

 

The foundation stone was laid by Mrs. Watson-Armstrong. Under the foundation stone was placed a description of the building, plans, local newspaper and coins. (The location of the foundation stone is unknown.) The Consecration of St. Gabriel’s Church by Bishop Jacob took place on Friday, 29th September 1899. A licence for Marriages was obtained in October and on 27th December 1899 Queen Victoria sanctioned the formation of the new Parish.

 

Spot the difference!

 

That takes us to until 29th September 1899, when the church was consecrated. As the postcard below illustrates this was only stage one of the construction.

 

The most obvious missing feature is the tower but if the building looks a bit short it is because the chancel is missing. The lower building at the south east corner was temporary vestries and the chimney was for the boiler in the cellar. Next time you are passing see if you can still find a chimney. There are no pinnacles on the turrets at the west end. The card was stamped with a Newcastle upon Tyne post mark at 5 pm AU 20 04.

 

It also shows pillars supporting a gate leading to the vicarage. There is a 1901 record that Mr Watson-Armstrong, Lord Armstrong’s nephew and heir kindly gave a site at the west end of the Church for a vicarage. An anonymous donor gave £1,000 towards the cost and a grant was made available from the Ecclesiastical Commissioners of £1,300. Mr Rich was given instructions to prepare plans. The clergy (vicar and two curates) plus housekeeper (Miss Welch) and maid moved into the new vicarage in May 1903. They had been living at 8 Rothbury Terrace. The new vicarage cost £3,500.

 

An extract from the April 1901 magazine reads:

“The enlargement of St Gabriel’s is an absolute necessary. It is admitted by all that the Church is too small, especially Sunday evenings when we are crowded out and very often would be worshipers have to go away as they cannot find a seat. We must, therefore, consider a scheme for the enlargement of the Church and provision for increased accommodation.”

 

And in a similar tone in October 1904:

“We have been told that people sometimes stay away from church on Sunday evenings because there is some difficulty in getting seats. The Bishop has consented to the North aisle being used before it is actually consecrated. We are glad to find how much more the North aisle has been appreciated; it is indeed a wonderful improvement to the church and it helps to see more of what it will be like when completed. We can now much more readily picture to ourselves how fine the effect will be when the North Transept arch is opened and the chancel added.”

 

Clearly building work is progressing and in 1905 we read that the dedication and consecration of the new parts of the church took place on 29 September. This was carried out by the Bishop and included the chancel, organ chamber, north aisle and transept and the porches at a cost of £14,000.

 

Also in 1905 the lower part of the tower was built and donated by Lord Armstrong. The next mention of the tower is in 1907 when it is noted that the Sale of Work was opened by Lord Armstrong and afforded an opportunity of thanking him for his generosity to St Gabriel’s. His latest gift was the tower by now making steady progress

 

Lord Armstrong also paid for the inscription around the top of the tower. The architect asked the vicar for a suitable engraving to go around the four sides and he choose the Sanctus:

 

Holy Holy Holy, Lord God of Hosts, | Heaven and Earth are full | of your Glory. Glory be to thee | Lord most High. Amen Alleluia

 

It was started on the south side as a result the east side on Heaton

 

Road reads Heaven and Earth are full! This was enough for a lady to write to the vicar and ask “…what is to become of me?” The tower is 99 feet high and some of the lettering is now showing its age.

 

In the parish magazine in July 1909, the Vicar, Churchwardens and Building Fund Committee wrote collectively regarding the inadequacy of the temporary vestries. The erection of permanent vestries were the next portion of the church extension scheme to be built. The new choir vestry would be a room sufficiently to provide for parish meetings, classes etc. This article appears to have had the desired effect as in September 1910 the Archdeacon of Northumberland dedicated new vestries for the Clergy, Churchwardens and Choir as well as two smaller rooms. Various furnishings were also dedicated but more about them another time.

 

This post card has a post mark of 1 Nov 15. The vestries mentioned above have been completed but there is clearly work to be done on the south side of the chancel. This is where the Lady Chapel now stands. It may have remained like this until 1930/31.

 

At the annual meeting in the spring of 1914 the vicar reported that an application for a grant for completion of the church had been declined by the Bishop but that he, the Bishop, would recommend a grant for a Parish Hall with rooms. A grant of £500 was awarded in August 1915 on condition that the congregation found the balance, around £1,250 by June 1916. At this stage the plan was to build on the site of the iron building on Rothbury Terrace, the City Council having indicated that it must be removed by 1917 due to its deteriorating condition.

 

A canteen was opened in the Iron Building from 5.30pm to 9.30pm for soldiers billeted in the parish.

The Iron Building was sold in 1919 for £150 having served as a church and parish hall for 30 years. This meant that there was no hall for social events. Lord Armstrong made available an allotment site on Chillingham Road at half its commercial value but it is not until 1923 that the Bishop agreed a free grant of £2,000 and a loan of £1,500. Plans were submitted for a hall to accommodate 500 with other rooms of varying sizes for classes and recreation.

 

The foundation stone was not laid until 6th September 1924. Then there were concerns about the slowness of the work and questions were being asked about what was going on behind the hoardings Chillingham Road/Cartington Terrace corner. Delays were caused by fresh negotiations with the contractors over costs and then a builders strike. The building was eventually blessed on 3rd December 1925.

 

It was to take until 1930 before the final phase of building work consisting of the South Transept and Lady Chapel was agreed. At this time it was decided to abandon the original plan for a Baptistry. This was to have been in the south west corner beside the porch. You can see the undressed stone on the post card at the beginning of this article. It is still undressed today partly hidden by a bay tree.

The final building work was completed in 1931 and dedicated by the Bishop on 4th October 1931. He also dedicated many internal features.

 

Newcastle upon Tyne, or simply Newcastle is a cathedral city and metropolitan borough in Tyne and Wear, England. It is located on the River Tyne's northern bank, opposite Gateshead to the south. It is the most populous settlement in the Tyneside conurbation and North East England.

 

Newcastle developed around a Roman settlement called Pons Aelius, the settlement became known as Monkchester before taking on the name of a castle built in 1080 by William the Conqueror's eldest son, Robert Curthose. It was one of the world's largest ship building and repair centres during the industrial revolution. Newcastle was part of the county of Northumberland until 1400, when it separated and formed a county of itself. In 1974, Newcastle became part of Tyne and Wear. Since 2018, the city council has been part of the North of Tyne Combined Authority.

 

The history of Newcastle upon Tyne dates back almost 2,000 years, during which it has been controlled by the Romans, the Angles and the Norsemen amongst others. Newcastle upon Tyne was originally known by its Roman name Pons Aelius. The name "Newcastle" has been used since the Norman conquest of England. Due to its prime location on the River Tyne, the town developed greatly during the Middle Ages and it was to play a major role in the Industrial Revolution, being granted city status in 1882. Today, the city is a major retail, commercial and cultural centre.

 

Roman settlement

The history of Newcastle dates from AD 122, when the Romans built the first bridge to cross the River Tyne at that point. The bridge was called Pons Aelius or 'Bridge of Aelius', Aelius being the family name of Roman Emperor Hadrian, who was responsible for the Roman wall built across northern England along the Tyne–Solway gap. Hadrian's Wall ran through present-day Newcastle, with stretches of wall and turrets visible along the West Road, and at a temple in Benwell. Traces of a milecastle were found on Westgate Road, midway between Clayton Street and Grainger Street, and it is likely that the course of the wall corresponded to present-day Westgate Road. The course of the wall can be traced eastwards to the Segedunum Roman fort at Wallsend, with the fort of Arbeia down-river at the mouth of the Tyne, on the south bank in what is now South Shields. The Tyne was then a wider, shallower river at this point and it is thought that the bridge was probably about 700 feet (210 m) long, made of wood and supported on stone piers. It is probable that it was sited near the current Swing Bridge, due to the fact that Roman artefacts were found there during the building of the latter bridge. Hadrian himself probably visited the site in 122. A shrine was set up on the completed bridge in 123 by the 6th Legion, with two altars to Neptune and Oceanus respectively. The two altars were subsequently found in the river and are on display in the Great North Museum in Newcastle.

 

The Romans built a stone-walled fort in 150 to protect the river crossing which was at the foot of the Tyne Gorge, and this took the name of the bridge so that the whole settlement was known as Pons Aelius. The fort was situated on a rocky outcrop overlooking the new bridge, on the site of the present Castle Keep. Pons Aelius is last mentioned in 400, in a Roman document listing all of the Roman military outposts. It is likely that nestling in the shadow of the fort would have been a small vicus, or village. Unfortunately, no buildings have been detected; only a few pieces of flagging. It is clear that there was a Roman cemetery near Clavering Place, behind the Central station, as a number of Roman coffins and sarcophagi have been unearthed there.

 

Despite the presence of the bridge, the settlement of Pons Aelius was not particularly important among the northern Roman settlements. The most important stations were those on the highway of Dere Street running from Eboracum (York) through Corstopitum (Corbridge) and to the lands north of the Wall. Corstopitum, being a major arsenal and supply centre, was much larger and more populous than Pons Aelius.

 

Anglo-Saxon development

The Angles arrived in the North-East of England in about 500 and may have landed on the Tyne. There is no evidence of an Anglo-Saxon settlement on or near the site of Pons Aelius during the Anglo-Saxon age. The bridge probably survived and there may well have been a small village at the northern end, but no evidence survives. At that time the region was dominated by two kingdoms, Bernicia, north of the Tees and ruled from Bamburgh, and Deira, south of the Tees and ruled from York. Bernicia and Deira combined to form the kingdom of Northanhymbra (Northumbria) early in the 7th century. There were three local kings who held the title of Bretwalda – 'Lord of Britain', Edwin of Deira (627–632), Oswald of Bernicia (633–641) and Oswy of Northumbria (641–658). The 7th century became known as the 'Golden Age of Northumbria', when the area was a beacon of culture and learning in Europe. The greatness of this period was based on its generally Christian culture and resulted in the Lindisfarne Gospels amongst other treasures. The Tyne valley was dotted with monasteries, with those at Monkwearmouth, Hexham and Jarrow being the most famous. Bede, who was based at Jarrow, wrote of a royal estate, known as Ad Murum, 'at the Wall', 12 miles (19 km) from the sea. It is thought that this estate may have been in what is now Newcastle. At some unknown time, the site of Newcastle came to be known as Monkchester. The reason for this title is unknown, as we are unaware of any specific monasteries at the site, and Bede made no reference to it. In 875 Halfdan Ragnarsson, the Danish Viking conqueror of York, led an army that attacked and pillaged various monasteries in the area, and it is thought that Monkchester was also pillaged at this time. Little more was heard of it until the coming of the Normans.

 

Norman period

After the arrival of William the Conqueror in England in 1066, the whole of England was quickly subjected to Norman rule. However, in Northumbria there was great resistance to the Normans, and in 1069 the newly appointed Norman Earl of Northumbria, Robert de Comines and 700 of his men were killed by the local population at Durham. The Northumbrians then marched on York, but William was able to suppress the uprising. That same year, a second uprising occurred when a Danish fleet landed in the Humber. The Northumbrians again attacked York and destroyed the garrison there. William was again able to suppress the uprising, but this time he took revenge. He laid waste to the whole of the Midlands and the land from York to the Tees. In 1080, William Walcher, the Norman bishop of Durham and his followers were brutally murdered at Gateshead. This time Odo, bishop of Bayeux, William's half brother, devastated the land between the Tees and the Tweed. This was known as the 'Harrying of the North'. This devastation is reflected in the Domesday Book. The destruction had such an effect that the North remained poor and backward at least until Tudor times and perhaps until the Industrial Revolution. Newcastle suffered in this respect with the rest of the North.

 

In 1080 William sent his eldest son, Robert Curthose, north to defend the kingdom against the Scots. After his campaign, he moved to Monkchester and began the building of a 'New Castle'. This was of the "motte-and-bailey" type of construction, a wooden tower on top of an earthen mound (motte), surrounded by a moat and wooden stockade (bailey). It was this castle that gave Newcastle its name. In 1095 the Earl of Northumbria, Robert de Mowbray, rose up against the king, William Rufus, and Rufus sent an army north to recapture the castle. From then on the castle became crown property and was an important base from which the king could control the northern barons. The Northumbrian earldom was abolished and a Sheriff of Northumberland was appointed to administer the region. In 1091 the parish church of St Nicholas was consecrated on the site of the present Anglican cathedral, close by the bailey of the new castle. The church is believed to have been a wooden building on stone footings.

 

Not a trace of the tower or mound of the motte and bailey castle remains now. Henry II replaced it with a rectangular stone keep, which was built between 1172 and 1177 at a cost of £1,444. A stone bailey, in the form of a triangle, replaced the previous wooden one. The great outer gateway to the castle, called 'the Black Gate', was built later, between 1247 and 1250, in the reign of Henry III. There were at that time no town walls and when attacked by the Scots, the townspeople had to crowd into the bailey for safety. It is probable that the new castle acted as a magnet for local merchants because of the safety it provided. This in turn would help to expand trade in the town. At this time wool, skins and lead were being exported, whilst alum, pepper and ginger were being imported from France and Flanders.

 

Middle Ages

Throughout the Middle Ages, Newcastle was England's northern fortress, the centre for assembled armies. The Border war against Scotland lasted intermittently for several centuries – possibly the longest border war ever waged. During the civil war between Stephen and Matilda, David 1st of Scotland and his son were granted Cumbria and Northumberland respectively, so that for a period from 1139 to 1157, Newcastle was effectively in Scottish hands. It is believed that during this period, King David may have built the church of St Andrew and the Benedictine nunnery in Newcastle. However, King Stephen's successor, Henry II was strong enough to take back the Earldom of Northumbria from Malcolm IV.

 

The Scots king William the Lion was imprisoned in Newcastle, in 1174, after being captured at the Battle of Alnwick. Edward I brought the Stone of Scone and William Wallace south through the town and Newcastle was successfully defended against the Scots three times during the 14th century.

 

Around 1200, stone-faced, clay-filled jetties were starting to project into the river, an indication that trade was increasing in Newcastle. As the Roman roads continued to deteriorate, sea travel was gaining in importance. By 1275 Newcastle was the sixth largest wool exporting port in England. The principal exports at this time were wool, timber, coal, millstones, dairy produce, fish, salt and hides. Much of the developing trade was with the Baltic countries and Germany. Most of the Newcastle merchants were situated near the river, below the Castle. The earliest known charter was dated 1175 in the reign of Henry II, giving the townspeople some control over their town. In 1216 King John granted Newcastle a mayor[8] and also allowed the formation of guilds (known as Mysteries). These were cartels formed within different trades, which restricted trade to guild members. There were initially twelve guilds. Coal was being exported from Newcastle by 1250, and by 1350 the burgesses received a royal licence to export coal. This licence to export coal was jealously guarded by the Newcastle burgesses, and they tried to prevent any one else on the Tyne from exporting coal except through Newcastle. The burgesses similarly tried to prevent fish from being sold anywhere else on the Tyne except Newcastle. This led to conflicts with Gateshead and South Shields.

 

In 1265, the town was granted permission to impose a 'Wall Tax' or Murage, to pay for the construction of a fortified wall to enclose the town and protect it from Scottish invaders. The town walls were not completed until early in the 14th century. They were two miles (3 km) long, 9 feet (2.7 m) thick and 25 feet (7.6 m) high. They had six main gates, as well as some smaller gates, and had 17 towers. The land within the walls was divided almost equally by the Lort Burn, which flowed southwards and joined the Tyne to the east of the Castle. The town began to expand north of the Castle and west of the Lort Burn with various markets being set up within the walls.

 

In 1400 Henry IV granted a new charter, creating a County corporate which separated the town, but not the Castle, from the county of Northumberland and recognised it as a "county of itself" with a right to have a sheriff of its own. The burgesses were now allowed to choose six aldermen who, with the mayor would be justices of the peace. The mayor and sheriff were allowed to hold borough courts in the Guildhall.

 

Religious houses

During the Middle Ages a number of religious houses were established within the walls: the first of these was the Benedictine nunnery of St Bartholomew founded in 1086 near the present-day Nun Street. Both David I of Scotland and Henry I of England were benefactors of the religious house. Nothing of the nunnery remains now.

 

The friary of Blackfriars, Newcastle (Dominican) was established in 1239. These were also known as the Preaching Friars or Shod Friars, because they wore sandals, as opposed to other orders. The friary was situated in the present-day Friars Street. In 1280 the order was granted royal permission to make a postern in the town walls to communicate with their gardens outside the walls. On 19 June 1334, Edward Balliol, claimant to be King of Scotland, did homage to King Edward III, on behalf of the kingdom of Scotland, in the church of the friary. Much of the original buildings of the friary still exist, mainly because, after the Dissolution of the Monasteries the friary of Blackfriars was rented out by the corporation to nine of the local trade guilds.

 

The friary of Whitefriars (Carmelite) was established in 1262. The order was originally housed on the Wall Knoll in Pandon, but in 1307 it took over the buildings of another order, which went out of existence, the Friars of the Sac. The land, which had originally been given by Robert the Bruce, was situated in the present-day Hanover Square, behind the Central station. Nothing of the friary remains now.

 

The friary of Austinfriars (Augustinian) was established in 1290. The friary was on the site where the Holy Jesus Hospital was built in 1682. The friary was traditionally the lodging place of English kings whenever they visited or passed through Newcastle. In 1503 Princess Margaret, eldest daughter of Henry VII of England, stayed two days at the friary on her way to join her new husband James IV of Scotland.

 

The friary of Greyfriars (Franciscans) was established in 1274. The friary was in the present-day area between Pilgrim Street, Grey Street, Market Street and High Chare. Nothing of the original buildings remains.

 

The friary of the Order of the Holy Trinity, also known as the Trinitarians, was established in 1360. The order devoted a third of its income to buying back captives of the Saracens, during the Crusades. Their house was on the Wall Knoll, in Pandon, to the east of the city, but within the walls. Wall Knoll had previously been occupied by the White Friars until they moved to new premises in 1307.

 

All of the above religious houses were closed in about 1540, when Henry VIII dissolved the monasteries.

 

An important street running through Newcastle at the time was Pilgrim Street, running northwards inside the walls and leading to the Pilgrim Gate on the north wall. The street still exists today as arguably Newcastle's main shopping street.

 

Tudor period

The Scottish border wars continued for much of the 16th century, so that during that time, Newcastle was often threatened with invasion by the Scots, but also remained important as a border stronghold against them.

 

During the Reformation begun by Henry VIII in 1536, the five Newcastle friaries and the single nunnery were dissolved and the land was sold to the Corporation and to rich merchants. At this time there were fewer than 60 inmates of the religious houses in Newcastle. The convent of Blackfriars was leased to nine craft guilds to be used as their headquarters. This probably explains why it is the only one of the religious houses whose building survives to the present day. The priories at Tynemouth and Durham were also dissolved, thus ending the long-running rivalry between Newcastle and the church for control of trade on the Tyne. A little later, the property of the nunnery of St Bartholomew and of Grey Friars were bought by Robert Anderson, who had the buildings demolished to build his grand Newe House (also known as Anderson Place).

 

With the gradual decline of the Scottish border wars the town walls were allowed to decline as well as the castle. By 1547, about 10,000 people were living in Newcastle. At the beginning of the 16th century exports of wool from Newcastle were more than twice the value of exports of coal, but during the century coal exports continued to increase.

 

Under Edward VI, John Dudley, Duke of Northumberland, sponsored an act allowing Newcastle to annexe Gateshead as its suburb. The main reason for this was to allow the Newcastle Hostmen, who controlled the export of Tyne coal, to get their hands on the Gateshead coal mines, previously controlled by the Bishop of Durham. However, when Mary I came to power, Dudley met his downfall and the decision was reversed. The Reformation allowed private access to coal mines previously owned by Tynemouth and Durham priories and as a result coal exports increase dramatically, from 15,000 tons in 1500 to 35,000 tons in 1565, and to 400,000 tons in 1625.

 

The plague visited Newcastle four times during the 16th century, in 1579 when 2,000 people died, in 1589 when 1700 died, in 1595 and finally in 1597.

 

In 1600 Elizabeth I granted Newcastle a charter for an exclusive body of electors, the right to elect the mayor and burgesses. The charter also gave the Hostmen exclusive rights to load coal at any point on the Tyne. The Hostmen developed as an exclusive group within the Merchant Adventurers who had been incorporated by a charter in 1547.

 

Stuart period

In 1636 there was a serious outbreak of bubonic plague in Newcastle. There had been several previous outbreaks of the disease over the years, but this was the most serious. It is thought to have arrived from the Netherlands via ships that were trading between the Tyne and that country. It first appeared in the lower part of the town near the docks but gradually spread to all parts of the town. As the disease gained hold the authorities took measures to control it by boarding up any properties that contained infected persons, meaning that whole families were locked up together with the infected family members. Other infected persons were put in huts outside the town walls and left to die. Plague pits were dug next to the town's four churches and outside the town walls to receive the bodies in mass burials. Over the course of the outbreak 5,631 deaths were recorded out of an estimated population of 12,000, a death rate of 47%.

 

In 1637 Charles I tried to raise money by doubling the 'voluntary' tax on coal in return for allowing the Newcastle Hostmen to regulate production and fix prices. This caused outrage amongst the London importers and the East Anglian shippers. Both groups decided to boycott Tyne coal and as a result forced Charles to reverse his decision in 1638.

 

In 1640 during the Second Bishops' War, the Scots successfully invaded Newcastle. The occupying army demanded £850 per day from the Corporation to billet the Scottish troops. Trade from the Tyne ground to a halt during the occupation. The Scots left in 1641 after receiving a Parliamentary pardon and a £4,000,000 loan from the town.

 

In 1642 the English Civil War began. King Charles realised the value of the Tyne coal trade and therefore garrisoned Newcastle. A Royalist was appointed as governor. At that time, Newcastle and King's Lynn were the only important seaports to support the crown. In 1644 Parliament blockaded the Tyne to prevent the king from receiving revenue from the Tyne coal trade. Coal exports fell from 450,000 to 3,000 tons and London suffered a hard winter without fuel. Parliament encouraged the coal trade from the Wear to try to replace that lost from Newcastle but that was not enough to make up for the lost Tyneside tonnage.

 

In 1644 the Scots crossed the border. Newcastle strengthened its defences in preparation. The Scottish army, with 40,000 troops, besieged Newcastle for three months until the garrison of 1,500 surrendered. During the siege, the Scots bombarded the walls with their artillery, situated in Gateshead and Castle Leazes. The Scottish commander threatened to destroy the steeple of St Nicholas's Church by gunfire if the mayor, Sir John Marley, did not surrender the town. The mayor responded by placing Scottish prisoners that they had captured in the steeple, so saving it from destruction. The town walls were finally breached by a combination of artillery and sapping. In gratitude for this defence, Charles gave Newcastle the motto 'Fortiter Defendit Triumphans' to be added to its coat of arms. The Scottish army occupied Northumberland and Durham for two years. The coal taxes had to pay for the Scottish occupation. In 1645 Charles surrendered to the Scots and was imprisoned in Newcastle for nine months. After the Civil War the coal trade on the Tyne soon picked up and exceeded its pre-war levels.

 

A new Guildhall was completed on the Sandhill next to the river in 1655, replacing an earlier facility damaged by fire in 1639, and became the meeting place of Newcastle Town Council. In 1681 the Hospital of the Holy Jesus was built partly on the site of the Austin Friars. The Guildhall and Holy Jesus Hospital still exist.

 

Charles II tried to impose a charter on Newcastle to give the king the right to appoint the mayor, sheriff, recorder and town clerk. Charles died before the charter came into effect. In 1685, James II tried to replace Corporation members with named Catholics. However, James' mandate was suspended in 1689 after the Glorious Revolution welcoming William of Orange. In 1689, after the fall of James II, the people of Newcastle tore down his bronze equestrian statue in Sandhill and tossed it into the Tyne. The bronze was later used to make bells for All Saints Church.

 

In 1689 the Lort Burn was covered over. At this time it was an open sewer. The channel followed by the Lort Burn became the present day Dean Street. At that time, the centre of Newcastle was still the Sandhill area, with many merchants living along the Close or on the Side. The path of the main road through Newcastle ran from the single Tyne bridge, through Sandhill to the Side, a narrow street which climbed steeply on the north-east side of the castle hill until it reached the higher ground alongside St Nicholas' Church. As Newcastle developed, the Side became lined with buildings with projecting upper stories, so that the main street through Newcastle was a narrow, congested, steep thoroughfare.

 

In 1701 the Keelmen's Hospital was built in the Sandgate area of the city, using funds provided by the keelmen. The building still stands today.

 

Eighteenth century

In the 18th century, Newcastle was the country's largest print centre after London, Oxford and Cambridge, and the Literary and Philosophical Society of 1793, with its erudite debates and large stock of books in several languages predated the London Library by half a century.

 

In 1715, during the Jacobite rising in favour of the Old Pretender, an army of Jacobite supporters marched on Newcastle. Many of the Northumbrian gentry joined the rebels. The citizens prepared for its arrival by arresting Jacobite supporters and accepting 700 extra recruits into the local militia. The gates of the city were closed against the rebels. This proved enough to delay an attack until reinforcements arrived forcing the rebel army to move across to the west coast. The rebels finally surrendered at Preston.

 

In 1745, during a second Jacobite rising in favour of the Young Pretender, a Scottish army crossed the border led by Bonnie Prince Charlie. Once again Newcastle prepared by arresting Jacobite supporters and inducting 800 volunteers into the local militia. The town walls were strengthened, most of the gates were blocked up and some 200 cannon were deployed. 20,000 regulars were billeted on the Town Moor. These preparations were enough to force the rebel army to travel south via the west coast. They were eventually defeated at Culloden in 1746.

 

Newcastle's actions during the 1715 rising in resisting the rebels and declaring for George I, in contrast to the rest of the region, is the most likely source of the nickname 'Geordie', applied to people from Tyneside, or more accurately Newcastle. Another theory, however, is that the name 'Geordie' came from the inventor of the Geordie lamp, George Stephenson. It was a type of safety lamp used in mining, but was not invented until 1815. Apparently the term 'German Geordie' was in common use during the 18th century.

 

The city's first hospital, Newcastle Infirmary opened in 1753; it was funded by public subscription. A lying-in hospital was established in Newcastle in 1760. The city's first public hospital for mentally ill patients, Wardens Close Lunatic Hospital was opened in October 1767.

 

In 1771 a flood swept away much of the bridge at Newcastle. The bridge had been built in 1250 and repaired after a flood in 1339. The bridge supported various houses and three towers and an old chapel. A blue stone was placed in the middle of the bridge to mark the boundary between Newcastle and the Palatinate of Durham. A temporary wooden bridge had to be built, and this remained in use until 1781, when a new stone bridge was completed. The new bridge consisted of nine arches. In 1801, because of the pressure of traffic, the bridge had to be widened.

 

A permanent military presence was established in the city with the completion of Fenham Barracks in 1806. The facilities at the Castle for holding assizes, which had been condemned for their inconvenience and unhealthiness, were replaced when the Moot Hall opened in August 1812.

 

Victorian period

Present-day Newcastle owes much of its architecture to the work of the builder Richard Grainger, aided by architects John Dobson, Thomas Oliver, John and Benjamin Green and others. In 1834 Grainger won a competition to produce a new plan for central Newcastle. He put this plan into effect using the above architects as well as architects employed in his own office. Grainger and Oliver had already built Leazes Terrace, Leazes Crescent and Leazes Place between 1829 and 1834. Grainger and Dobson had also built the Royal Arcade at the foot of Pilgrim Street between 1830 and 1832. The most ambitious project covered 12 acres 12 acres (49,000 m2) in central Newcastle, on the site of Newe House (also called Anderson Place). Grainger built three new thoroughfares, Grey Street, Grainger Street and Clayton Street with many connecting streets, as well as the Central Exchange and the Grainger Market. John Wardle and George Walker, working in Grainger's office, designed Clayton Street, Grainger Street and most of Grey Street. Dobson designed the Grainger Market and much of the east side of Grey Street. John and Benjamin Green designed the Theatre Royal at the top of Grey Street, where Grainger placed the column of Grey's Monument as a focus for the whole scheme. Grey Street is considered to be one of the finest streets in the country, with its elegant curve. Unfortunately most of old Eldon Square was demolished in the 1960s in the name of progress. The Royal Arcade met a similar fate.

 

In 1849 a new bridge was built across the river at Newcastle. This was the High Level Bridge, designed by Robert Stephenson, and slightly up river from the existing bridge. The bridge was designed to carry road and rail traffic across the Tyne Gorge on two decks with rail traffic on the upper deck and road traffic on the lower. The new bridge meant that traffic could pass through Newcastle without having to negotiate the steep, narrow Side, as had been necessary for centuries. The bridge was opened by Queen Victoria, who one year later opened the new Central Station, designed by John Dobson. Trains were now able to cross the river, directly into the centre of Newcastle and carry on up to Scotland. The Army Riding School was also completed in 1849.

 

In 1854 a large fire started on the Gateshead quayside and an explosion caused it to spread across the river to the Newcastle quayside. A huge conflagration amongst the narrow alleys, or 'chares', destroyed the homes of 800 families as well as many business premises. The narrow alleys that had been destroyed were replaced by streets containing blocks of modern offices.

 

In 1863 the Town Hall in St Nicholas Square replaced the Guildhall as the meeting place of Newcastle Town Council.

 

In 1876 the low level bridge was replaced by a new bridge known as the Swing Bridge, so called because the bridge was able to swing horizontally on a central axis and allow ships to pass on either side. This meant that for the first time sizeable ships could pass up-river beyond Newcastle. The bridge was built and paid for by William Armstrong, a local arms manufacturer, who needed to have warships access his Elswick arms factory to fit armaments to them. The Swing Bridge's rotating mechanism is adapted from the cannon mounts developed in Armstrong's arms works. In 1882 the Elswick works began to build ships as well as to arm them. The Barrack Road drill hall was completed in 1890.

 

Industrialisation

In the 19th century, shipbuilding and heavy engineering were central to the city's prosperity; and the city was a powerhouse of the Industrial Revolution. Newcastle's development as a major city owed most to its central role in the production and export of coal. The phrase "taking coals to Newcastle" was first recorded in 1538; it proverbially denotes bringing a particular commodity to a place that has more than enough of it already.

 

Innovation in Newcastle and surrounding areas included the following:

 

George Stephenson developed a miner's safety lamp at the same time that Humphry Davy developed a rival design. The lamp made possible the opening up of ever deeper mines to provide the coal that powered the industrial revolution.

George and his son Robert Stephenson were hugely influential figures in the development of the early railways. George developed Blücher, a locomotive working at Killingworth colliery in 1814, whilst Robert was instrumental in the design of Rocket, a revolutionary design that was the forerunner of modern locomotives. Both men were involved in planning and building railway lines, all over this country and abroad.

 

Joseph Swan demonstrated a working electric light bulb about a year before Thomas Edison did the same in the USA. This led to a dispute as to who had actually invented the light bulb. Eventually the two rivals agreed to form a mutual company between them, the Edison and Swan Electric Light Company, known as Ediswan.

 

Charles Algernon Parsons invented the steam turbine, for marine use and for power generation. He used Turbinia, a small, turbine-powered ship, to demonstrate the speed that a steam turbine could generate. Turbinia literally ran rings around the British Fleet at a review at Spithead in 1897.

 

William Armstrong invented a hydraulic crane that was installed in dockyards up and down the country. He then began to design light, accurate field guns for the British army. These were a vast improvement on the existing guns that were then in use.

 

The following major industries developed in Newcastle or its surrounding area:

 

Glassmaking

A small glass industry existed in Newcastle from the mid-15th century. In 1615 restrictions were put on the use of wood for manufacturing glass. It was found that glass could be manufactured using the local coal, and so a glassmaking industry grew up on Tyneside. Huguenot glassmakers came over from France as refugees from persecution and set up glasshouses in the Skinnerburn area of Newcastle. Eventually, glass production moved to the Ouseburn area of Newcastle. In 1684 the Dagnia family, Sephardic Jewish emigrants from Altare, arrived in Newcastle from Stourbridge and established glasshouses along the Close, to manufacture high quality flint glass. The glass manufacturers used sand ballast from the boats arriving in the river as the main raw material. The glassware was then exported in collier brigs. The period from 1730 to 1785 was the highpoint of Newcastle glass manufacture, when the local glassmakers produced the 'Newcastle Light Baluster'. The glassmaking industry still exists in the west end of the city with local Artist and Glassmaker Jane Charles carrying on over four hundred years of hot glass blowing in Newcastle upon Tyne.

 

Locomotive manufacture

In 1823 George Stephenson and his son Robert established the world's first locomotive factory near Forth Street in Newcastle. Here they built locomotives for the Stockton and Darlington Railway and the Liverpool and Manchester Railway, as well as many others. It was here that the famous locomotive Rocket was designed and manufactured in preparation for the Rainhill Trials. Apart from building locomotives for the British market, the Newcastle works also produced locomotives for Europe and America. The Forth Street works continued to build locomotives until 1960.

 

Shipbuilding

In 1296 a wooden, 135 ft (41 m) long galley was constructed at the mouth of the Lort Burn in Newcastle, as part of a twenty-ship order from the king. The ship cost £205, and is the earliest record of shipbuilding in Newcastle. However the rise of the Tyne as a shipbuilding area was due to the need for collier brigs for the coal export trade. These wooden sailing ships were usually built locally, establishing local expertise in building ships. As ships changed from wood to steel, and from sail to steam, the local shipbuilding industry changed to build the new ships. Although shipbuilding was carried out up and down both sides of the river, the two main areas for building ships in Newcastle were Elswick, to the west, and Walker, to the east. By 1800 Tyneside was the third largest producer of ships in Britain. Unfortunately, after the Second World War, lack of modernisation and competition from abroad gradually caused the local industry to decline and die.

 

Armaments

In 1847 William Armstrong established a huge factory in Elswick, west of Newcastle. This was initially used to produce hydraulic cranes but subsequently began also to produce guns for both the army and the navy. After the Swing Bridge was built in 1876 allowing ships to pass up river, warships could have their armaments fitted alongside the Elswick works. Armstrong's company took over its industrial rival, Joseph Whitworth of Manchester in 1897.

 

Steam turbines

Charles Algernon Parsons invented the steam turbine and, in 1889, founded his own company C. A. Parsons and Company in Heaton, Newcastle to make steam turbines. Shortly after this, he realised that steam turbines could be used to propel ships and, in 1897, he founded a second company, Parsons Marine Steam Turbine Company in Wallsend. It is there that he designed and manufactured Turbinia. Parsons turbines were initially used in warships but soon came to be used in merchant and passenger vessels, including the liner Mauretania which held the blue riband for the Atlantic crossing until 1929. Parsons' company in Heaton began to make turbo-generators for power stations and supplied power stations all over the world. The Heaton works, reduced in size, remains as part of the Siemens AG industrial giant.

 

Pottery

In 1762 the Maling pottery was founded in Sunderland by French Huguenots, but transferred to Newcastle in 1817. A factory was built in the Ouseburn area of the city. The factory was rebuilt twice, finally occupying a 14-acre (57,000 m2) site that was claimed to be the biggest pottery in the world and which had its own railway station. The pottery pioneered use of machines in making potteries as opposed to hand production. In the 1890s the company went up-market and employed in-house designers. The period up to the Second World War was the most profitable with a constant stream of new designs being introduced. However, after the war, production gradually declined and the company closed in 1963.

 

Expansion of the city

Newcastle was one of the boroughs reformed by the Municipal Corporations Act 1835: the reformed municipal borough included the parishes of Byker, Elswick, Heaton, Jesmond, Newcastle All Saints, Newcastle St Andrew, Newcastle St John, Newcastle St Nicholas, and Westgate. The urban districts of Benwell and Fenham and Walker were added in 1904. In 1935, Newcastle gained Kenton and parts of the parishes of West Brunton, East Denton, Fawdon, Longbenton. The most recent expansion in Newcastle's boundaries took place under the Local Government Act 1972 on 1 April 1974, when Newcastle became a metropolitan borough, also including the urban districts of Gosforth and Newburn, and the parishes of Brunswick, Dinnington, Hazlerigg, North Gosforth and Woolsington from the Castle Ward Rural District, and the village of Westerhope.

 

Meanwhile Northumberland County Council was formed under the Local Government Act 1888 and benefited from a dedicated meeting place when County Hall was completed in the Castle Garth area of Newcastle in 1910. Following the Local Government Act 1972 County Hall relocated to Morpeth in April 1981.

 

Twentieth century

In 1925 work began on a new high-level road bridge to span the Tyne Gorge between Newcastle and Gateshead. The capacity of the existing High-Level Bridge and Swing Bridge were being strained to the limit, and an additional bridge had been discussed for a long time. The contract was awarded to the Dorman Long Company and the bridge was finally opened by King George V in 1928. The road deck was 84 feet (26 m) above the river and was supported by a 531 feet (162 m) steel arch. The new Tyne Bridge quickly became a symbol for Newcastle and Tyneside, and remains so today.

 

During the Second World War, Newcastle was largely spared the horrors inflicted upon other British cities bombed during the Blitz. Although the armaments factories and shipyards along the River Tyne were targeted by the Luftwaffe, they largely escaped unscathed. Manors goods yard and railway terminal, to the east of the city centre, and the suburbs of Jesmond and Heaton suffered bombing during 1941. There were 141 deaths and 587 injuries, a relatively small figure compared to the casualties in other industrial centres of Britain.

 

In 1963 the city gained its own university, the University of Newcastle upon Tyne, by act of parliament. A School of Medicine and Surgery had been established in Newcastle in 1834. This eventually developed into a college of medicine attached to Durham University. A college of physical science was also founded and became Armstrong College in 1904. In 1934 the two colleges merged to become King's College, Durham. This remained as part of Durham University until the new university was created in 1963. In 1992 the city gained its second university when Newcastle Polytechnic was granted university status as Northumbria University.

 

Newcastle City Council moved to the new Newcastle Civic Centre in 1968.

 

As heavy industries declined in the second half of the 20th century, large sections of the city centre were demolished along with many areas of slum housing. The leading political figure in the city during the 1960s was T. Dan Smith who oversaw a massive building programme of highrise housing estates and authorised the demolition of a quarter of the Georgian Grainger Town to make way for Eldon Square Shopping Centre. Smith's control in Newcastle collapsed when it was exposed that he had used public contracts to advantage himself and his business associates and for a time Newcastle became a byword for civic corruption as depicted in the films Get Carter and Stormy Monday and in the television series Our Friends in the North. However, much of the historic Grainger Town area survived and was, for the most part, fully restored in the late 1990s. Northumberland Street, initially the A1, was gradually closed to traffic from the 1970s and completely pedestrianised by 1998.

 

In 1978 a new rapid transport system, the Metro, was built, linking the Tyneside area. The system opened in August 1980. A new bridge was built to carry the Metro across the river between Gateshead and Newcastle. This was the Queen Elizabeth II Bridge, commonly known as the Metro Bridge. Eventually the Metro system was extended to reach Newcastle Airport in 1991, and in 2002 the Metro system was extended to the nearby city of Sunderland.

 

As the 20th century progressed, trade on the Newcastle and Gateshead quaysides gradually declined, until by the 1980s both sides of the river were looking rather derelict. Shipping company offices had closed along with offices of firms related to shipping. There were also derelict warehouses lining the riverbank. Local government produced a master plan to re-develop the Newcastle quayside and this was begun in the 1990s. New offices, restaurants, bars and residential accommodation were built and the area has changed in the space of a few years into a vibrant area, partially returning the focus of Newcastle to the riverside, where it was in medieval times.

 

The Gateshead Millennium Bridge, a foot and cycle bridge, 26 feet (7.9 m) wide and 413 feet (126 m) long, was completed in 2001. The road deck is in the form of a curve and is supported by a steel arch. To allow ships to pass, the whole structure, both arch and road-deck, rotates on huge bearings at either end so that the road deck is lifted. The bridge can be said to open and shut like a human eye. It is an important addition to the re-developed quayside area, providing a vital link between the Newcastle and Gateshead quaysides.

 

Recent developments

Today the city is a vibrant centre for office and retail employment, but just a short distance away there are impoverished inner-city housing estates, in areas originally built to provide affordable housing for employees of the shipyards and other heavy industries that lined the River Tyne. In the 2010s Newcastle City Council began implementing plans to regenerate these depressed areas, such as those along the Ouseburn Valley.

Towards the end of 1914, early in World War I, disturbing rumours began to circulate that the newest German submarines were capable of a much higher surface speed than British boats, one report giving their speed at about 22 knots. The rumours were sufficiently strong to force serious consideration of the matter by the Admiralty, and at the same time consideration was given to the idea that submarines should have a high enough surface speed to be able to work with the fleet. The reports concerning the speed of the German submarines proved to be spurious, but the idea of a British submarine with a high surface speed gained ground. The immediate result of this concern was the development of the J Class, which were unique with their three shafts. Originally eight boats were planned but this was reduced to six and then increased to seven. As a result of these changes the boats originally intended to be J7 and J8 were renumbered in April 1915 as J3 and J4 respectively.

 

J7's submerged displacement of 1,760 tons was 60 tons less than that of her sister boats. Her conning tower was located further aft and the gun was mounted in a lower position.

 

HMS J7 commissioned in the Royal Navy on 15 September 1917 under the command of Lieutenant Commander F.H.D. Byron RN and was allocated to a flotilla based at Blyth, Northumberland.

 

On 5 November 1917 J7 departed Blyth for her first patrol. Whilst on patrol in the North Sea on 6 March 1918 an enemy submarine was sighted, but J7 was unable to attack and the enemy passed from sight.

 

The submarine was under refit during April and May 1918 at Walker Naval Yard on the River Tyne. She sailed for patrol on 25 May and evaded a U-boat attack the same day.

 

On 10 July an enemy submarine was sighted and both vessels dived. Shortly after a sighting was made of an enemy submarine on the surface, going away, J7 surfaced, challenged and opened fire. The enemy dived. An enemy submarine was sighted on 23 July, but J7 was unable to attack and the enemy disappeared.

 

On 5 October 1918 J7 dived to intercept a reported submarine, but broke off the search without contact.

 

The boat was at sea when the Armistice was signed on 11 November 1918. She returned to Blyth on 15 November. On 19 February 1919 she proceeded to Jarrow.

 

Following the conclusion of hostilities in World War I, the Admiralty in 1918 presented the six remaining boats of the J Class to the Australian Government - J6 had been sunk in error in 1918 by a British ship. All the submarines commissioned into the Royal Australian Navy at Portsmouth on 25 March 1919, as tenders to the submarine depot ship HMAS Platypus, J7 being the senior boat, under the command of Lieutenant Commander Oswald E. Hallifax DSO RN.

 

The beam tubes were removed from all six J Class submarines before they sailed for Australia. The tubes were despatched separately to Garden Island. The reasons given for the removal were that the beam tubes were not a success and that increased accommodation was required.

  

HMS Submarine J7 off the River Tyne prior to sailing for Australia in February, 1919.

On 9 April 1919 Platypus and the submarines, escorted by the light cruiser HMAS Sydney, sailed from Portsmouth for Australia, their first two ports of call being Gibraltar and Valetta.

 

On the night of 28 April, the night before the vessels arrived at Port Said, J3's starboard main engine shaft snapped. Thus handicapped she could not keep up with the others and consequently on departure for Aden on 30 April, J3 was in tow of Sydney.

 

The vessels arrived at Aden on 5 May. On the same day the light cruiser HMAS Brisbane, which had left Portsmouth on 17 April, also arrived. On 7 May all the vessels sailed for Colombo. Brisbane took over the tow of J3 while Sydney took J5 in tow as that boat had also developed engine trouble. Three days after arrival at Colombo on 15 May, Brisbane sailed with J5 in tow, taking her all the way to Sydney, where they arrived on 27 June.

 

J3 was taken in hand at Colombo for repairs. On 31 May Sydney, J1, J2, J4 and J7 sailed for Singapore, followed on 2 June by Platypus and J3. The vessels were reunited at Singapore from where all except Sydney sailed on 18 June. Sydney sailed for Australia a few days later but did not rejoin the other vessels. On 29 June Platypus and the five submarines arrived at Thursday Island, although J7 was three hours late because of trouble with her engine lubricating system. The last call before Sydney was Brisbane, Sydney being reached on 15 July.

 

Having arrived in poor condition, the submarines were taken in hand at Garden Island Dockyard for refitting. After her refit was completed J7 sailed for the submarine base at Geelong, Victoria.

 

After uneventful service, little of which was spent at sea, J7 and her five sisters paid off into Reserve at Westernport on 12 July 1922. The boats had become victims of the worsening economic conditions of the time, coupled with their high cost of maintenance.

 

On 1 November 1929 J7 was sold to Morris and Watt Pty Ltd of South Melbourne. She was towed from Flinders Naval Depot, Crib Point, where she had served as a reserve source of electric power, on 4 December 1929. She was dismantled and the hull sunk in 1930 as a breakwater at the Sandringham Yacht Club, Sandringham, Port Phillip Bay, where it remain

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based on historical facts. BEWARE!

  

Some Background:

The Lockheed F-94 Starfire was a first-generation jet aircraft of the United States Air Force. It was developed from the twin-seat Lockheed T-33 Shooting Star in the late 1940s as an all-weather, day/night interceptor, replacing the propeller-driven North American F-82 Twin Mustang in this role. The system was designed to overtake the F-80 in terms of performance, but more so to intercept the new high-level Soviet bombers capable of nuclear attacks on America and her Allies - in particular, the new Tupelov Tu-4. The F-94 was furthermore the first operational USAF fighter equipped with an afterburner and was the first jet-powered all-weather fighter to enter combat during the Korean War in January 1953.

 

The initial production model, the F-94A, entered operational service in May 1950. Its armament consisted of four 0.50 in (12.7 mm) M3 Browning machine guns mounted in the fuselage with the muzzles exiting under the radome for the APG-33 radar, a derivative from the AN/APG-3, which directed the Convair B-36's tail guns and had a range of up to 20 miles (32 km). Two 165 US Gallon (1,204 litre) drop tanks, as carried by the F-80 and T-33, were carried on the wingtips. Alternatively, these could be replaced by a pair of 1,000 lb (454 kg) bombs under the wings, giving the aircraft a secondary fighter bomber capability. 109 were produced.

 

The subsequent F-94B, which entered service in January 1951, was outwardly virtually identical to the F-94A. Its Allison J33 turbojet had a number of modifications made, though, which made it a very reliable engine. The pilot was provided with a roomier cockpit and the canopy received a bow frame in the center between the two crew members. A new Instrument Landing System (ILS) was fitted, too, which made operations at night and/or in bad weather much safer. However, this new variant’s punch with just four machine guns remained weak, and, to improve the load of fire, wing-mounted pods with two additional pairs of 0.5” machine guns were introduced – but these hardly improved the interceptor’s effectiveness. 356 of the F-94B were nevertheless built.

 

The following F-94C was extensively modified and initially designated F-97, but it was ultimately decided just to treat it as a new version of the F-94. USAF interest was lukewarm since aircraft technology had already developed at a fast pace – supersonic performance had already become standard. Lockheed funded development themselves, converting two F-94B airframes to YF-94C prototypes for evaluation with a completely new, much thinner wing, a swept tail surface and a more powerful Pratt & Whitney J48. This was a license-built version of the afterburning Rolls-Royce Tay, which produced a dry thrust of 6,350 pounds-force (28.2 kN) and approximately 8,750 pounds-force (38.9 kN) with afterburning. Instead of machine guns, the proposed new variant was exclusively armed with unguided air-to-air missiles.

Tests were positive and eventually the F-94C was adopted for USAF service, since it was the best interim solution for an all-weather fighter at that time. It still had to rely on Ground Control Interception Radar (GCI) sites to vector the interceptor to intruding aircraft, though.

 

The F-94C's introduction and the availability of the more effective Northrop F-89C/D Scorpion and the North American F-86D Sabre interceptors led to a quick relegation of the earlier F-94 variants from mid-1954 onwards to second line units and to Air National Guards. By 1955 most of them had already been phased out of USAF service, and some of these relatively young surplus machines were subsequently exported or handed over to friendly nations, too. When sent to the ANG, the F-94As were modified by Lockheed to F-94B standards and then returned to the ANG as B models. They primarily replaced outdated F-80C Shooting Stars and F-51D/H Mustangs.

 

At that time the USAF was looking for a tactical reconnaissance aircraft, a more effective successor for the RF-80A which had shown its worth and weaknesses during the Korea War. For instance, the plane could not fly at low altitude long enough to perform suitable visual reconnaissance, and its camera equipment was still based on WWII standards. Lockheed saw the opportunity to fill this operational gap with conversions of existing F-94A/B airframes, which had, in most cases, only had clocked few flying hours, primarily at high altitudes where Soviet bombers were expected to lurk, and still a lot of airframe life to offer. This led to another private venture, the RF-94B, auspiciously christened “Stargazer”.

 

The RF-94B was based on the F-94B interceptor with its J33 engine and the original unswept tail. The F-94B’s wings were retained but received a different leading-edge profile to better cope with operations at low altitude. The interceptor’s nose with the radome and the machine guns underneath was replaced by a new all-metal nose cone, which was more than 3 feet longer than the former radar nose, with windows for several sets of cameras; the wedge-shaped nose cone quickly earned the aircraft the unofficial nickname “Crocodile”.

One camera was looking ahead into flight direction and could be mounted at different angled downward (but not moved during flight), followed by two oblique cameras, looking to the left and the right, and a vertical camera as well as a long-range camera focussed on the horizon, which was behind a round window at port side. An additional, spacious compartment in front of the landing gear well held an innovative Tri-Metrogen horizon-to-horizon view system that consisted of three synchronized cameras. Coupled with a computerized control system based on light, speed, and altitude, it adjusted camera settings to produce pictures with greater delineation.

All cameras could be triggered individually by pilot or a dedicated observer/camera systems operator in the 2nd seat. Talking into a wire recorder, the crew could describe ground movements that might not have appeared in still pictures. A vertical view finder with a periscopic presentation on the cockpit panel was added for the pilot to enhance visual reconnaissance and target identification directly under the aircraft. Using magnesium flares carried under its wings in flash-ejector cartridges, the RF-94B was furthermore able to fly night missions.

The RF-94B was supposed to operate unarmed, but it could still carry a pair of 1.000 lb bombs under its wings or, thanks to added plumbings, an extra pair of drop tanks for ferry flights. The F-94A/B’s machine gun pods as well as the F-94C’s unguided missile launchers could be mounted to the wings, too, making it a viable attack aircraft in a secondary role.

 

The USAF was highly interested in this update proposal for the outdated interceptors (almost 500 F-94A/Bs had been built) and ordered 100 RF-94B conversions with an option for 100 more – just when a severe (and superior) competitor entered the stage after a lot of development troubles: Republic’s RF-84F Thunderflash reconnaissance version. The first YRF-84F had already been completed in February 1952 and it had an overall slightly better performance than the RF-94B. However, it offered more internal space for reconnaissance systems and was able to carry up to fifteen cameras with the support of many automatized systems, so that it was a single seater. Being largely identical to the F-84F and sharing its technical and logistical infrastructures, the USAF decided on short notice to change its procurement decision and rather adopt the more modern and promising Thunderflash as its standard tactical reconnaissance aircraft. The RF-94B conversion order was reduced to the initial 100 aircraft, and to avoid operational complexity these aircraft were exclusively delivered to Air National Guardss that had experience with the F-94A/B to replace their obsolete RF-80As.

 

Gradual replacement lasted until 1958, and while the RF-94B’s performance was overall better than the RF-80A’s, it was still disappointing and not the expected tactical intelligence gathering leap forward. The airframe did not cope well with constant low-level operations, and the aircraft’s marginal speed and handling did not ensure its survivability. However, unlike the RF-84F, which suffered from frequent engine problems, the Stargazers’ J33 made them highly reliable platforms – even though the complex Tri-Metrogen device turned out to be capricious, so that it was soon replaced with up to three standard cameras.

 

For better handling and less drag esp. at low altitude, the F-94B’s large Fletcher type wingtip tanks were frequently replaced with smaller ones with about half capacity. It also became common practice to operate the RF-94Bs with only a crew of one, and from 1960 on the RF-94B was, thanks to its second seat, more and more used as a trainer before pilots mounted more potent reconnaissance aircraft like the RF-101 Voodoo, which eventually replaced the RF-94B in ANG service. The last RF-94B was phased out in 1968, and, unlike the RF-84F, it was not operated by any foreign air force.

  

General characteristics:

Crew: 2 (but frequently operated by a single pilot)

Length: 43 ft 4 3/4 in (13.25 m)

Wingspan (with tip tanks): 40 ft 9 1/2 in (12.45 m)

Height: 12 ft. 2 (3.73 m)

Wing area: 234' 8" sq ft (29.11 m²)

Empty weight: 10,064 lb (4,570 kg)

Loaded weight: 15,330 lb (6,960 kg)

Max. takeoff weight: 24,184 lb (10,970 kg)

 

Powerplant:

1× Allison J33-A-33 turbojet, rated at 4,600 lbf (20.4 kN) continuous thrust,

5,400 lbf (24 kN) with water injection and 6,000 lbf (26.6 kN) thrust with afterburner

 

Performance:

Maximum speed: 630 mph (1,014 km/h) at height and in level flight

Range: 930 mi (813 nmi, 1,500 km) in combat configuration with two drop tanks

Ferry range: 1,457 mi (1,275 nmi, 2,345 km)

Service ceiling: 42,750 ft (14,000 m)

Rate of climb: 6,858 ft/min (34.9 m/s)

Wing loading: 57.4 lb/ft² (384 kg/m²)

Thrust/weight: 0.48

 

Armament:

No internal guns; 2x 165 US Gallon (1,204 liter) drop tanks on the wing tips and…

2x underwing hardpoints for two additional 165 US Gallon (1,204 liter) ferry tanks

or bombs of up to 1.000 lb (454 kg) caliber each, plus…

2x optional (rarely fitted) pods on the wings’ leading edges with either a pair of 0.5" (12.7 mm)

machine guns or twelve 2.75” (70 mm) Mk 4/Mk 40 Folding-Fin Aerial Rockets each

  

The kit and its assembly:

This project was originally earmarked as a submission for the 2021 “Reconnaissance & Surveillance” group build at whatifmodellers.com, in the form of a Heller F-94B with a new nose section. The inspiration behind this build was the real-world EF-94C (s/n 50-963): a solitary conversion with a bulbous camera nose. However, the EF-94C was not a reconnaissance aircraft but rather a chase plane/camera ship for the Air Research and Development Command, hence its unusual designation with the suffix “E”, standing for “Exempt” instead of the more appropriate “R” for a dedicated recce aircraft. There also was another EF-94C, but this was a totally different kind of aircraft: an ejection seat testbed.

 

I had a surplus Heller F-94B kit in The Stash™ and it was built almost completely OOB and did – except for some sinkholes and standard PSR work – not pose any problem. In fact, the old Heller Starfire model is IMHO a pretty good representation of the aircraft. O.K., its age might show, but almost anything you could ask for at 1:72 scale is there, including a decent, detailed cockpit.

 

The biggest change was the new camera nose, and it was scratched from an unlikely donor part: it consists of a Matchbox B-17G tail gunner station, slimmed down by the gunner station glazing's width at the seam in the middle, and this "sandwich" was furthermore turned upside down. Getting the transitional sections right took lots of PSR, though, and I added some styrene profiles to integrate the new nose into the rest of the hull. It was unintentional, but the new nose profile reminds a lot of a RF-101 recce Voodoo, and there's, with the straight wings, a very F-89ish look to the aircraft now? There's also something F2H-2ish about the outlines?

 

The large original wing tip tanks were cut off and replaced with smaller alternatives from a Hasegawa A-37. Because it was easy to realize on this kit I lowered the flaps, together with open ventral air brakes. The cockpit was taken OOB, I just modified the work station on the rear seat and replaced the rubber sight protector for the WSO with two screens for a camera operator. Finally, the one-piece cockpit glazing was cut into two parts to present the model with an open canopy.

  

Painting and markings:

This was a tough decision: either an NMF finish (the natural first choice), an overall light grey anti-corrosive coat of paint, both with relatively colorful unit markings, or camouflage. The USAF’s earlier RF-80As carried a unique scheme in olive drab/neutral grey with a medium waterline, but that would look rather vintage on the F-94. I decided that some tactical camouflage would make most sense on this kind of aircraft and eventually settled for the USAF’s SEA scheme with reduced tactical markings, which – after some field tests and improvisations in Vietnam – became standardized and was officially introduced to USAF aircraft around 1965 as well as to ANG units.

 

Even though I had already built a camouflaged F-94 some time ago (a Hellenic aircraft in worn SEA colors), I settled for this route. The basic colors (FS 30219, 34227, 34279 and 36622) all came from Humbrol (118, 117, 116 and 28, respectively), and for the pattern I adapted the paint scheme of the USAF’s probably only T-33 in SEA colors: a trainer based on Iceland during the Seventies and available as a markings option in one of the Special Hobby 1:32 T-33 kits. The low waterline received a wavy shape, inspired by an early ANG RF-101 in SEA camouflage I came across in a book. The new SEA scheme was apparently applied with a lot of enthusiasm and properness when it was brand new, but this quickly vaned. As an extra, the wing tip tanks received black anti-glare sections on their inner faces and a black anti-glare panel was added in front of the windscreen - a decal from a T-33 aftermarket sheet. Beyond a black ink wash the model received some subtle panel post-shading, but rather to emphasize surface details than for serious weathering.

 

The cockpit became very dark grey (Revell 06) while the landing gear wells were kept in zinc chromate green primer (Humbrol 80, Grass Green), with bright red (Humbrol 60, Matt Red) cover interiors and struts and wheels in aluminum (Humbrol 56). The interior of the flaps and the ventral air brakes became red, too.

 

The decals/markings came from a Special Hobby 1:72 F-86H; there’s a dedicated ANG boxing of the kit that comes with an optional camouflaged aircraft of the NY ANG, the least unit to operate the “Sabre Hog” during the Seventies. Since this 138th TFS formerly operated the F-94A/B, it was a perfect option for the RF-94B! I just used a different Bu. No. code on the fin, taken from a PrintScale A/T-37 set, and most stencils were perocured from the scrap box.

After a final light treatment with graphite around the afterburner for a more metallic shine of the iron metallic (Revell 97) underneath, the kit was sealed with a coat of matt acrylic varnish (Italeri).

  

A camouflaged F-94 is an unusual sight, but it works very well. The new/longer nose considerably changes the aircraft's profile, and even though the change is massive, the "Crocodile" looks surprisingly plausible, if not believable! And, despite the long nose, the aircraft looks pretty sleek, especially in the air.

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based on historical facts. BEWARE!

  

Some background:

The Grumman Mohawk began as a joint Army-Marine program through the then-Navy Bureau of Aeronautics (BuAer), for an observation/attack plane that would outperform the light and vulnerable Cessna L-19 Bird Dog. In June 1956, the Army issued Type Specification TS145, which called for the development and procurement of a two-seat, twin turboprop aircraft designed to operate from small, unimproved fields under all weather conditions. It would be faster, with greater firepower, and heavier armor than the Bird Dog, which had proved very vulnerable during the Korean War.

 

The Mohawk's mission would include observation, artillery spotting, air control, emergency resupply, naval target spotting, liaison, and radiological monitoring. The Navy specified that the aircraft had to be capable of operating from small "jeep" escort class carriers (CVEs). The DoD selected Grumman Aircraft Corporation's G-134 design as the winner of the competition in 1957. Marine requirements contributed an unusual feature to the design: since the Marines were authorized to operate fixed-wing aircraft in the close air support (CAS) role, the mockup featured underwing pylons for rockets, bombs, and other stores, and this caused a lot of discord. The Air Force did not like the armament capability of the Mohawk and tried to get it removed. On the other side, the Marines did not want the sophisticated sensors the Army wanted, so when their Navy sponsors opted to buy a fleet oil tanker, they eventually dropped from the program altogether. The Army continued with armed Mohawks (and the resulting competence controversy with the Air Force) and also developed cargo pods that could be dropped from underwing hard points to resupply troops in emergencies.

 

In mid-1961, the first Mohawks to serve with U.S. forces overseas were delivered to the 7th Army at Sandhofen Airfield near Mannheim, Germany. Before its formal acceptance, the camera-carrying AO-1AF was flown on a tour of 29 European airfields to display it to the U.S. Army field commanders and potential European customers. In addition to their Vietnam and European service, SLAR-equipped Mohawks began operational missions in 1963 patrolling the Korean Demilitarized Zone.

 

Germany and France showed early interest in the Mohawk, and two OV-1s were field-tested by both nations over the course of several months. No direct orders resulted, though, but the German Bundesheer (Army) was impressed by the type’s performance and its capability as an observation and reconnaissance platform. Grumman even signed a license production agreement with the French manufacturer Breguet Aviation in exchange for American rights to the Atlantic maritime patrol aircraft, but no production orders followed.

 

This could have been the end of the OV-1 in Europe, but in 1977 the German government, primarily the interior ministry and its intelligence agency, the Bundesnachrichtendienst (BND), showed interest in a light and agile SIGINT/ELINT platform that could fly surveillance missions along the inner-German border to the GDR and also to Czechoslovakia. Beyond visual reconnaissance with cameras and IR sensors, the aircraft was to be specifically able to identify and locate secret radio stations that were frequently operated by Eastern Block agents (esp. by the GDR) all across Western Germany, but primarily close to the inner-German border due to the clandestine stations’ low power. The Bundeswehr already operated a small ELINT/ECM fleet, consisting of converted HFB 320 ‘Hansa’ business jets, but these were not suited for stealthy and inconspicuous low flight level missions that were envisioned, and they also lacked the ability to fly slowly enough to locate potential “radio nests”.

 

The pan and the objective were clear, but the ELINT project caused a long and severe political debate concerning the operator of such an aerial platform. Initially, the Bundesheer, who had already tested the OV-1, claimed responsibility, but the interior ministry in the form of the German customs department as well as the German police’s Federal Border Guard, the Bundesgrenzschutz and the Luftwaffe (the proper operator for fixed-wing aircraft within the German armed forces), wrestled for this competence. Internally, the debate and the project ran under the handle “Schimmelreiter” (literally “The Rider on the White Horse”), after a northern German legendary figure, which eventually became the ELINT system’s semi-official name after it had been revealed to the public. After much tossing, in 1979 the decision was made to procure five refurbished U.S. Army OV-1As, tailored to the German needs and – after long internal debates – operate them by the Luftwaffe.

 

The former American aircraft were hybrids: they still had the OV-1A’s original short wings, but already the OV-1D’s stronger engines and its internal pallet system for interchangeable electronics. The machines received the designation OV-1G (for Germany) and were delivered in early 1980 via ship without any sensors or cameras. These were of Western German origin, developed and fitted locally, tailored to the special border surveillance needs.

 

The installation and testing of the “Schimmelreiter” ELINT suite lasted until 1982. It was based on a Raytheon TI Systems emitter locator system, but it was locally adapted by AEG-Telefunken to the airframe and the Bundeswehr’s special tasks and needs. The system’s hardware was stowed in the fuselage, its sensor arrays were mounted into a pair of underwing nacelles, which occupied the OV-1’s standard hardpoints, allowing a full 360° coverage. In order to cool the electronics suite and regulate the climate in the internal equipment bays, the OV-1G received a powerful heat exchanger, mounted under a wedge-shaped fairing on the spine in front of the tail – the most obvious difference of this type from its American brethren. The exact specifications of the “Schimmelreiter” ELINT suite remained classified, but special emphasis was placed upon COMINT (Communications Intelligence), a sub-category of signals intelligence that engages in dealing with messages or voice information derived from the interception of foreign communications. Even though the “Schimmelreiter” suite was the OV-1Gs’ primary reconnaissance tool, the whole system could be quickly de-installed for other sensor packs and reconnaissance tasks (even though this never happened), or augmented by single modules, what made upgrades and mission specialization easy. Beyond the ELINT suite, the OV-1G could be outfitted with cameras and other sensors on exchangeable pallets in the fuselage, too. This typically included a panoramic camera in a wedge-shaped ventral fairing, which would visually document the emitter sensors’ recordings.

 

A special feature of the German OV-1s was the integration of a brand new, NATO-compatible “Link-16” data link system via a MIDS-LVT (Multifunctional Information Distribution System). Even though this later became a standard for military systems, the OV-1G broke the ground for this innovative technology. The MIDS was an advanced command, control, communications, computing and intelligence (C4I) system incorporating high-capacity, jam-resistant, digital communication links for exchange of near real-time tactical information, including both data and voice, among air, ground, and sea elements. Outwardly, the MIDS was only recognizable through a shallow antenna blister behind the cockpit.

 

Even though the OV-1Gs initially retained their former American uniform olive drab livery upon delivery and outfitting in German service, they soon received a new wraparound camouflage for their dedicated low-level role in green and black (Luftwaffe Norm 83 standard), which was better suited for the European theatre of operations. In Luftwaffe service, the OV-1Gs received the tactical codes 18+01-05 and the small fleet was allocated to the Aufklärungsgeschwader (AG) 51 “Immelmann”, where the machines formed, beyond two squadrons with RF-4E Phantom IIs, an independent 3rd squadron. This small unit was from the start based as a detachment at Lechfeld, located in Bavaria/Southern Germany, instead of AG 51’s home airbase Bremgarten in South-Western Germany, because Lechfeld was closer to the type’s typical theatre of operations along Western Germany’s Eastern borders. Another factor in favor of this different airbase was the fact that Lechfeld was, beyond Tornado IDS fighter bombers, also the home of the Luftwaffe’s seven HFB 320M ECM aircraft, operated by the JaBoG32’s 3rd squadron, so that the local maintenance crews were familiar with complex electronics and aircraft systems, and the base’s security level was appropriate, too.

 

With the end of the Cold War in 1990, the OV-1Gs role and field of operation gradually shifted further eastwards. With the inner-German Iron Curtain gone, the machines were now frequently operated along the Polish and Czech Republic border, as well as in international airspace over the Baltic Sea, monitoring the radar activities along the coastlines and esp. the activities of Russian Navy ships that operated from Kaliningrad and Saint Petersburg. For these missions, the machines were frequently deployed to the “new” air bases Laage and Holzdorf in Eastern Germany.

 

In American service, the OV-1s were retired from Europe in 1992 and from operational U.S. Army service in 1996. In Germany, the OV-1 was kept in service for a considerably longer time – with little problems, since the OV-1 airframes had relatively few flying hours on their clocks. The Luftwaffe’s service level for the aircraft was high and spare parts remained easy to obtain from the USA, and there were still OV-1 parts in USAF storage in Western German bases.

 

The German HFB 320M fleet was retired between 1993 and 1994 and, in part, replaced by the Tornado ECR. At the same time AG 51 was dissolved and the OV-1Gs were nominally re-allocated to JaboG 32/3. With this unit the OV-1Gs remained operational until 2010, undergoing constant updates and equipment changes. For instance, the machines received in 1995 a powerful FLIR sensor in a small turret in the aircraft’s nose, which improved the aircraft’s all-weather reconnaissance capabilities and was intended to spot hidden radio posts even under all-weather/night conditions, once their signal was recognized and located. The aircrafts’ radio emitter locator system was updated several times, too, and, as a passive defensive measure against heat-guided air-to-air missiles/MANPADS, an IR jammer was added, extending the fuselage beyond the tail. These machines received the suffix “Phase II”, even though all five aircraft were updated the same way.

Reports that the OV-1Gs were furthermore retrofitted with the avionics to mount and launch AIM-9 Sidewinder AAMs under the wing tips for self-defense remained unconfirmed, even more so because no aircraft was ever seen carrying arms – neither the AIM-9 nor anything else. Plans to make the OV-1Gs capable of carrying the Luftwaffe’s AGM-65 Maverick never went beyond the drawing board, either. However, BOZ chaff/flare dispenser pods and Cerberus ECM pods were occasionally seen on the ventral pylons from 1998 onwards.

 

No OV-1G was lost during the type’s career in Luftwaffe service, and after the end of the airframes’ service life, all five German OV-1Gs were scrapped in 2011. There was, due to worsening budget restraints, no direct successor, even though the maritime surveillance duties were taken over by Dornier Do 228/NGs operated by the German Marineflieger (naval air arm).

  

General characteristics:

Crew: Two: pilot, observer/systems operator

Length: 44 ft 4 in (13.53 m) overall with FLIR sensor and IR jammer

Wingspan: 42 ft 0 in (12.8 m)

Height: 12 ft 8 in (3.86 m)

Wing area: 330 sq. ft (30.65 m²)

Empty weight: 12,054 lb (5,467 kg)

Loaded weight: 15,544 lb (7,051 kg)

Max. takeoff weight: 18,109 lb (8,214 kg)

 

Powerplant:

2× Lycoming T53-L-701 turboprops, 1,400 shp (1,044 kW) each

 

Performance:

Never exceed speed: 450 mph (390 knots, 724 km/h)

Maximum speed: 305 mph (265 knots, 491 km/h) at 10,000 ft (3,050 m)

Cruise speed: 207 mph (180 knots, 334 km/h) (econ cruise)

Stall speed: 84 mph (73 knots, 135 km/h)

Range: 944 mi (820 nmi, 1,520 km) (SLAR mission)

Service ceiling: 25,000 ft (7,620 m)

Rate of climb: 3,450 ft/min (17.5 m/s)

 

Armament:

A total of eight external hardpoints (two ventral, three under each outer wing)

for external loads; the wing hardpoints were typically occupied with ELINT sensor pods, while the

ventral hardpoints frequently carried 300 l drop tanks to extend loiter time and range;

Typically, no offensive armament was carried, even though bombs or gun/missile pods were possible.

  

The kit and its assembly:

This build became a submission to the “Reconnaissance” Group Build at whatifmodellers.com in July 2021, and it spins further real-world events. Germany actually tested two OV-1s in the Sixties (by the German Army/Bundesheer, not by the air force), but the type was not procured or operated. The test aircraft carried a glossy, olive drab livery (US standard, I think) with German national markings.

However, having a vintage Hasegawa OV-1A in the stash, I wondered what an operational German OV-1 might have looked like, especially if it had been operated into the Eighties and beyond, in the contemporary Norm 83 paint scheme? This led to this purely fictional OV-1G.

 

The kit was mostly built OOB, and the building experience was rather so-so – after all, it’s a pretty old mold/boxing (in my case the Hasegawa/Hales kit is from 1978, the mold is from 1968!). Just a few things were modified/added in order to tweak the standard, short-winged OV-1A into something more modern and sophisticated.

 

When searching for a solution to mount some ELINT sensor arrays, I did not want to copy the OV-1B’s characteristic offset, ventral SLAR fairing. I rather settled for the late RV-1D’s solution with sensor pods under the outer wings. Unfortunately, the OV-1A kit came with the type’s original short wings, so that the pods had to occupy the inner underwing pair of hardpoints. The pods were scratched from square styrene profiles and putty, so that they received a unique look. The Mohawk’s pair of ventral hardpoints were mounted, but – after considering some drop tanks or an ECM pod there - left empty, so that the field of view for the ventral panoramic camera would not be obscured.

 

Other small additions are some radar warning sensor bumps on the nose, some extra antennae, a shallow bulge for the MIDS antenna on the spine, the FLIR turret on the nose (with parts from an Italeri AH-1 and a Kangnam Yak-38!), and I added a tail stinger for a retrofitted (scratched) IR decoy device, inspired by the American AN/ALG-147. This once was a Matchbox SNEB unguided missile pod.

  

Painting and markings:

For the intended era, the German Norm 83 paint scheme, which is still in use today on several Luftwaffe types like the Transall, PAH-2 or CH-53, appeared like a natural choice. It’s a tri-color wraparound scheme, consisting of RAL 6003 (Olivgrün), FS 34097 (Forest Green) and RAL 7021 (Teerschwarz). The paints I used are Humbrol 86 (which is supposed to be a WWI version of RAL 6003, it lacks IMHO yellow but has good contrast to the other tones), Humbrol 116 and Revell 9. The pattern itself was adapted from the German Luftwaffe’s Dornier Do 28D “Skyservants” with Norm 83 camouflage, because of the type’s similar outlines.

 

A black ink washing was applied for light weathering, plus some post-shading of panels with lighter shades of the basic camouflage tones for a more plastic look. The cockpit interior was painted in light grey (Humbrol 167), while the landing gear and the interior of the air brakes became white. The scratched SLAR pods became light grey, with flat di-electric panels in medium grey (created with decal material).

The cockpit interior was painted in a rather light grey (Humbrol 167), the pilots received typical olive drab Luftwaffe overalls, one with a white “bone dome” and the other with a more modern light grey helmet.

 

The decals were improvised. National markings and tactical codes came from TL Modellbau sheets, the AG 51 emblems were taken from a Hasegawa RF-4E sheet. The black walkways were taken from the Mohak’s OOB sheet, the black de-icer leading edges on wings and tail were created with generic black decal material. Finally, the model was sealed with a coat of matt acrylic varnish (Italeri).

  

An interesting result, and the hybrid paint scheme with the additional desert camouflage really makes the aircraft an unusual sight, adding to its credibility.

Davis-Monthan Air Force Base boneyard museum, Tucson, Arizona

----

Two Allison/Rolls-Royce T56-A-427 turboprops, 5,100-shp each

 

DSC_0419 Anx2 V2 2014-10-25 1200h Q90 0.5k-1.5k

English:

CH-148 Cyclone

Royal Canadian Air Force

 

The CH-148 Cyclone is one of the most capable maritime helicopters in the world. It is Canada’s main ship-borne maritime helicopter, and it provides air support to the Royal Canadian Navy.

 

The Cyclone can be used for surface and sub-surface surveillance, search and rescue missions, tactical transport and more. It can operate during the day or night and in most weather conditions to support missions in Canada and around the world.

 

Length: 17.22 m

Length (folded configuration): 14.78 m

Rotor span: 17.48 m

Height: 5.44 m

Maximum Gross Weight: 13,000 kg

Maximum speed: 287 km/h

Range: 740 km

Location(s):

Patricia Bay, B.C.

Shearwater, N.S.

  

----------------------------------------------------------------------------------------

 

Français :

CH-148 Cyclone

Aviation royale canadienne

 

Le CH-148 Cyclone figure parmi les hélicoptères maritimes les plus efficaces au monde. À titre de principal hélicoptère maritime embarqué du Canada, son travail consiste à apporter un soutien aérien à la Marine royale canadienne.

 

Le CH-148 Cyclone accomplit notamment des missions de surveillance et de contrôle de surface et sous-marins, de recherche et de sauvetage et de transport tactique. Il peut accomplir son travail de jour comme de nuit, dans la majorité des conditions météorologiques, afin de soutenir les missions canadiennes et internationales.

 

Longeur : 17,22 m

Longeur (plié) : 14,78 m

Envergure du rotor : 17,48 m

Hauteur : 5,44 m

Masse totale maximale : 13 000 kg

Vitesse maximale : 287 km/h

Autonomie : 740 km

Bases :

Patricia Bay, C.-B.

Shearwater, N.-É.

  

www.rcaf-arc.forces.gc.ca/en/aircraft-current/ch-148.page

 

These angel creatures are all combat–capable and are among those that appear to aid the Prime Galaxy in small numbers from time to time and would fight in a full–fledged army of God in the event of an apocalyptic–scale conflict against demons and/or abominations. Also featured here is one very special individual.

 

• Kuthlody: A being that deliberately resembles a musical note in basic shape. However, functionally there is nothing musical about the Kuthlody, sadly. Instead, it is a multi–purpose battle–oriented unit that can free–float but also rest on the ground by standing on its "chin", and flies around swinging itself at enemies (when there are enemies to be swung at; when there aren't it just flies around aimlessly). In addition, the Kuthlody possesses four small, circular blades that can be launched from its sides at will and controlled remotely in midair, and return to the user after hitting (or missing) the target, like a boomerang. Kuthlodies also have an alternate mode which they enter when picked up and used as weapons by larger humanoid–like beings such as DeyRhine. They do not mind being used as melee weapons at all, for it is not all that different than what they would normally do. This angel's mean durability value is 650.

 

• Harus–Ovactus: While the DeyRhine is the Juggernaut of Faith, the Harus–Ovactus is the Juggernaut of Justice. The two creatures are counterparts of one another. And while the DeyRhine, though inherently powerful, is a ceremonial creature not particularly suited for fighting, the Harus–Ovactus is made for fighting or, more accurately, for shooting and bombarding. Also, it can speak telepathically, unlike the DeyRhine, at least to other angels.

One of the most violent angels out there (as far as angels do go), it resembles a moderately–sized flying saucer that is constantly kept afloat by the Rainbow Energy capsule sticking out of its bottom, which unfortunately is its weak point, though fortunately it is also very sturdy and not any easier to dislodge or destroy than any other part of the angel's body. And the Harus–Ovactus has a durability value of over 5,000.

They originate from the Temple of Infinity, where each new Harus–Ovactus is hand–crafted by Vaynmizs himself, and after being brought to life begin patrolling between both Paradise and Neo–Skyhold. They are equipped with three main weapons: two standard–issue Rainbow Energy lasers, two highly accurate non–lethal sniper guns that instantly tranquilize any living thing their projectiles touch, and bomb hatches that drop powerful wide–radius magical grenades on enemies, which are harmless to angels and positively lethal to everything else. Due to the angel's violent nature, the Harus–Ovactus is highly corruptible and can be hijacked and/or reprogrammed by demons. In this situation it must be destroyed as soon as possible.

 

• Jebgulex: A slight, lanky humanoid angel with a single massive eye in place of a face that controls a floating platform which it stands and rides around on and will never fall off of, and several normal–sized eyes that float above its head. Said platform has a structure beneath it that includes an indestructible Rainbow Energy laser that will only disappear if the Jebgulex itself is killed. All of its eyes, both the floating ones and the giant ones, can also shoot these lasers. The Jebgulex has one handless, featureless and useless arm, and another one that can, again, shoot Rainbow Energy lasers. Due to lacking a mouth, it cannot talk, but would if it did have one. Its durability value is roughly 400. This is somewhat made up for by its many eyes, all of which provide vision in addition to their laser powers.

 

• Enkheses: Firstly, note that the word "Enkheses" is both the singular and plural form of this creature's name. The Enkheses is a corporeal, humanoid angelic warrior with a stout, short and fat body and predominantly purple complexion. It spends most of its time receiving prayer, which makes it more powerful as with many other angels, in the outer circles of Paradise. It also has a mind and personality, and is allowed two hours per day to indulge itself in productive ways such as reading, writing and creating other art, which sometimes goes on to be added to the permanent fixtures of Heaven if it is good enough. Enkheses are only able to compose and visualize about good and pure things, both due to mandate and by their own nature, so what they produce usually isn't as varied or compelling as what mortals can produce, but can have just as much talent and effort put into it. In times of crisis however, they are more than capable of defending themselves and even being part of the offensive, and, as mentioned above, they would be among the ranks of an angel army if one ever needed to be assembled. Enkheses have superhumanoid strength and fighting skills, and durability values of more than 1,000. Because of the similarities between the two beings, the Merthaldu consider the Enkheses to be the patron angels of their race and often name themselves after them.

 

• Yuyonarf: Yuyonarfs are very small flying angels that always act in groups of three or more. They are similar in many respects to the Harus–Ovactus in that they are created by Vaynmizs at the Temple of Infinity and can fly freely throughout all the levels of Heaven. The key difference is that Yuyonarfs are much, much smaller and are intended to be implemented as minor and/or support units to complement their larger siblings. Their fronts very much resemble faces or masks, though this is coincidental, and small, sharp projectiles are shot through the holes in these alleged masks. They are also surrounded by small force fields that can absorb most hostile projectiles that come near them. The designs and appearances of the "faces" and force fields vary wildly between individuals, and there are millions of them in existence, all with an in some way unique appearance. Each "pack" of Yuyonarfs shares a single mind between its members, while each individual has its own (tiny and simple) soul. And yes, there is a difference. The Yuyonarf is about 2–3 feet in height and they have durability values ranging from 200–400.

 

• Connor "'The Great' Thorn" Thorn, the Messiah of the Delta Octant: "Thorn" was the name of the messianic hero whose appearance was foretold in passage 7:19 of the Next Testament, and who would deliver the Delta Octant from certain destruction at the hands of one of the greatest evils to ever befall the Prime Galaxy, Cosmo'rath: the most vile and ruthless portion of Reson's Arcane Order, led by the Xoultac Evil Ninja Emperor Heinrich, who is now known to have been a certifiable sociopath by demon standards, and also a pathological liar because he wasn't even a ninja whatsoever! Anyway, he was Bad with a capital "B" and his minions were equally evil. The conflict against them was known as the Vision Wars, and it was one of the most brutal the galaxy has ever seen. But, it was written that Thorn would come and save all from him and them just when things were looking their bleakest. The faithful never doubted that their hero would come eventually, not even when an entire species was eradicated and another 100% corrupted beyond redemption (Note: survivors from both those races were later found elsewhere and thanks to them they are not extinct). But today, no one doubts that no one expected for Thorn to be a human. You read that correctly, a human: the only known one to ever set foot into the Nava–Verse and thus the very last of his kind alive (or was he?). And he wasn't even sent down from the humans' Heaven above our Heaven either, but was rather taken from Earth during his lifetime and well before the Rapture, and abruptly re–materialized aboard Air Station Alpha–Beta–Delta–Gamma–Omega in the middle of the infamous battle against the corrupted Rorke–Norgs invading it in early Age 568. It is generally agreed upon that if Thorn did not appear then and there, every Flufewog aboard that installation would have died that day. But when he did appear, the final outcome of the battle was the destruction of the entire invading force and their ship, albeit with very heavy casualties on the good side. Thorn was injured severely in the battle, wherein he killed key Cosmo'rath general Yemu'Ix the Netojax, and afterward crash landed on planet Sertrop in an escape pod where he was discovered by the Merthaldu of a nearby conveniently–located village, and given treatment. It was here that Thorn revealed his status as a human, to the shock of everyone present. Unfortunately, the circumstances under which he was brought to our universe from his have been lost to history, for no one wrote anything down due to the urgent situation they were all in. It was also here that he befriended a Glanmi named Frilla, the last of her kind on Sertrop, who would play a key role later even in death.

Connor Thorn was then taken to Sertrop's central city of Nog'Dod, and sent toward Heinrich's floating palace of Pride orbiting Yominasst. To make a long story short, he and some others infiltrated the palace and eventually killed Heinrich. However, Thorn was mortally wounded in doing so and was saved only thanks to the quick thinking of the Kittpo Écuate, who in desperation poured vast quantities of the deceased Frilla's blood into the gaping hole in his body. All the bodily fluids of Glanmi have healing properties but cannot normally save someone from wounds as severe as Thorn's, but thanks to a miracle, God the Father allowed Frilla's soul to be merged with Thorn's, saving his life and permanently turning him into a human–Glanmi hybrid. The transformation was not immediate, but rather took place over the next several days. Connor Thorn was now an eternally youthful and biologically immortal mutant. He went on to later have many more heroic adventures, though none as notable as his first.

Thorn lived until Age 809, when he was killed by Lord Reson in during an ill–advised attack on the immensely powerful villain who had been spotted in the Gomorran Desert Plane. He was part of an elite strike team sent down through the Lower Dimensional Rift to try to assassinate the demon(?), of which there were no survivors. As billions mourned the hero's loss, the angels announced that he had been reunited with his own kind as a pure human soul in the Heaven above our Heaven. Many manly tears were shed that fateful day.

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based on historical facts. BEWARE!

  

Some Background:

The Lockheed F-94 Starfire was a first-generation jet aircraft of the United States Air Force. It was developed from the twin-seat Lockheed T-33 Shooting Star in the late 1940s as an all-weather, day/night interceptor, replacing the propeller-driven North American F-82 Twin Mustang in this role. The system was designed to overtake the F-80 in terms of performance, but more so to intercept the new high-level Soviet bombers capable of nuclear attacks on America and her Allies - in particular, the new Tupelov Tu-4. The F-94 was furthermore the first operational USAF fighter equipped with an afterburner and was the first jet-powered all-weather fighter to enter combat during the Korean War in January 1953.

 

The initial production model, the F-94A, entered operational service in May 1950. Its armament consisted of four 0.50 in (12.7 mm) M3 Browning machine guns mounted in the fuselage with the muzzles exiting under the radome for the APG-33 radar, a derivative from the AN/APG-3, which directed the Convair B-36's tail guns and had a range of up to 20 miles (32 km). Two 165 US Gallon (1,204 litre) drop tanks, as carried by the F-80 and T-33, were carried on the wingtips. Alternatively, these could be replaced by a pair of 1,000 lb (454 kg) bombs under the wings, giving the aircraft a secondary fighter bomber capability. 109 were produced.

 

The subsequent F-94B, which entered service in January 1951, was outwardly virtually identical to the F-94A. Its Allison J33 turbojet had a number of modifications made, though, which made it a very reliable engine. The pilot was provided with a roomier cockpit and the canopy received a bow frame in the center between the two crew members. A new Instrument Landing System (ILS) was fitted, too, which made operations at night and/or in bad weather much safer. However, this new variant’s punch with just four machine guns remained weak, and, to improve the load of fire, wing-mounted pods with two additional pairs of 0.5” machine guns were introduced – but these hardly improved the interceptor’s effectiveness. 356 of the F-94B were nevertheless built.

 

The following F-94C was extensively modified and initially designated F-97, but it was ultimately decided just to treat it as a new version of the F-94. USAF interest was lukewarm since aircraft technology had already developed at a fast pace – supersonic performance had already become standard. Lockheed funded development themselves, converting two F-94B airframes to YF-94C prototypes for evaluation with a completely new, much thinner wing, a swept tail surface and a more powerful Pratt & Whitney J48. This was a license-built version of the afterburning Rolls-Royce Tay, which produced a dry thrust of 6,350 pounds-force (28.2 kN) and approximately 8,750 pounds-force (38.9 kN) with afterburning. Instead of machine guns, the proposed new variant was exclusively armed with unguided air-to-air missiles.

Tests were positive and eventually the F-94C was adopted for USAF service, since it was the best interim solution for an all-weather fighter at that time. It still had to rely on Ground Control Interception Radar (GCI) sites to vector the interceptor to intruding aircraft, though.

 

The F-94C's introduction and the availability of the more effective Northrop F-89C/D Scorpion and the North American F-86D Sabre interceptors led to a quick relegation of the earlier F-94 variants from mid-1954 onwards to second line units and to Air National Guards. By 1955 most of them had already been phased out of USAF service, and some of these relatively young surplus machines were subsequently exported or handed over to friendly nations, too. When sent to the ANG, the F-94As were modified by Lockheed to F-94B standards and then returned to the ANG as B models. They primarily replaced outdated F-80C Shooting Stars and F-51D/H Mustangs.

 

At that time the USAF was looking for a tactical reconnaissance aircraft, a more effective successor for the RF-80A which had shown its worth and weaknesses during the Korea War. For instance, the plane could not fly at low altitude long enough to perform suitable visual reconnaissance, and its camera equipment was still based on WWII standards. Lockheed saw the opportunity to fill this operational gap with conversions of existing F-94A/B airframes, which had, in most cases, only had clocked few flying hours, primarily at high altitudes where Soviet bombers were expected to lurk, and still a lot of airframe life to offer. This led to another private venture, the RF-94B, auspiciously christened “Stargazer”.

 

The RF-94B was based on the F-94B interceptor with its J33 engine and the original unswept tail. The F-94B’s wings were retained but received a different leading-edge profile to better cope with operations at low altitude. The interceptor’s nose with the radome and the machine guns underneath was replaced by a new all-metal nose cone, which was more than 3 feet longer than the former radar nose, with windows for several sets of cameras; the wedge-shaped nose cone quickly earned the aircraft the unofficial nickname “Crocodile”.

One camera was looking ahead into flight direction and could be mounted at different angled downward (but not moved during flight), followed by two oblique cameras, looking to the left and the right, and a vertical camera as well as a long-range camera focussed on the horizon, which was behind a round window at port side. An additional, spacious compartment in front of the landing gear well held an innovative Tri-Metrogen horizon-to-horizon view system that consisted of three synchronized cameras. Coupled with a computerized control system based on light, speed, and altitude, it adjusted camera settings to produce pictures with greater delineation.

All cameras could be triggered individually by pilot or a dedicated observer/camera systems operator in the 2nd seat. Talking into a wire recorder, the crew could describe ground movements that might not have appeared in still pictures. A vertical view finder with a periscopic presentation on the cockpit panel was added for the pilot to enhance visual reconnaissance and target identification directly under the aircraft. Using magnesium flares carried under its wings in flash-ejector cartridges, the RF-94B was furthermore able to fly night missions.

The RF-94B was supposed to operate unarmed, but it could still carry a pair of 1.000 lb bombs under its wings or, thanks to added plumbings, an extra pair of drop tanks for ferry flights. The F-94A/B’s machine gun pods as well as the F-94C’s unguided missile launchers could be mounted to the wings, too, making it a viable attack aircraft in a secondary role.

 

The USAF was highly interested in this update proposal for the outdated interceptors (almost 500 F-94A/Bs had been built) and ordered 100 RF-94B conversions with an option for 100 more – just when a severe (and superior) competitor entered the stage after a lot of development troubles: Republic’s RF-84F Thunderflash reconnaissance version. The first YRF-84F had already been completed in February 1952 and it had an overall slightly better performance than the RF-94B. However, it offered more internal space for reconnaissance systems and was able to carry up to fifteen cameras with the support of many automatized systems, so that it was a single seater. Being largely identical to the F-84F and sharing its technical and logistical infrastructures, the USAF decided on short notice to change its procurement decision and rather adopt the more modern and promising Thunderflash as its standard tactical reconnaissance aircraft. The RF-94B conversion order was reduced to the initial 100 aircraft, and to avoid operational complexity these aircraft were exclusively delivered to Air National Guardss that had experience with the F-94A/B to replace their obsolete RF-80As.

 

Gradual replacement lasted until 1958, and while the RF-94B’s performance was overall better than the RF-80A’s, it was still disappointing and not the expected tactical intelligence gathering leap forward. The airframe did not cope well with constant low-level operations, and the aircraft’s marginal speed and handling did not ensure its survivability. However, unlike the RF-84F, which suffered from frequent engine problems, the Stargazers’ J33 made them highly reliable platforms – even though the complex Tri-Metrogen device turned out to be capricious, so that it was soon replaced with up to three standard cameras.

 

For better handling and less drag esp. at low altitude, the F-94B’s large Fletcher type wingtip tanks were frequently replaced with smaller ones with about half capacity. It also became common practice to operate the RF-94Bs with only a crew of one, and from 1960 on the RF-94B was, thanks to its second seat, more and more used as a trainer before pilots mounted more potent reconnaissance aircraft like the RF-101 Voodoo, which eventually replaced the RF-94B in ANG service. The last RF-94B was phased out in 1968, and, unlike the RF-84F, it was not operated by any foreign air force.

  

General characteristics:

Crew: 2 (but frequently operated by a single pilot)

Length: 43 ft 4 3/4 in (13.25 m)

Wingspan (with tip tanks): 40 ft 9 1/2 in (12.45 m)

Height: 12 ft. 2 (3.73 m)

Wing area: 234' 8" sq ft (29.11 m²)

Empty weight: 10,064 lb (4,570 kg)

Loaded weight: 15,330 lb (6,960 kg)

Max. takeoff weight: 24,184 lb (10,970 kg)

 

Powerplant:

1× Allison J33-A-33 turbojet, rated at 4,600 lbf (20.4 kN) continuous thrust,

5,400 lbf (24 kN) with water injection and 6,000 lbf (26.6 kN) thrust with afterburner

 

Performance:

Maximum speed: 630 mph (1,014 km/h) at height and in level flight

Range: 930 mi (813 nmi, 1,500 km) in combat configuration with two drop tanks

Ferry range: 1,457 mi (1,275 nmi, 2,345 km)

Service ceiling: 42,750 ft (14,000 m)

Rate of climb: 6,858 ft/min (34.9 m/s)

Wing loading: 57.4 lb/ft² (384 kg/m²)

Thrust/weight: 0.48

 

Armament:

No internal guns; 2x 165 US Gallon (1,204 liter) drop tanks on the wing tips and…

2x underwing hardpoints for two additional 165 US Gallon (1,204 liter) ferry tanks

or bombs of up to 1.000 lb (454 kg) caliber each, plus…

2x optional (rarely fitted) pods on the wings’ leading edges with either a pair of 0.5" (12.7 mm)

machine guns or twelve 2.75” (70 mm) Mk 4/Mk 40 Folding-Fin Aerial Rockets each

  

The kit and its assembly:

This project was originally earmarked as a submission for the 2021 “Reconnaissance & Surveillance” group build at whatifmodellers.com, in the form of a Heller F-94B with a new nose section. The inspiration behind this build was the real-world EF-94C (s/n 50-963): a solitary conversion with a bulbous camera nose. However, the EF-94C was not a reconnaissance aircraft but rather a chase plane/camera ship for the Air Research and Development Command, hence its unusual designation with the suffix “E”, standing for “Exempt” instead of the more appropriate “R” for a dedicated recce aircraft. There also was another EF-94C, but this was a totally different kind of aircraft: an ejection seat testbed.

 

I had a surplus Heller F-94B kit in The Stash™ and it was built almost completely OOB and did – except for some sinkholes and standard PSR work – not pose any problem. In fact, the old Heller Starfire model is IMHO a pretty good representation of the aircraft. O.K., its age might show, but almost anything you could ask for at 1:72 scale is there, including a decent, detailed cockpit.

 

The biggest change was the new camera nose, and it was scratched from an unlikely donor part: it consists of a Matchbox B-17G tail gunner station, slimmed down by the gunner station glazing's width at the seam in the middle, and this "sandwich" was furthermore turned upside down. Getting the transitional sections right took lots of PSR, though, and I added some styrene profiles to integrate the new nose into the rest of the hull. It was unintentional, but the new nose profile reminds a lot of a RF-101 recce Voodoo, and there's, with the straight wings, a very F-89ish look to the aircraft now? There's also something F2H-2ish about the outlines?

 

The large original wing tip tanks were cut off and replaced with smaller alternatives from a Hasegawa A-37. Because it was easy to realize on this kit I lowered the flaps, together with open ventral air brakes. The cockpit was taken OOB, I just modified the work station on the rear seat and replaced the rubber sight protector for the WSO with two screens for a camera operator. Finally, the one-piece cockpit glazing was cut into two parts to present the model with an open canopy.

  

Painting and markings:

This was a tough decision: either an NMF finish (the natural first choice), an overall light grey anti-corrosive coat of paint, both with relatively colorful unit markings, or camouflage. The USAF’s earlier RF-80As carried a unique scheme in olive drab/neutral grey with a medium waterline, but that would look rather vintage on the F-94. I decided that some tactical camouflage would make most sense on this kind of aircraft and eventually settled for the USAF’s SEA scheme with reduced tactical markings, which – after some field tests and improvisations in Vietnam – became standardized and was officially introduced to USAF aircraft around 1965 as well as to ANG units.

 

Even though I had already built a camouflaged F-94 some time ago (a Hellenic aircraft in worn SEA colors), I settled for this route. The basic colors (FS 30219, 34227, 34279 and 36622) all came from Humbrol (118, 117, 116 and 28, respectively), and for the pattern I adapted the paint scheme of the USAF’s probably only T-33 in SEA colors: a trainer based on Iceland during the Seventies and available as a markings option in one of the Special Hobby 1:32 T-33 kits. The low waterline received a wavy shape, inspired by an early ANG RF-101 in SEA camouflage I came across in a book. The new SEA scheme was apparently applied with a lot of enthusiasm and properness when it was brand new, but this quickly vaned. As an extra, the wing tip tanks received black anti-glare sections on their inner faces and a black anti-glare panel was added in front of the windscreen - a decal from a T-33 aftermarket sheet. Beyond a black ink wash the model received some subtle panel post-shading, but rather to emphasize surface details than for serious weathering.

 

The cockpit became very dark grey (Revell 06) while the landing gear wells were kept in zinc chromate green primer (Humbrol 80, Grass Green), with bright red (Humbrol 60, Matt Red) cover interiors and struts and wheels in aluminum (Humbrol 56). The interior of the flaps and the ventral air brakes became red, too.

 

The decals/markings came from a Special Hobby 1:72 F-86H; there’s a dedicated ANG boxing of the kit that comes with an optional camouflaged aircraft of the NY ANG, the least unit to operate the “Sabre Hog” during the Seventies. Since this 138th TFS formerly operated the F-94A/B, it was a perfect option for the RF-94B! I just used a different Bu. No. code on the fin, taken from a PrintScale A/T-37 set, and most stencils were perocured from the scrap box.

After a final light treatment with graphite around the afterburner for a more metallic shine of the iron metallic (Revell 97) underneath, the kit was sealed with a coat of matt acrylic varnish (Italeri).

  

A camouflaged F-94 is an unusual sight, but it works very well. The new/longer nose considerably changes the aircraft's profile, and even though the change is massive, the "Crocodile" looks surprisingly plausible, if not believable! And, despite the long nose, the aircraft looks pretty sleek, especially in the air.

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based historical facts. BEWARE!

  

Some background:

The Wasp was a transonic British jet-powered fighter aircraft that was developed by Folland for the Royal Air Force (RAF) during the late 1940s and early 1950s. The Wasp’s origins could be traced back to a privately funded 1952 concept for a bigger and more capable day fighter aircraft than Folland’s very light Midget/Gnat. The Wasp’s development had been continued until the Gnat’s service introduction, and by then it had evolved under the handle “Fo-145” into a supersonic aircraft that took advantage of the new Armstrong Siddeley Sapphire turbojet engine, swept wings and area rule. The aircraft was built with the minimum airframe size to take the reheated Saphire and a radar system that would allow it to deploy the new de Havilland Blue Jay (later Firestreak) guided air-to-air missile. In this form the aircraft was expected to surpass the Royal Air Force’s contemporary day fighter, the only gun-armed Hawker Hunter, which had been in service since 1954, while using basically the same engine as its F.2 variant, in both performance and armament aspects. The missile-armed Wasp was also expected to replace the disappointing Supermarine Swift and the Fairey Fireflash AAMs that had been developed for it.

The Wasp strongly resembled the smaller Gnat, with a similar but much thinner shoulder mounted wing, with a sweep of 35° at quarter chord, but the new aircraft featured some innovations. Beyond the area-ruled fuselage, the aircraft had full-span leading edge slats and trailing edge flaps with roll control achieved using spoilers rather than traditional ailerons. Anticipating supersonic performance, the tailplane was all-moving. The cockpit had been raised and offered the pilot a much better all-round field of view.

 

The Wasp was armed with four 30 mm (1.18 in) ADEN cannon, located under the air intakes. Each gun had a provision of 125 rounds, from form a mutual ventral ammunition bay that could be quickly replaced. Four underwing hardpoints could carry an ordnance load of up to 4.000 lb, and the Wasp’s main armament consisted of up to four IR-guided “Firestreak” AAMs. To effectively deploy them, however, a radar system was necessary. For launch, the missile seeker was slaved to the Wasp’s AI.Mk.20 X-band radar until lock was achieved and the weapon was launched, leaving the interceptor free to acquire another target. The AI.Mk.20 had been developed by EKCO since 1953 under the development label “Green Willow” for the upcoming EE Lightning interceptor, should the latter’s more complex and powerful Ferranti AIRPASS system fail. A major advantage of the AI.Mk.20 was that it had been designed as a single unit so it could be fit into the nose of smaller single-seat fighters, despite its total weight of roughly 400 lb (200 kg). For the Firestreak AAM, EKCO had developed a spiral-scan radar with a compact 18 in (460 mm) antenna that offered an effective range of about 10 miles (16 km), although only against targets very close to the centerline of the radar. The radar’s maximum detection range was 25 mi (40 km) and the system also acted as a ranging radar, providing range input to the gyro gunsight for air-to-air gunnery.

Beyond Firestreaks, the Wasp could also carry drop tanks (which were area-ruled and coulc only be carried on the inner pair of pylons), SNEB Pods with eighteen 68 mm (2.68 in) unguided rocket projectiles against air and ground targets, or iron bombs of up to 1.000 lb caliber. Other equipment included a nose-mounted, and a forward-facing gun camera.

 

The Royal Air Force was sufficiently impressed to order two prototypes. Since the afterburning version of the Sapphire was not ready yet, the first prototype flew on 30 July 1954 with a non-afterburning engine, an Armstrong Siddeley Sapphire Sa.6 with 8,000 lbf (35.59 kN). In spite of this lack of power the aircraft nevertheless nearly reached Mach 1 in its maiden flight. The second prototype, equipped with the intended Sapphire Sa.7 afterburning engine with 11,000 lbf (48.9 kN) thrust engine, showed the aircraft’s full potential. The Wasp turned out to have very good handling, and the RAF officially ordered sixty Folland Fo-145 day-fighters under the designation “Wasp F.Mk.1”. The only changes from the prototypes were small leading-edge extensions at the wing roots, improving low speed handling, esp. during landings and at high angles of incidence in flight.

 

Most Wasps were delivered to RAF Germany frontline units, including No. 20 and 92 Squadrons based in Northern Germany. However, the Wasp’s active service did not last long, because technological advancements quickly rendered the aircraft obsolete in its original interceptor role. The Wasp’s performance had not turned out as significantly superior to the Hunter as expected. Range was rather limited, and the aircraft turned out to be underpowered, since the reheated Sapphire Sa6 did not develop as much power as expected. The AI.Mk.20 radar was rather weak and capricious, too, and the Firestreak was an operational nightmare. The missile was, due to its solid Magpie rocket motor and the ammonia coolant for the IR seeker head, highly toxic and RAF armorers had to wear some form of CRBN protection to safely mount the missile onto an aircraft. Furthermore, unlike modern missiles, Firestreak’s effectiveness was very limited since it could only be fired outside cloud - and over Europe or in winter, skies were rarely clear.

 

Plans for a second production run of the Folland Wasp with a more powerful Sapphire Sa7R engine with a raised thrust of 12,300 lbf (54.7 kN) and updated avionics were not carried out. During the 1960s, following the successful introduction of the supersonic English Electric Lightning in the interceptor role, the Wasp, as well as the older but more prosperous and versatile Hunter, transitioned to being operated as a fighter-bomber, advanced trainer and for tactical photo reconnaissance missions.

This led to a limited MLU program for the F.Mk.1s and conversions of the remaining airframes into two new variants: the new main version was the GR.Mk.2, a dedicated CAS/ground attack variant, which had its radar removed and replaced with ballast, outwardly recognizable through a solid metal nose which replaced the original fiberglass radome. Many of these machines also had two of the 30mm guns removed to save weight. Furthermore, a handful Wasps were converted into PR.Mk.3s. These had as set of five cameras in a new nose section with various windows, and all the guns and the ammunition bay were replaced with an additional fuel tank, operating as pure, unarmed reconnaissance aircraft. When Folland was integrated into the Hawker Siddeley Group in 1963 the aircraft’s official name was changed accordingly, even though the Folland name heritage persisted.

 

Most of these aircraft remained allocated to RAF Germany units and retired towards the late Sixties, but four GR.Mk.2s were operated by RAF No. 57 (Reserve) Squadron and based at No. 3 Flying Training School at Cranwell, where they were flown as adversaries in dissimilar aerial combat training. The last of the type was withdrawn from service in 1969, but one aircraft remained flying with the Aeroplane and Armament Experimental Establishment at Boscombe Down until 24 January 1975.

  

General characteristics:

Crew: 1

Length: 45 ft 10.5 in (13.983 m)

Wingspan: 31 ft 7.5 in (9.639 m)

Height: 13 ft 2.75 in (4.0323 m)

Wing area: 250 sq ft (23 m2)

Empty weight: 13,810 lb (6,264 kg)

Gross weight: 21,035 lb (9,541 kg)

Max takeoff weight: 23,459 lb (10,641 kg)

 

Powerplant:

1× Armstrong Siddeley Sapphire Sa.6, producing 7,450 lbf (33.1 kN) thrust at 8,300 rpm,

military power dry, and 11,000 lbf (48.9 kN) with afterburner

 

Performance:

Maximum speed: 631 kn (726 mph, 1,169 km/h) / M1.1 at 35,000 ft (10,668 m)

654 kn (753 mph; 1,211 km/h) at sea level

Cruise speed: 501 kn (577 mph, 928 km/h)

Range: 1,110 nmi (1,280 mi, 2,060 km)

Service ceiling: 49,000 ft (15,000 m)

Rate of climb: 16,300 ft/min (83 m/s)

Wing loading: 84 lb/sq ft (410 kg/m2)

Thrust/weight: 0.5

 

Armament:

4× 30 mm (1.18 in) ADEN cannon, 125 rounds per gun

4× underwing hardpoints for a total external ordnance of 4.000 lb, including Firestreak AAMs,

SNEB pods, bombs of up to 1.000 lb caliber or two 125 imp gal (570 l) drop tanks

  

The kit and its assembly

This kit travesty is a remake of a simple but brilliant idea of fellow modeler chrisonord at whatifmodellers’com (www.whatifmodellers.com/index.php?topic=48434.msg899420#m...), who posted his own build in late 2020: a Grumman Tiger in standard contemporary RAF colors as Folland Wasp GR.Mk.2. The result looked like a highly credible “big brother” or maybe successor of Folland’s diminutive Midge/Gnat fighter, something in the Hawker Hunter’s class. I really like the idea a lot and decided that it was, one and a half years later, to build my personal interpretation of the subject – also because I had a Hasegawa F11F kit in The Stash™ without a proper plan.

 

The Tiger was built basically OOB – a simple and straightforward affair that goes together well, just the fine, raised panel lines show the mould’s age. The only changes I made: the arrester hook disappeared under PSR, small stabilizer fins (from an Italeri BAe Hawk) were added under the tail section, and I replaced the Tiger’s rugged twin wheel front landing gear with a single wheel alternative, left over from a Matchbox T-2 Buckeye. On the main landing gear, the rearward-facing stabilizing struts were deleted (for a lighter look of a land-based aircraft) and their wells filled with putty. A late modification were additional swing arms for the main landing gear, though: once the kit could sit on its own three feet, the stance was odd and low, esp. under the tail – probably due to the new front wheel. As a remedy I glued additional swing arm elements, made from 1mm steel wire, under the original struts, what moved the main wheel a little backwards and raised the main landing gear my 1mm. Does not sound like much, but it was enough to lift the tail and give the aircraft a more convincing stance and ground clearance.

 

The area-ruled drop tanks and their respective pylons were taken from the Hasegawa kit. For a special “British” touch – because the Tiger had a radome (into which no radar was ever fitted, though) – I added a pair of Firestreak AAMs on the outer underwing stations, procured from a Gomix Gloster Javelin (which comes with four of these, plus pylons).

  

Painting and markings:

Since the RAF theme was more or less settled, paintwork revolved around more or less authentical colors and markings. The Wasp received a standard RAF day fighter scheme from the late Fifties, with upper camouflage in RAF Dark Green/Dark Sea Grey and Light Aircraft Grey undersides with a low waterline. I used Humbrol 163, 106 and 166, respectively – Ocean Grey was used because I did not have the proper 164 at hand, but 106 also offered the benefit of a slightly better contrast to the murky Dark Green. A black ink washing was applied plus some panel post-shading. The silver leading edges on wings, stabilizers and fin were created with decal sheet material, avoiding the inconvenience of masking.

 

The cockpit interior was painted in a very dark grey (Revell 09, Anthracite) while the landing gear, wheels and wells received a greyish-metallic finish (Humbrol 56, Aluminum Dope). The air intakes’ interior became bright aluminum (Revell 99), the area around the jet nozzle was painted with Revell 91 (Iron metallic) and later treated with graphite for a dark metallic shine. The drop tanks were camouflaged, the Firestreaks became white so that they would stand out well and add to a certain vintage look.

 

The decals were a mix from various sources. The No. 20 Squadron badges and the Type D high-viz roundels on the wings were left over from an Airfix Hawker Hunter. The fuselage roundels came from an Italeri BAe Hawk sheet, IIRC. The bent fin flash, all the stencils as well as the serial code (which was puzzled together from two real serials and was AFAIK not allocated to any real RAF aircraft) came from an Xtradecal Supermarine Swift sheet. The individual red “B” letter came from a Matchbox A.W. Meteor night fighter.

 

Finally, the kit was sealed with matt acrylic varnish – I considered a glossy finish, since this was typical for RAF aircraft in the Fifties, but eventually just gave the radome a light shine.

  

Basically a simple project, and quickly done in just a couple of days. However, chrisonord’s great eye for similarities makes this “Tiger in disguise” a great fictional aircraft model with only little effort, it’s IMHO very convincing. And the RAF colors and markings suit the F11F very well.

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based historical facts. BEWARE!

 

Some background:

The Mikoyan-Gurevich MiG-19 (NATO reporting name: "Farmer") was a Soviet second-generation, single-seat, twin jet-engine fighter aircraft. It was the first Soviet production aircraft capable of supersonic speeds in level flight. A comparable U.S. "Century Series" fighter was the North American F-100 Super Sabre, although the MiG-19 would primarily oppose the more modern McDonnell Douglas F-4 Phantom II and Republic F-105 Thunderchief over North Vietnam. Furthermore, the North American YF-100 Super Sabre prototype appeared approximately one year after the MiG-19, making the MiG-19 the first operational supersonic jet in the world.

 

On 20 April 1951, OKB-155 was given the order to develop the MiG-17 into a new fighter called "I-340", also known as "SM-1". It was to be powered by two Mikulin AM-5 non-afterburning jet engines, a scaled-down version of the Mikulin AM-3, with 19.6 kN (4,410 lbf) of thrust. The I-340 was supposed to attain 1,160 km/h (725 mph, Mach 0.97) at 2,000 m (6,562 ft), 1,080 km/h (675 mph, Mach 1.0) at 10,000 m (32,808 ft), climb to 10,000 m (32,808 ft) in 2.9 minutes, and have a service ceiling of no less than 17,500 m (57,415 ft).

After several prototypes with many detail improvements, the ministers of the Soviet Union issued the order #286-133 to start serial production on February 17, 1954, at the factories in Gorkiy and Novosibirsk. Factory trials were completed on September 12 the same year, and government trials started on September 30.

 

Initial enthusiasm for the aircraft was dampened by several problems. The most alarming of these was the danger of a midair explosion due to overheating of the fuselage fuel tanks located between the engines. Deployment of airbrakes at high speeds caused a high-g pitch-up. Elevators lacked authority at supersonic speeds. The high landing speed of 230 km/h (145 mph), compared to 160 km/h (100 mph) for the MiG-15, combined with the lack of a two-seat trainer version, slowed pilot transition to the type. Handling problems were addressed with the second prototype, "SM-9/2", which added a third ventral airbrake and introduced all-moving tailplanes with a damper to prevent pilot-induced oscillations at subsonic speeds. It flew on 16 September 1954, and entered production as the MiG-19S.

 

Approximately 5,500 MiG-19's were produced, first in the USSR and in Czechoslovakia as the Avia S-105, but mainly in the People's Republic of China as the Shenyang J-6. The aircraft saw service with a number of other national air forces, including those of Cuba, North Vietnam, Egypt, Pakistan, and North Korea. The aircraft saw combat during the Vietnam War, the 1967 Six Day War, and the 1971 Bangladesh War.

 

However, jet fighter development made huge leaps in the 1960s, and OKB MiG was constantly trying to improve the MiG-19's performance, esp. against fast and high-flying enemies, primarily bombers but also spy planes like the U-2.

 

As the MiG-19S was brought into service with the Soviet air forces in mid-1956, the OKB MiG was continuing the refinement of the SM-1/I-340 fighter. One of these evolutionary paths was the SM-12 (literally, “SM-1, second generation”) family of prototypes, the ultimate extrapolation of the basic MiG-19 design, which eventually led to the MiG-19bis interceptor that filled the gap between the MiG-19S and the following, highly successful MiG-21.

 

The SM-12 first saw life as an exercise in drag reduction by means of new air intake configurations, since the MiG-19’s original intake with rounded lips became inefficient at supersonic speed (its Western rival, the North American F-100, featured a sharp-lipped nose air intake from the start). The first of three prototypes, the SM-12/1, was essentially a MiG-19S with an extended and straight-tapered nose with sharp-lipped orifice and a pointed, two-position shock cone on the intake splitter. The simple arrangement proved to be successful and was further refined.

 

The next evolutionary step, the SM-12/3, differed from its predecessors primarily in two new R3-26 turbojets developed from the earlier power plant by V. N. Sorokin. These each offered an afterburning thrust of 3,600kg, enabling the SM-12/3 to attain speeds ranging between 1,430km/h at sea level, or Mach=1.16, and 1,930km/h at 12,000m, or Mach=1.8, and an altitude of between 17,500 and 18,000m during its test program. This outstanding performance prompted further development with a view to production as a point defense interceptor.

 

Similarly powered by R3-26 engines, and embodying major nose redesign with a larger orifice permitting introduction of a substantial two-position conical centerbody for a TsD-30 radar, a further prototype was completed as the SM-12PM. Discarding the wing root NR-30 cannon of preceding prototypes, the SM-12PM was armed with only two K-5M (RS-2U) beam-riding missiles and entered flight test in 1957. This configuration would become the basis for the MiG-19bis interceptor that eventually was ordered into limited production (see below).

 

However, the SM-12 development line did not stop at this point. At the end of 1958, yet another prototype, the SM-12PMU, joined the experimental fighter family. This had R3M-26 turbojets uprated to 3.800kg with afterburning, but these were further augmented by a U-19D accelerator, which took the form of a permanent ventral pack containing an RU-013 rocket motor and its propellant tanks. Developed by D. D. Sevruk, the RU-013 delivered 3,000kg of additional thrust, and with the aid of this rocket motor, the SM-12PMU attained an altitude of 24,000m and a speed of Mach=1.69. But this effort was to no avail: the decision had been taken meanwhile to manufacture the Ye-7 in series as the MiG-21, and further development of the SM-12 series was therefore discontinued.

 

Nevertheless, since full operational status of the new MiG-21 was expected to remain pending for some time, production of a modified SM-12PM was ordered as a gap filler. Not only would this fighter bridge the performance gap to the Mach 2-capable MiG-21, it also had the benefit of being based on proven technologies and would not require a new basic pilot training.

 

The new aircraft received the official designation MiG-19bis. Compared with the SM-12PM prototype, the MiG-19bis differed in some details and improvements. The SM-12PM’s most significant shortfall was its short range – at full power, it had only a range of 750 km! This could be mended through an additional fuel tank in an enlarged dorsal fairing behind the cockpit. With this internal extra fuel, range could be extended by a further 200 - 250km range, but drop tanks had typically to be carried, too, in order to extend the fighter’ combat radius with two AAMs to 500 km. Specifically for the MiG-19bis, new, supersonic drop tanks (PTB-490) were designed, and these were later adapted for the MiG-21, too.

 

The air intake shock cone was re-contoured and the shifting mechanism improved: Instead of a simple, conical shape, the shock cone now had a more complex curvature with two steps and the intake orifice area was widened to allow a higher airflow rate. The air intake’s efficiency was further optimized through gradual positions of the shock cone.

As a positive side effect, the revised shock cone offered space for an enlarged radar dish, what improved detection range and resolution. The TsD-30 radar for the fighter’s missile-only armament was retained, even though the K-5’s effective range of only 2–6 km (1¼ – 3¾ mi) made it only suitable against slow and large targets like bombers. All guns were deleted in order to save weight or make room for the electronic equipment. The tail section was also changed because the R3M-26 engines and their afterburners were considerably longer than the MiG-19's original RM-5 engines. The exhausts now markedly protruded from the tail section, and the original, characteristic pen nib fairing between the two engines had been modified accordingly.

 

Production started in 1960, but only a total of roundabout 180 MiG-19bis, which received the NATO code "Farmer F", were built and the Soviet Union remained the only operator of the type. The first aircraft entered Soviet Anti-Air Defense in early 1961, and the machines were concentrated in PVO interceptor units around major sites like Moscow, Sewastopol at the Black Sea and Vladivostok in the Far East.

 

With the advent of the MiG-21, though, their career did not last long. Even though many machines were updated to carry the K-13 (the IR-guided AA-2 "Atoll") as well as the improved K-55 AAMs, with no change of the type’s designation, most MiG-19bis were already phased out towards the late 1960s and quickly replaced by 2nd generation MiG-21s as well as heavier and more capable Suchoj interceptors like the Su-9, -11 and -15. By 1972, all MiG-19bis had been retired.

  

General characteristics:

Crew: 1

Length: 13.54 m (44 ft 4 in), fuselage only with shock cone in forward position

15.48 m (50 8 ½ in) including pitot

Wingspan: 9 m (29 ft 6 in)

Height: 3.8885 m (12 ft 9 in)

Wing area: 25 m² (269 ft²)

Empty weight: 5,210 kg (11,475 lb)

Loaded weight: 7,890 kg (17,380 lb)

Max. takeoff weight: 9,050 kg (19,935 lb)

Fuel capacity: 2,450 l (556 imp gal; 647 US gal) internal;

plus 760 l (170 imp gal; 200 US gal) with 2 drop tanks

 

Powerplant:

2× Sorokin R3M-26 turbojets, rated at 37.2 kN (8,370 lbf) thrust each with afterburning

 

Performance:

Maximum speed: 1,380km/h at sea level (Mach=1.16)

1,850km/h at 12,000m (Mach=1.8)

Range: 1,250 km (775 mi; 750 nmi) at 14,000 m (45,000 ft) with 2 × 490 l drop tanks

Combat range: 500 km (312 mi; 270 nmi)

Ferry range: 2,000 km (1,242 mi; 690 nmi)

Service ceiling: 19,750 m (64,690 ft)

Rate of climb: 180 m/s (35,000 ft/min)

Wing loading: 353.3 kg/m² (72.4 lb/ft²)

Thrust/weight: 0.86

 

Armament:

No internal guns.

4× underwing pylons; typically, a pair of PTB-490 drop tanks were carried on the outer pylon pair,

plus a pair of air-to air missiles on the inner pair: initially two radar-guided Kaliningrad K-5M (RS-2US)

AAMs, later two radar-guided K-55 or IR-guided Vympel K-13 (AA-2 'Atoll') AAMs

  

The kit and its assembly:

Another submission for the 2018 Cold War Group Build at whatifmodelers.com, and again the opportunity to build a whiffy model from the project list. But it’s as fictional as one might think, since the SM-12 line of experimental “hybrid” fighters between the MiG-19 and the MiG-21 was real. But none of these aircraft ever made it into serial production, and in real life the MiG-21 showed so much potential that the attempts to improve the MiG-19 were stopped and no operational fighter entered production or service.

 

However, the SM-12, with its elongated nose and the central shock cone, makes a nice model subject, and I imagined what a service aircraft might have looked like? It would IMHO have been close, if not identical, to the SM-12PM, since this was the most refined pure jet fighter in the development family.

 

The basis for the build was a (dead cheap) Mastercraft MiG-19, which is a re-edition of the venerable Kovozávody Prostějov (KP) kit – as a tribute to modern tastes, it comes with (crudely) engraved panel, but it has a horrible fit all over. For instance, there was a 1mm gap between the fuselage and the right wing, the wing halves’ outlines did not match at all and it is questionable if the canopy actually belongs to the kit at all? PSR everywhere. I also had a Plastyk version of this kit on the table some time ago, but it was of a much better quality! O.K., the Mastercraft kit comes cheap, but it’s, to be honest, not a real bargain.

 

Even though the result would not be crisp I did some mods and changes. Internally, a cockpit tub was implanted (OOB there’s just a wacky seat hanging in mid air) plus some serious lead weight in the nose section for a proper stance.

On the outside, the new air intake is the most obvious change. I found a Su-17 intake (from a Mastercraft kit, too) and used a piece from a Matchbox B-17G’s dorsal turret to elongate the nose – it had an almost perfect diameter and a mildly conical shape. Some massive PSR work was necessary to blend the parts together, though.

The tail received new jet nozzles, scratched from steel needle protection covers, and the tail fairing was adjusted according to the real SM-12’s shape.

 

Ordnance was adapted, too: the drop tanks come from a Mastercraft MiG-21, and these supersonic PTB-490 tanks were indeed carried by the real SM-12 prototypes because the uprated engines were very thirsty and the original, teardrop-shaped MiG-19 tanks simply too draggy for the much faster SM-12. As a side note, the real SM-12’s short range was one of the serious factors that prevented the promising type’s production in real life. In order to overcome the poor range weakness I added an enlarged spine (half of a drop tank), inspired by the MiG-21 SMT, that would house an additional internal fuel tank.

 

The R2-SU/K-5 AAMs come from a vintage Mastercraft Soviet aircraft weapon set, which carries a pair of these 1st generation AAMs. While the molds seem to be a bit soft, the missiles look pretty convincing. Their pylons were taken from the kit (OOB they carry unguided AAM pods and are placed behind the main landing gear wells), just reversed and placed on the wings’ leading edges – similar to the real SM-12’s arrangement.

  

Painting and markings:

No surprises. In the Sixties, any PVO aircraft was left in bare metal, so there was hardly an alternative to a NMF finish.

 

Painting started with an all-over coat with acrylic Revell 99 (Aluminum), just the spine tank became light grey (Revell 371) for some contrast, and I painted some di-electric covers in a deep green (Revell 48).

The cockpit interior was painted with a bright mix of Revell 55 and some 48, while the landing gear wells and the back section of the cockpit were painted in a bluish grey (Revell 57).

The landing gear was painted in Steel (unpolished Modelmaster metallizer) and received classic, bright green wheel discs (Humbrol 2). As a small, unusual highlight the pitot boom under the chin received red and white stripes – seen on occasional MiG-19S fighters in Soviet service, and the anti-flutter booms on the stabilizers became bright red, too.

 

After the basic painting was done the kit received a black ink wash. Once this had dried and wiped off with a soft cotton cloth, post shading with various metallizer tones was added in order to liven up the uniform aircraft (including Humbrol’s matt and polished aluminum, and the exhaust section was treated with steel). Some panel lines were emphasized with a thin pencil.

 

Decals were puzzled together from various sources, a Guards badge and a few Russian stencils were added, too. Finally, the kit was sealed with a coat of sheen acrylic varnish (a 2:1 mix of Italeri matt and semi-gloss varnish).

 

The K-5 missiles, last but not least, were painted in aluminum, too, but their end caps (both front and tail section) became off-white.

  

The Mastercraft kit on which this conversion was based is crude, so I did not have high expectations concerning the outcome. But the new nose blends nicely into the MiG-19 fuselage, and the wide spine is a subtle detail that makes the aircraft look more “beefy” and less MiG-19-ish. The different drop tanks – even though they are authentic – visually add further speed. And despite many flaws, I am quite happy with the result of roundabout a week’s work.

Towards the end of 1914, early in World War I, disturbing rumours began to circulate that the newest German submarines were capable of a much higher surface speed than British boats, one report giving their speed at about 22 knots. The rumours were sufficiently strong to force serious consideration of the matter by the Admiralty, and at the same time consideration was given to the idea that submarines should have a high enough surface speed to be able to work with the fleet. The reports concerning the speed of the German submarines proved to be spurious, but the idea of a British submarine with a high surface speed gained ground. The immediate result of this concern was the development of the J Class, which were unique with their three shafts. Originally eight boats were planned but this was reduced to six and then increased to seven. As a result of these changes the boats originally intended to be J7 and J8 were renumbered in April 1915 as J3 and J4 respectively.

 

J7's submerged displacement of 1,760 tons was 60 tons less than that of her sister boats. Her conning tower was located further aft and the gun was mounted in a lower position.

 

HMS J7 commissioned in the Royal Navy on 15 September 1917 under the command of Lieutenant Commander F.H.D. Byron RN and was allocated to a flotilla based at Blyth, Northumberland.

 

On 5 November 1917 J7 departed Blyth for her first patrol. Whilst on patrol in the North Sea on 6 March 1918 an enemy submarine was sighted, but J7 was unable to attack and the enemy passed from sight.

 

The submarine was under refit during April and May 1918 at Walker Naval Yard on the River Tyne. She sailed for patrol on 25 May and evaded a U-boat attack the same day.

 

On 10 July an enemy submarine was sighted and both vessels dived. Shortly after a sighting was made of an enemy submarine on the surface, going away, J7 surfaced, challenged and opened fire. The enemy dived. An enemy submarine was sighted on 23 July, but J7 was unable to attack and the enemy disappeared.

 

On 5 October 1918 J7 dived to intercept a reported submarine, but broke off the search without contact.

 

The boat was at sea when the Armistice was signed on 11 November 1918. She returned to Blyth on 15 November. On 19 February 1919 she proceeded to Jarrow.

 

Following the conclusion of hostilities in World War I, the Admiralty in 1918 presented the six remaining boats of the J Class to the Australian Government - J6 had been sunk in error in 1918 by a British ship. All the submarines commissioned into the Royal Australian Navy at Portsmouth on 25 March 1919, as tenders to the submarine depot ship HMAS Platypus, J7 being the senior boat, under the command of Lieutenant Commander Oswald E. Hallifax DSO RN.

 

The beam tubes were removed from all six J Class submarines before they sailed for Australia. The tubes were despatched separately to Garden Island. The reasons given for the removal were that the beam tubes were not a success and that increased accommodation was required.

  

HMS Submarine J7 off the River Tyne prior to sailing for Australia in February, 1919.

On 9 April 1919 Platypus and the submarines, escorted by the light cruiser HMAS Sydney, sailed from Portsmouth for Australia, their first two ports of call being Gibraltar and Valetta.

 

On the night of 28 April, the night before the vessels arrived at Port Said, J3's starboard main engine shaft snapped. Thus handicapped she could not keep up with the others and consequently on departure for Aden on 30 April, J3 was in tow of Sydney.

 

The vessels arrived at Aden on 5 May. On the same day the light cruiser HMAS Brisbane, which had left Portsmouth on 17 April, also arrived. On 7 May all the vessels sailed for Colombo. Brisbane took over the tow of J3 while Sydney took J5 in tow as that boat had also developed engine trouble. Three days after arrival at Colombo on 15 May, Brisbane sailed with J5 in tow, taking her all the way to Sydney, where they arrived on 27 June.

 

J3 was taken in hand at Colombo for repairs. On 31 May Sydney, J1, J2, J4 and J7 sailed for Singapore, followed on 2 June by Platypus and J3. The vessels were reunited at Singapore from where all except Sydney sailed on 18 June. Sydney sailed for Australia a few days later but did not rejoin the other vessels. On 29 June Platypus and the five submarines arrived at Thursday Island, although J7 was three hours late because of trouble with her engine lubricating system. The last call before Sydney was Brisbane, Sydney being reached on 15 July.

 

Having arrived in poor condition, the submarines were taken in hand at Garden Island Dockyard for refitting. After her refit was completed J7 sailed for the submarine base at Geelong, Victoria.

 

After uneventful service, little of which was spent at sea, J7 and her five sisters paid off into Reserve at Westernport on 12 July 1922. The boats had become victims of the worsening economic conditions of the time, coupled with their high cost of maintenance.

 

On 1 November 1929 J7 was sold to Morris and Watt Pty Ltd of South Melbourne. She was towed from Flinders Naval Depot, Crib Point, where she had served as a reserve source of electric power, on 4 December 1929. She was dismantled and the hull sunk in 1930 as a breakwater at the Sandringham Yacht Club, Sandringham, Port Phillip Bay, where it remain

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based on historical facts. BEWARE!

  

Some Background:

The Lockheed F-94 Starfire was a first-generation jet aircraft of the United States Air Force. It was developed from the twin-seat Lockheed T-33 Shooting Star in the late 1940s as an all-weather, day/night interceptor, replacing the propeller-driven North American F-82 Twin Mustang in this role. The system was designed to overtake the F-80 in terms of performance, but more so to intercept the new high-level Soviet bombers capable of nuclear attacks on America and her Allies - in particular, the new Tupelov Tu-4. The F-94 was furthermore the first operational USAF fighter equipped with an afterburner and was the first jet-powered all-weather fighter to enter combat during the Korean War in January 1953.

 

The initial production model, the F-94A, entered operational service in May 1950. Its armament consisted of four 0.50 in (12.7 mm) M3 Browning machine guns mounted in the fuselage with the muzzles exiting under the radome for the APG-33 radar, a derivative from the AN/APG-3, which directed the Convair B-36's tail guns and had a range of up to 20 miles (32 km). Two 165 US Gallon (1,204 litre) drop tanks, as carried by the F-80 and T-33, were carried on the wingtips. Alternatively, these could be replaced by a pair of 1,000 lb (454 kg) bombs under the wings, giving the aircraft a secondary fighter bomber capability. 109 were produced.

 

The subsequent F-94B, which entered service in January 1951, was outwardly virtually identical to the F-94A. Its Allison J33 turbojet had a number of modifications made, though, which made it a very reliable engine. The pilot was provided with a roomier cockpit and the canopy received a bow frame in the center between the two crew members. A new Instrument Landing System (ILS) was fitted, too, which made operations at night and/or in bad weather much safer. However, this new variant’s punch with just four machine guns remained weak, and, to improve the load of fire, wing-mounted pods with two additional pairs of 0.5” machine guns were introduced – but these hardly improved the interceptor’s effectiveness. 356 of the F-94B were nevertheless built.

 

The following F-94C was extensively modified and initially designated F-97, but it was ultimately decided just to treat it as a new version of the F-94. USAF interest was lukewarm since aircraft technology had already developed at a fast pace – supersonic performance had already become standard. Lockheed funded development themselves, converting two F-94B airframes to YF-94C prototypes for evaluation with a completely new, much thinner wing, a swept tail surface and a more powerful Pratt & Whitney J48. This was a license-built version of the afterburning Rolls-Royce Tay, which produced a dry thrust of 6,350 pounds-force (28.2 kN) and approximately 8,750 pounds-force (38.9 kN) with afterburning. Instead of machine guns, the proposed new variant was exclusively armed with unguided air-to-air missiles.

Tests were positive and eventually the F-94C was adopted for USAF service, since it was the best interim solution for an all-weather fighter at that time. It still had to rely on Ground Control Interception Radar (GCI) sites to vector the interceptor to intruding aircraft, though.

 

The F-94C's introduction and the availability of the more effective Northrop F-89C/D Scorpion and the North American F-86D Sabre interceptors led to a quick relegation of the earlier F-94 variants from mid-1954 onwards to second line units and to Air National Guards. By 1955 most of them had already been phased out of USAF service, and some of these relatively young surplus machines were subsequently exported or handed over to friendly nations, too. When sent to the ANG, the F-94As were modified by Lockheed to F-94B standards and then returned to the ANG as B models. They primarily replaced outdated F-80C Shooting Stars and F-51D/H Mustangs.

 

At that time the USAF was looking for a tactical reconnaissance aircraft, a more effective successor for the RF-80A which had shown its worth and weaknesses during the Korea War. For instance, the plane could not fly at low altitude long enough to perform suitable visual reconnaissance, and its camera equipment was still based on WWII standards. Lockheed saw the opportunity to fill this operational gap with conversions of existing F-94A/B airframes, which had, in most cases, only had clocked few flying hours, primarily at high altitudes where Soviet bombers were expected to lurk, and still a lot of airframe life to offer. This led to another private venture, the RF-94B, auspiciously christened “Stargazer”.

 

The RF-94B was based on the F-94B interceptor with its J33 engine and the original unswept tail. The F-94B’s wings were retained but received a different leading-edge profile to better cope with operations at low altitude. The interceptor’s nose with the radome and the machine guns underneath was replaced by a new all-metal nose cone, which was more than 3 feet longer than the former radar nose, with windows for several sets of cameras; the wedge-shaped nose cone quickly earned the aircraft the unofficial nickname “Crocodile”.

One camera was looking ahead into flight direction and could be mounted at different angled downward (but not moved during flight), followed by two oblique cameras, looking to the left and the right, and a vertical camera as well as a long-range camera focussed on the horizon, which was behind a round window at port side. An additional, spacious compartment in front of the landing gear well held an innovative Tri-Metrogen horizon-to-horizon view system that consisted of three synchronized cameras. Coupled with a computerized control system based on light, speed, and altitude, it adjusted camera settings to produce pictures with greater delineation.

All cameras could be triggered individually by pilot or a dedicated observer/camera systems operator in the 2nd seat. Talking into a wire recorder, the crew could describe ground movements that might not have appeared in still pictures. A vertical view finder with a periscopic presentation on the cockpit panel was added for the pilot to enhance visual reconnaissance and target identification directly under the aircraft. Using magnesium flares carried under its wings in flash-ejector cartridges, the RF-94B was furthermore able to fly night missions.

The RF-94B was supposed to operate unarmed, but it could still carry a pair of 1.000 lb bombs under its wings or, thanks to added plumbings, an extra pair of drop tanks for ferry flights. The F-94A/B’s machine gun pods as well as the F-94C’s unguided missile launchers could be mounted to the wings, too, making it a viable attack aircraft in a secondary role.

 

The USAF was highly interested in this update proposal for the outdated interceptors (almost 500 F-94A/Bs had been built) and ordered 100 RF-94B conversions with an option for 100 more – just when a severe (and superior) competitor entered the stage after a lot of development troubles: Republic’s RF-84F Thunderflash reconnaissance version. The first YRF-84F had already been completed in February 1952 and it had an overall slightly better performance than the RF-94B. However, it offered more internal space for reconnaissance systems and was able to carry up to fifteen cameras with the support of many automatized systems, so that it was a single seater. Being largely identical to the F-84F and sharing its technical and logistical infrastructures, the USAF decided on short notice to change its procurement decision and rather adopt the more modern and promising Thunderflash as its standard tactical reconnaissance aircraft. The RF-94B conversion order was reduced to the initial 100 aircraft, and to avoid operational complexity these aircraft were exclusively delivered to Air National Guardss that had experience with the F-94A/B to replace their obsolete RF-80As.

 

Gradual replacement lasted until 1958, and while the RF-94B’s performance was overall better than the RF-80A’s, it was still disappointing and not the expected tactical intelligence gathering leap forward. The airframe did not cope well with constant low-level operations, and the aircraft’s marginal speed and handling did not ensure its survivability. However, unlike the RF-84F, which suffered from frequent engine problems, the Stargazers’ J33 made them highly reliable platforms – even though the complex Tri-Metrogen device turned out to be capricious, so that it was soon replaced with up to three standard cameras.

 

For better handling and less drag esp. at low altitude, the F-94B’s large Fletcher type wingtip tanks were frequently replaced with smaller ones with about half capacity. It also became common practice to operate the RF-94Bs with only a crew of one, and from 1960 on the RF-94B was, thanks to its second seat, more and more used as a trainer before pilots mounted more potent reconnaissance aircraft like the RF-101 Voodoo, which eventually replaced the RF-94B in ANG service. The last RF-94B was phased out in 1968, and, unlike the RF-84F, it was not operated by any foreign air force.

  

General characteristics:

Crew: 2 (but frequently operated by a single pilot)

Length: 43 ft 4 3/4 in (13.25 m)

Wingspan (with tip tanks): 40 ft 9 1/2 in (12.45 m)

Height: 12 ft. 2 (3.73 m)

Wing area: 234' 8" sq ft (29.11 m²)

Empty weight: 10,064 lb (4,570 kg)

Loaded weight: 15,330 lb (6,960 kg)

Max. takeoff weight: 24,184 lb (10,970 kg)

 

Powerplant:

1× Allison J33-A-33 turbojet, rated at 4,600 lbf (20.4 kN) continuous thrust,

5,400 lbf (24 kN) with water injection and 6,000 lbf (26.6 kN) thrust with afterburner

 

Performance:

Maximum speed: 630 mph (1,014 km/h) at height and in level flight

Range: 930 mi (813 nmi, 1,500 km) in combat configuration with two drop tanks

Ferry range: 1,457 mi (1,275 nmi, 2,345 km)

Service ceiling: 42,750 ft (14,000 m)

Rate of climb: 6,858 ft/min (34.9 m/s)

Wing loading: 57.4 lb/ft² (384 kg/m²)

Thrust/weight: 0.48

 

Armament:

No internal guns; 2x 165 US Gallon (1,204 liter) drop tanks on the wing tips and…

2x underwing hardpoints for two additional 165 US Gallon (1,204 liter) ferry tanks

or bombs of up to 1.000 lb (454 kg) caliber each, plus…

2x optional (rarely fitted) pods on the wings’ leading edges with either a pair of 0.5" (12.7 mm)

machine guns or twelve 2.75” (70 mm) Mk 4/Mk 40 Folding-Fin Aerial Rockets each

  

The kit and its assembly:

This project was originally earmarked as a submission for the 2021 “Reconnaissance & Surveillance” group build at whatifmodellers.com, in the form of a Heller F-94B with a new nose section. The inspiration behind this build was the real-world EF-94C (s/n 50-963): a solitary conversion with a bulbous camera nose. However, the EF-94C was not a reconnaissance aircraft but rather a chase plane/camera ship for the Air Research and Development Command, hence its unusual designation with the suffix “E”, standing for “Exempt” instead of the more appropriate “R” for a dedicated recce aircraft. There also was another EF-94C, but this was a totally different kind of aircraft: an ejection seat testbed.

 

I had a surplus Heller F-94B kit in The Stash™ and it was built almost completely OOB and did – except for some sinkholes and standard PSR work – not pose any problem. In fact, the old Heller Starfire model is IMHO a pretty good representation of the aircraft. O.K., its age might show, but almost anything you could ask for at 1:72 scale is there, including a decent, detailed cockpit.

 

The biggest change was the new camera nose, and it was scratched from an unlikely donor part: it consists of a Matchbox B-17G tail gunner station, slimmed down by the gunner station glazing's width at the seam in the middle, and this "sandwich" was furthermore turned upside down. Getting the transitional sections right took lots of PSR, though, and I added some styrene profiles to integrate the new nose into the rest of the hull. It was unintentional, but the new nose profile reminds a lot of a RF-101 recce Voodoo, and there's, with the straight wings, a very F-89ish look to the aircraft now? There's also something F2H-2ish about the outlines?

 

The large original wing tip tanks were cut off and replaced with smaller alternatives from a Hasegawa A-37. Because it was easy to realize on this kit I lowered the flaps, together with open ventral air brakes. The cockpit was taken OOB, I just modified the work station on the rear seat and replaced the rubber sight protector for the WSO with two screens for a camera operator. Finally, the one-piece cockpit glazing was cut into two parts to present the model with an open canopy.

  

Painting and markings:

This was a tough decision: either an NMF finish (the natural first choice), an overall light grey anti-corrosive coat of paint, both with relatively colorful unit markings, or camouflage. The USAF’s earlier RF-80As carried a unique scheme in olive drab/neutral grey with a medium waterline, but that would look rather vintage on the F-94. I decided that some tactical camouflage would make most sense on this kind of aircraft and eventually settled for the USAF’s SEA scheme with reduced tactical markings, which – after some field tests and improvisations in Vietnam – became standardized and was officially introduced to USAF aircraft around 1965 as well as to ANG units.

 

Even though I had already built a camouflaged F-94 some time ago (a Hellenic aircraft in worn SEA colors), I settled for this route. The basic colors (FS 30219, 34227, 34279 and 36622) all came from Humbrol (118, 117, 116 and 28, respectively), and for the pattern I adapted the paint scheme of the USAF’s probably only T-33 in SEA colors: a trainer based on Iceland during the Seventies and available as a markings option in one of the Special Hobby 1:32 T-33 kits. The low waterline received a wavy shape, inspired by an early ANG RF-101 in SEA camouflage I came across in a book. The new SEA scheme was apparently applied with a lot of enthusiasm and properness when it was brand new, but this quickly vaned. As an extra, the wing tip tanks received black anti-glare sections on their inner faces and a black anti-glare panel was added in front of the windscreen - a decal from a T-33 aftermarket sheet. Beyond a black ink wash the model received some subtle panel post-shading, but rather to emphasize surface details than for serious weathering.

 

The cockpit became very dark grey (Revell 06) while the landing gear wells were kept in zinc chromate green primer (Humbrol 80, Grass Green), with bright red (Humbrol 60, Matt Red) cover interiors and struts and wheels in aluminum (Humbrol 56). The interior of the flaps and the ventral air brakes became red, too.

 

The decals/markings came from a Special Hobby 1:72 F-86H; there’s a dedicated ANG boxing of the kit that comes with an optional camouflaged aircraft of the NY ANG, the least unit to operate the “Sabre Hog” during the Seventies. Since this 138th TFS formerly operated the F-94A/B, it was a perfect option for the RF-94B! I just used a different Bu. No. code on the fin, taken from a PrintScale A/T-37 set, and most stencils were perocured from the scrap box.

After a final light treatment with graphite around the afterburner for a more metallic shine of the iron metallic (Revell 97) underneath, the kit was sealed with a coat of matt acrylic varnish (Italeri).

  

A camouflaged F-94 is an unusual sight, but it works very well. The new/longer nose considerably changes the aircraft's profile, and even though the change is massive, the "Crocodile" looks surprisingly plausible, if not believable! And, despite the long nose, the aircraft looks pretty sleek, especially in the air.

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based historical facts. BEWARE!

  

The KAI T-50 Golden Eagle (골든이글) is a family of South Korean supersonic advanced trainers and light combat aircraft, developed by Korea Aerospace Industries (KAI) with Lockheed Martin. The T-50 is South Korea's first indigenous supersonic aircraft and one of the world's few supersonic trainers.

 

The T-50 program started in the late Nineties and was originally intended to develop an indigenous trainer aircraft capable of supersonic flight, to train and prepare pilots for the KF-16 and F-15K, replacing trainers such as T-38 and A-37 that were then in service with the ROKAF. Prior South Korean aircraft programs include the turboprop KT-1 basic trainer produced by Daewoo Aerospace (now part of KAI), and license-manufactured KF-16.

 

The mother program, code-named KTX-2, began in 1992, but the Ministry of Finance and Economy suspended the original project in 1995 due to financial constraints. The basic design of the aircraft was set by 1999, and eventually the development of the aircraft was funded 70% by the South Korean government, 17% by KAI, and 13% by Lockheed Martin.

 

In general, the T-50 series of aircraft closely resembles the KF-16 in configuration, but it actually is a completely new design: the T-50 is 11% smaller and 23% lighter than an F-16, and in order to create enough space for the two-seat cockpit, the air intake was bifurcated and placed under the wing gloves, resembling the F/A-18's layout.

 

The aircraft was formally designated as the T-50 'Golden Eagle' in February 2000, the T-50A designation had been reserved by the U.S. military to prevent it from being inadvertently assigned to another aircraft model. Final assembly of the first T-50 took place between 15 January and 14 September 2001. The first flight of the T-50 took place in August 2002, and initial operational assessment from 28 July to 14 August 2003.

 

The trainer has a cockpit for two pilots in a tandem arrangement, both crew members sitting in "normal" election seats, not in the F-16's reclined position. The high-mounted canopy is applied with stretched acrylic, providing the pilots with good visibility, and has been tested to offer the canopy with ballistic protection against 4-lb objects impacting at 400 knots.

 

The ROKAF, as original development driver, placed an initial production contract for 25 T-50s in December 2003, with aircraft scheduled to be delivered between 2005 and 2009. Original T-50 aircraft were equipped with the AN/APG-67(v)4 radar from Lockheed Martin. The T-50 trainer is powered by a GE F404 engine built under license by Samsung Techwin. Under the terms of the T-50/F404-102 co-production agreement, GE provides engine kits directly to Samsung Techwin who produces designated parts as well as performing final engine assembly and testing.

 

The T-50 program quickly expanded beyond a pure trainer concept to include the TA-50 armed trainer aircraft, as well as the FA-50 light attack aircraft, which has already similar capabilities as the multirole KF-16. Reconnaissance and electronic warfare variants were also being developed, designated as RA-50 and EA-50.

 

The TA-50 variant is a more heavily armed version of the T-50 trainer, intended for lead-in fighter training and light attack roles. It is equipped with an Elta EL/M-2032 fire control radar and designed to operate as a full-fledged combat platform. This variant mounts a lightweight three-barrel cannon version of the M61 Vulcan internally behind the cockpit, which fires linkless 20 mm ammunition. Wingtip rails can accommodate the AIM-9 Sidewinder missile, a variety of additional weapons can be mounted to underwing hardpoints, including precision-guided weapons, air-to-air missiles, and air-to-ground missiles. The TA-50 can also mount additional utility pods for reconnaissance, targeting assistance, and electronic warfare. Compatible air-to-surface weapons include the AGM-65 Maverick missile, Hydra 70 and LOGIR rocket launchers, CBU-58 and Mk-20 cluster bombs, and Mk-82, -83, and -84 general purpose bombs.

 

Among the operators of the TA-50 are the Philippines, Thailand and the ROKAF, and the type has attracted a global interest, also in Europe. The young Republic of Scotland Air Corps (locally known as Poblachd na h-Alba Adhair an Airm) chose, soon after the country's independence from the United Kingdom, after its departure from the European Union in 2017, the TA-50 as a complement to its initial procurements and add more flexibility to its small and young air arm.

 

According to a White Paper published by the Scottish National Party (SNP) in 2013, an independent Scotland would have an air force equipped with up to 16 air defense aircraft, six tactical transports, utility rotorcraft and maritime patrol aircraft, and be capable of “contributing excellent conventional capabilities” to NATO. Outlining its ambition to establish an air force with an eventual 2,000 uniformed personnel and 300 reservists, the SNP stated the organization would initially be equipped with “a minimum of 12 interceptors in the Eurofighter/Typhoon class, based at Lossiemouth, a tactical air transport squadron, including around six [Lockheed Martin] C-130J Hercules, and a helicopter squadron”.

 

According to the document, “Key elements of air forces in place at independence, equipped initially from a negotiated share of current UK assets, will secure core tasks, principally the ability to police Scotland’s airspace, within NATO.” An in-country air command and control capability would be established within five years of a decision in favor of independence, it continues, with staff also to be “embedded within NATO structures”.

This plan was immediately set into action after the country's independence in late 2017 with the purchase of twelve refurbished Saab JAS 39A Gripen interceptors for Quick Reaction Alert duties and upgraded, former Swedish Air Force Sk 90 trainers for the RoScAC. But these second hand machines were just the initial step in the mid-term procurement plan.

 

The twelve KAI TA-50 aircraft procured as a second step were to fulfill the complex requirement for a light and cost-effective multi-purpose aircraft that could be used in a wide variety of tasks: primarily as an advanced trainer for supersonic flight and as a trainer for the fighter role (since all Scottish Gripens were single seaters and dedicated to the interceptor/air defense role), but also as a light attack and point defense aircraft.

 

Scotland was offered refurbished F-16C and Ds, but this was declined as the type was deemed to be too costly and complex. Beyond the KAI T-50, the Alenia Aermacchi M-346 Master and the BAe Hawk were considered, too, but, eventually, a modified TA-50 that was tailored to the RoScAC’s procurement plans was chosen by the Scottish government.

 

In order to fulfill the complex duty profile, the Scottish TA-50s were upgraded with elements from the FA-50 attack aircraft. They possess more internal fuel capacity, enhanced avionics, a longer radome and a tactical datalink. Its EL/M-2032 pulse-Doppler radar has been modified so that it offers now a range two-thirds greater than the TA-50's standard radar. It enables the aircraft to operate in any weather, detect surface targets and deploy AIM-120 AAMs for BVR interceptions. The machines can also be externally fitted with Rafael's Sky Shield or LIG Nex1's ALQ-200K ECM pods, Sniper or LITENING targeting pods, and Condor 2 reconnaissance pods to further improve the machine’s electronic warfare, reconnaissance, and targeting capabilities.

 

Another unique feature of the Scottish Golden Eagle is its powerplant: even though the machines are originally powered by a single General Electric F404 afterburning turbofan and designed around this engine, the RoScAC TF-50s are powered by a Volvo RM12 low-bypass afterburning turbofan. These are procured and serviced through Saab in Sweden, as a part of the long-term collaboration contract for the RoScAC’s Saab Gripen fleet. This decision was taken in order to decrease overall fleet costs through a unified engine.

 

The RM12 is a derivative of the General Electric F404-400. Changes from the standard F404 includes greater reliability for single-engine operations (including more stringent birdstrike protection) and slightly increased thrust. Several subsystems and components were also re-designed to reduce maintenance demands, and the F404's analogue Engine Control Unit was replaced with the Digital Engine Control – jointly developed by Volvo and GE – which communicates with the cockpit through the digital data buses and, as redundancy, mechanical calculators controlled by a single wire will regulate the fuel-flow into the engine.

 

Another modification of the RoScAC’s TA-50 is the exchange of the original General Dynamics A-50 3-barrel rotary cannon for a single barrel Mauser BK-27 27mm revolver cannon. Being slightly heavier and having a lower cadence, the BK-27 featured a much higher kinetic energy, accuracy and range. Furthermore, the BK-27 is the standard weapon of the other, Sweden-built aircraft in RoScAC service, so that further synergies and cost reductions were expected.

 

The Scottish Department of National Defense announced the selection of the TA-50 in August 2018, after having procured refurbished Saab Sk 90 and JAS 39 Gripen from Sweden as initial outfit of the country's small air arm with No. 1 Squadron based at Lossiemouth AB.

 

Funding for the twelve aircraft was approved by Congress on September 2018 and worth € 420 mio., making the Golden Eagle the young country’s first brand new military aircraft. Deliveries of the Golden Hawk TF.1, how the type was officially designated in Scottish service, began in November 2019, lasting until December 2020.

The first four Scottish Golden Hawk TF.1 aircraft were allocated to the newly established RoScAC No. 2 Squadron, based at Leuchars, where the RoScAC took control from the British Army. The latter had just taken over the former air base from the RAF in 2015, losing its “RAF air base” status and was consequentially re-designated “Leuchars Station”, primarily catering to the Royal Scots Dragoon Guards who have, in the meantime, become part of Scotland’s Army Corps. The brand new machines were publically displayed on the shared army and air corps facility in the RoScAC’s new paint scheme on 1st of December 2019 for the first time, and immediately took up service.

 

General characteristics:

Crew: 2

Length: 13.14 m (43.1 ft)

Wingspan (with wingtip missiles): 9.45 m (31 ft)

Height: 4.94 m (16.2 ft)

Wing area: 23.69 m² (255 ft²)

Empty weight: 6,470 kg (14,285 lb)

Max. takeoff weight: 12,300 kg (27,300 lb)

 

Powerplant:

1× Volvo RM12 afterburning turbofan, rated at 54 kN (12,100 lbf) dry thrust

and 80.5 kN (18,100 lbf) with afterburner

 

Performance:

Maximum speed: Mach 1.5 (1,640 km/h, 1,020 mph at 9,144 m or 30,000 ft)

Range: 1,851 km (1,150 mi)

Service ceiling: 14,630 m (48,000 ft)

Rate of climb: 198 m/s (39,000 ft/min)

Thrust/weight: 0.96

Max g limit: -3 g / +8 g

 

Armament:

1× 27mm Mauser BK-27 revolver cannon with 120 rounds

A total of 7 hardpoints (4 underwing, 2 wingtip and one under fuselage)

for up to 3,740 kg (8,250 lb) of payload

  

The kit and its assembly:

A rare thing concerning my builds: an alternative reality whif. A fictional air force of an independent Scotland crept into my mind after the hysterical “Brexit” events in 2016 and the former (failed) public vote concerning the independence of Scotland from the UK. What would happen to the military, if the independence would take place, nevertheless, and British forces left the country?

 

The aforementioned Scottish National Party (SNP) paper from 2013 is real, and I took it as a benchmark. Primary focus would certainly be set on air space defense, and the Gripen appears as a good and not too expensive choice. The Sk 90 is a personal invention, but would fulfill a good complementary role.

Nevertheless, another multi-role aircraft would make sense as an addition, and both M-346 and T-50 caught my eye (Russian options were ruled out due to the tense political relations), and I gave the TA-50 the “Go” because of its engine and its proximity to the Gripen.

 

The T-50 really looks like the juvenile offspring from a date between an F-16 and an F-18. There’s even a kit available, from Academy – but it’s a Snap-Fit offering without a landing gear but, as an alternative, a clear display that can be attached to the engine nozzle. It also comes with stickers instead of waterslide decals. This sounds crappy and toy-like, but, after taking a close look at kit reviews, I gave it a try.

 

And I am positively surprised. While the kit consists of only few parts, moulded in the colors of a ROCAF trainer as expected, the surfaces have minute, engraved detail. Fit is very good, too, and there’s even a decent cockpit that’s actually better than the offering of some “normal” model kits. The interior comes with multi-part seats, side consoles and dashboards that feature correctly shaped instrument details (no decals). The air intakes are great, too: seamless, with relatively thin walls, nice!

 

So far, so good. But not enough. I could have built the kit OOB with the landing gear tucked up, but I went for the more complicated route and trans-/implanted the complete landing gear from an Intech F-16, which is available for less than EUR 5,- (and not much worth, to be honest). AFAIK, there’s white metal landing gear for the T-50 available from Scale Aircraft Conversions, but it’s 1:48 and for this set’s price I could have bought three Intech F-16s…

 

But back to the conversion. This landing gear transplantation stunt sounds more complicated as it actually turned out to be. For the front wheel well I simply cut a long opening into the fuselage and added inside a styrene sheet as a well roof, attached under the cockpit floor.

For the main landing gear I just opened the flush covers on the T-50 fuselage, cut out the interior from the Intech F-16, tailored it a little and glued it into its new place.

 

This was made easy by the fact that the T-50 is a bit smaller than the F-16, so that the transplants are by tendency a little too large and offer enough “flesh” for adaptations. Once in place, the F-16 struts were mounted (also slightly tailored to fit well) and covers added. The front wheel cover was created with 0.5 mm styrene sheet, for the main covers I used the parts from the Intech F-16 kit because they were thinner than the leftover T-50 fuselage parts and feature some surface detail on the inside. They had to be adapted in size, though. But the operation worked like a charm, highly recommended!

 

Around the hull, some small details like missing air scoops, some pitots and antennae were added. In a bout of boredom (while waiting for ordered parts…) I also added static dischargers on the aerodynamic surfaces’ trailing edges – the kit comes with obvious attachment points, and they are a small detail that improves the modern look of the T-50 even more.

 

Since the Academy kit comes clean with only a ventral drop tank as ordnance, underwing pylons from a SEPECAT Jaguar (resin aftermarket parts from Pavla) and a pair of AGM-65 from the Italeri NATO Weapons set plus launch rails were added, plus a pair of Sidewinders (from a Hasegawa AAM set, painted as blue training rounds) on the wing tip launch rails.

Since the T-50 trainer comes unarmed, a gun nozzle had to be added – its position is very similar to the gun on board of the F-16, on the upper side of the port side LERX. Another addition are conformal chaff/flare dispensers at the fin’s base, adding some beef to the sleek aircraft.

  

Painting and markings:

I did not want a grey-in-grey livery, yet something “different” and rather typical or familiar for the British isles. My approach is actually a compromise, with classic RAF colors and design features inspired by camouflage experiments of the German Luftwaffe on F-4F Phantoms and Alpha Jets in the early Eighties.

 

For the upper sides I went for a classic British scheme, in Dark Green and Dark Sea Grey (Humbrol 163 and 164), colors I deem very appropriate for the Scottish landscape and for potential naval operations. These were combined with elements from late RAF interceptors: Barley Grey (Humbrol 167) for the flanks including the pylons, plus Light Aircraft Grey (Humbrol 166) for the undersides, with a relatively high waterline and a grey fin, so that a side or lower view would rather blend with the sky than the ground below.

 

Another creative field were the national markings: how could fictional Scottish roundels look like, and how to create them so that they are easy to make and replicate (for a full set for this kit, as well as for potential future builds…)? Designing and printing marking decals myself was an option, but I eventually settled for a composite solution which somewhat influenced the roundels’ design, too.

My Scottish roundel interpretationconsists of a blue disk with a white cross – it’s simple, different from any other contemporary national marking, esp. the UK roundel, and easy to create from single decal parts. In fact, the blue roundels were die-punched from blue decal sheet, and the cross consists of two thin white decal strips, cut into the correct length with the same stencil, using generic sheet material from TL Modellbau.

 

Another issue was the potential tactical code, and a small fleet only needs a simple system. Going back to a WWII system with letter codes for squadrons and individual aircraft was one option, but, IMHO, too complicated. I adopted the British single letter aircraft code, though, since this system is very traditional, but since the RoScAC would certainly not operate too many squadrons, I rather adapted a system similar to the Swedish or Spanish format with a single number representing the squadron. The result is a simple 2-digit code, and I adapted the German system of placing the tactical code on the fuselage, separated by the roundel. Keeping British traditions up I repeated the individual aircraft code letter on the fin, where a Scottish flag, a small, self-printed Fife coat-or-arms and a serial number were added, too.

 

The kit saw only light weathering and shading, and the kit was finally sealed with matt acrylic varnish (Italeri).

  

Creating this whif, based on an alternative historic timeline with a near future perspective, was fun – and it might spawn more models that circle around the story. A Scottish Sk 90 and a Gripen are certain options (and for both I have kits in the stash…), but there might also be an entry level trainer, some helicopters for the army and SAR duties, as well as a transport aircraft. The foundation has been laid out, now it’s time to fill Scotland’s history to come with detail and proof. ;-)

 

Besides, despite being a snap-fit kit, Academy’s T-50 is a nice basis, reminding me of some Hobby Boss kits but with less flaws (e .g. most of the interiors), except for the complete lack of a landing gear. But with the F-16 and Jaguar transplants the simple kit developed into something more convincing.

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based historical facts. BEWARE!

  

The KAI T-50 Golden Eagle (골든이글) is a family of South Korean supersonic advanced trainers and light combat aircraft, developed by Korea Aerospace Industries (KAI) with Lockheed Martin. The T-50 is South Korea's first indigenous supersonic aircraft and one of the world's few supersonic trainers.

 

The T-50 program started in the late Nineties and was originally intended to develop an indigenous trainer aircraft capable of supersonic flight, to train and prepare pilots for the KF-16 and F-15K, replacing trainers such as T-38 and A-37 that were then in service with the ROKAF. Prior South Korean aircraft programs include the turboprop KT-1 basic trainer produced by Daewoo Aerospace (now part of KAI), and license-manufactured KF-16.

 

The mother program, code-named KTX-2, began in 1992, but the Ministry of Finance and Economy suspended the original project in 1995 due to financial constraints. The basic design of the aircraft was set by 1999, and eventually the development of the aircraft was funded 70% by the South Korean government, 17% by KAI, and 13% by Lockheed Martin.

 

In general, the T-50 series of aircraft closely resembles the KF-16 in configuration, but it actually is a completely new design: the T-50 is 11% smaller and 23% lighter than an F-16, and in order to create enough space for the two-seat cockpit, the air intake was bifurcated and placed under the wing gloves, resembling the F/A-18's layout.

 

The aircraft was formally designated as the T-50 'Golden Eagle' in February 2000, the T-50A designation had been reserved by the U.S. military to prevent it from being inadvertently assigned to another aircraft model. Final assembly of the first T-50 took place between 15 January and 14 September 2001. The first flight of the T-50 took place in August 2002, and initial operational assessment from 28 July to 14 August 2003.

 

The trainer has a cockpit for two pilots in a tandem arrangement, both crew members sitting in "normal" election seats, not in the F-16's reclined position. The high-mounted canopy is applied with stretched acrylic, providing the pilots with good visibility, and has been tested to offer the canopy with ballistic protection against 4-lb objects impacting at 400 knots.

 

The ROKAF, as original development driver, placed an initial production contract for 25 T-50s in December 2003, with aircraft scheduled to be delivered between 2005 and 2009. Original T-50 aircraft were equipped with the AN/APG-67(v)4 radar from Lockheed Martin. The T-50 trainer is powered by a GE F404 engine built under license by Samsung Techwin. Under the terms of the T-50/F404-102 co-production agreement, GE provides engine kits directly to Samsung Techwin who produces designated parts as well as performing final engine assembly and testing.

 

The T-50 program quickly expanded beyond a pure trainer concept to include the TA-50 armed trainer aircraft, as well as the FA-50 light attack aircraft, which has already similar capabilities as the multirole KF-16. Reconnaissance and electronic warfare variants were also being developed, designated as RA-50 and EA-50.

 

The TA-50 variant is a more heavily armed version of the T-50 trainer, intended for lead-in fighter training and light attack roles. It is equipped with an Elta EL/M-2032 fire control radar and designed to operate as a full-fledged combat platform. This variant mounts a lightweight three-barrel cannon version of the M61 Vulcan internally behind the cockpit, which fires linkless 20 mm ammunition. Wingtip rails can accommodate the AIM-9 Sidewinder missile, a variety of additional weapons can be mounted to underwing hardpoints, including precision-guided weapons, air-to-air missiles, and air-to-ground missiles. The TA-50 can also mount additional utility pods for reconnaissance, targeting assistance, and electronic warfare. Compatible air-to-surface weapons include the AGM-65 Maverick missile, Hydra 70 and LOGIR rocket launchers, CBU-58 and Mk-20 cluster bombs, and Mk-82, -83, and -84 general purpose bombs.

 

Among the operators of the TA-50 are the Philippines, Thailand and the ROKAF, and the type has attracted a global interest, also in Europe. The young Republic of Scotland Air Corps (locally known as Poblachd na h-Alba Adhair an Airm) chose, soon after the country's independence from the United Kingdom, after its departure from the European Union in 2017, the TA-50 as a complement to its initial procurements and add more flexibility to its small and young air arm.

 

According to a White Paper published by the Scottish National Party (SNP) in 2013, an independent Scotland would have an air force equipped with up to 16 air defense aircraft, six tactical transports, utility rotorcraft and maritime patrol aircraft, and be capable of “contributing excellent conventional capabilities” to NATO. Outlining its ambition to establish an air force with an eventual 2,000 uniformed personnel and 300 reservists, the SNP stated the organization would initially be equipped with “a minimum of 12 interceptors in the Eurofighter/Typhoon class, based at Lossiemouth, a tactical air transport squadron, including around six [Lockheed Martin] C-130J Hercules, and a helicopter squadron”.

 

According to the document, “Key elements of air forces in place at independence, equipped initially from a negotiated share of current UK assets, will secure core tasks, principally the ability to police Scotland’s airspace, within NATO.” An in-country air command and control capability would be established within five years of a decision in favor of independence, it continues, with staff also to be “embedded within NATO structures”.

This plan was immediately set into action after the country's independence in late 2017 with the purchase of twelve refurbished Saab JAS 39A Gripen interceptors for Quick Reaction Alert duties and upgraded, former Swedish Air Force Sk 90 trainers for the RoScAC. But these second hand machines were just the initial step in the mid-term procurement plan.

 

The twelve KAI TA-50 aircraft procured as a second step were to fulfill the complex requirement for a light and cost-effective multi-purpose aircraft that could be used in a wide variety of tasks: primarily as an advanced trainer for supersonic flight and as a trainer for the fighter role (since all Scottish Gripens were single seaters and dedicated to the interceptor/air defense role), but also as a light attack and point defense aircraft.

 

Scotland was offered refurbished F-16C and Ds, but this was declined as the type was deemed to be too costly and complex. Beyond the KAI T-50, the Alenia Aermacchi M-346 Master and the BAe Hawk were considered, too, but, eventually, a modified TA-50 that was tailored to the RoScAC’s procurement plans was chosen by the Scottish government.

 

In order to fulfill the complex duty profile, the Scottish TA-50s were upgraded with elements from the FA-50 attack aircraft. They possess more internal fuel capacity, enhanced avionics, a longer radome and a tactical datalink. Its EL/M-2032 pulse-Doppler radar has been modified so that it offers now a range two-thirds greater than the TA-50's standard radar. It enables the aircraft to operate in any weather, detect surface targets and deploy AIM-120 AAMs for BVR interceptions. The machines can also be externally fitted with Rafael's Sky Shield or LIG Nex1's ALQ-200K ECM pods, Sniper or LITENING targeting pods, and Condor 2 reconnaissance pods to further improve the machine’s electronic warfare, reconnaissance, and targeting capabilities.

 

Another unique feature of the Scottish Golden Eagle is its powerplant: even though the machines are originally powered by a single General Electric F404 afterburning turbofan and designed around this engine, the RoScAC TF-50s are powered by a Volvo RM12 low-bypass afterburning turbofan. These are procured and serviced through Saab in Sweden, as a part of the long-term collaboration contract for the RoScAC’s Saab Gripen fleet. This decision was taken in order to decrease overall fleet costs through a unified engine.

 

The RM12 is a derivative of the General Electric F404-400. Changes from the standard F404 includes greater reliability for single-engine operations (including more stringent birdstrike protection) and slightly increased thrust. Several subsystems and components were also re-designed to reduce maintenance demands, and the F404's analogue Engine Control Unit was replaced with the Digital Engine Control – jointly developed by Volvo and GE – which communicates with the cockpit through the digital data buses and, as redundancy, mechanical calculators controlled by a single wire will regulate the fuel-flow into the engine.

 

Another modification of the RoScAC’s TA-50 is the exchange of the original General Dynamics A-50 3-barrel rotary cannon for a single barrel Mauser BK-27 27mm revolver cannon. Being slightly heavier and having a lower cadence, the BK-27 featured a much higher kinetic energy, accuracy and range. Furthermore, the BK-27 is the standard weapon of the other, Sweden-built aircraft in RoScAC service, so that further synergies and cost reductions were expected.

 

The Scottish Department of National Defense announced the selection of the TA-50 in August 2018, after having procured refurbished Saab Sk 90 and JAS 39 Gripen from Sweden as initial outfit of the country's small air arm with No. 1 Squadron based at Lossiemouth AB.

 

Funding for the twelve aircraft was approved by Congress on September 2018 and worth € 420 mio., making the Golden Eagle the young country’s first brand new military aircraft. Deliveries of the Golden Hawk TF.1, how the type was officially designated in Scottish service, began in November 2019, lasting until December 2020.

The first four Scottish Golden Hawk TF.1 aircraft were allocated to the newly established RoScAC No. 2 Squadron, based at Leuchars, where the RoScAC took control from the British Army. The latter had just taken over the former air base from the RAF in 2015, losing its “RAF air base” status and was consequentially re-designated “Leuchars Station”, primarily catering to the Royal Scots Dragoon Guards who have, in the meantime, become part of Scotland’s Army Corps. The brand new machines were publically displayed on the shared army and air corps facility in the RoScAC’s new paint scheme on 1st of December 2019 for the first time, and immediately took up service.

 

General characteristics:

Crew: 2

Length: 13.14 m (43.1 ft)

Wingspan (with wingtip missiles): 9.45 m (31 ft)

Height: 4.94 m (16.2 ft)

Wing area: 23.69 m² (255 ft²)

Empty weight: 6,470 kg (14,285 lb)

Max. takeoff weight: 12,300 kg (27,300 lb)

 

Powerplant:

1× Volvo RM12 afterburning turbofan, rated at 54 kN (12,100 lbf) dry thrust

and 80.5 kN (18,100 lbf) with afterburner

 

Performance:

Maximum speed: Mach 1.5 (1,640 km/h, 1,020 mph at 9,144 m or 30,000 ft)

Range: 1,851 km (1,150 mi)

Service ceiling: 14,630 m (48,000 ft)

Rate of climb: 198 m/s (39,000 ft/min)

Thrust/weight: 0.96

Max g limit: -3 g / +8 g

 

Armament:

1× 27mm Mauser BK-27 revolver cannon with 120 rounds

A total of 7 hardpoints (4 underwing, 2 wingtip and one under fuselage)

for up to 3,740 kg (8,250 lb) of payload

  

The kit and its assembly:

A rare thing concerning my builds: an alternative reality whif. A fictional air force of an independent Scotland crept into my mind after the hysterical “Brexit” events in 2016 and the former (failed) public vote concerning the independence of Scotland from the UK. What would happen to the military, if the independence would take place, nevertheless, and British forces left the country?

 

The aforementioned Scottish National Party (SNP) paper from 2013 is real, and I took it as a benchmark. Primary focus would certainly be set on air space defense, and the Gripen appears as a good and not too expensive choice. The Sk 90 is a personal invention, but would fulfill a good complementary role.

Nevertheless, another multi-role aircraft would make sense as an addition, and both M-346 and T-50 caught my eye (Russian options were ruled out due to the tense political relations), and I gave the TA-50 the “Go” because of its engine and its proximity to the Gripen.

 

The T-50 really looks like the juvenile offspring from a date between an F-16 and an F-18. There’s even a kit available, from Academy – but it’s a Snap-Fit offering without a landing gear but, as an alternative, a clear display that can be attached to the engine nozzle. It also comes with stickers instead of waterslide decals. This sounds crappy and toy-like, but, after taking a close look at kit reviews, I gave it a try.

 

And I am positively surprised. While the kit consists of only few parts, moulded in the colors of a ROCAF trainer as expected, the surfaces have minute, engraved detail. Fit is very good, too, and there’s even a decent cockpit that’s actually better than the offering of some “normal” model kits. The interior comes with multi-part seats, side consoles and dashboards that feature correctly shaped instrument details (no decals). The air intakes are great, too: seamless, with relatively thin walls, nice!

 

So far, so good. But not enough. I could have built the kit OOB with the landing gear tucked up, but I went for the more complicated route and trans-/implanted the complete landing gear from an Intech F-16, which is available for less than EUR 5,- (and not much worth, to be honest). AFAIK, there’s white metal landing gear for the T-50 available from Scale Aircraft Conversions, but it’s 1:48 and for this set’s price I could have bought three Intech F-16s…

 

But back to the conversion. This landing gear transplantation stunt sounds more complicated as it actually turned out to be. For the front wheel well I simply cut a long opening into the fuselage and added inside a styrene sheet as a well roof, attached under the cockpit floor.

For the main landing gear I just opened the flush covers on the T-50 fuselage, cut out the interior from the Intech F-16, tailored it a little and glued it into its new place.

 

This was made easy by the fact that the T-50 is a bit smaller than the F-16, so that the transplants are by tendency a little too large and offer enough “flesh” for adaptations. Once in place, the F-16 struts were mounted (also slightly tailored to fit well) and covers added. The front wheel cover was created with 0.5 mm styrene sheet, for the main covers I used the parts from the Intech F-16 kit because they were thinner than the leftover T-50 fuselage parts and feature some surface detail on the inside. They had to be adapted in size, though. But the operation worked like a charm, highly recommended!

 

Around the hull, some small details like missing air scoops, some pitots and antennae were added. In a bout of boredom (while waiting for ordered parts…) I also added static dischargers on the aerodynamic surfaces’ trailing edges – the kit comes with obvious attachment points, and they are a small detail that improves the modern look of the T-50 even more.

 

Since the Academy kit comes clean with only a ventral drop tank as ordnance, underwing pylons from a SEPECAT Jaguar (resin aftermarket parts from Pavla) and a pair of AGM-65 from the Italeri NATO Weapons set plus launch rails were added, plus a pair of Sidewinders (from a Hasegawa AAM set, painted as blue training rounds) on the wing tip launch rails.

Since the T-50 trainer comes unarmed, a gun nozzle had to be added – its position is very similar to the gun on board of the F-16, on the upper side of the port side LERX. Another addition are conformal chaff/flare dispensers at the fin’s base, adding some beef to the sleek aircraft.

  

Painting and markings:

I did not want a grey-in-grey livery, yet something “different” and rather typical or familiar for the British isles. My approach is actually a compromise, with classic RAF colors and design features inspired by camouflage experiments of the German Luftwaffe on F-4F Phantoms and Alpha Jets in the early Eighties.

 

For the upper sides I went for a classic British scheme, in Dark Green and Dark Sea Grey (Humbrol 163 and 164), colors I deem very appropriate for the Scottish landscape and for potential naval operations. These were combined with elements from late RAF interceptors: Barley Grey (Humbrol 167) for the flanks including the pylons, plus Light Aircraft Grey (Humbrol 166) for the undersides, with a relatively high waterline and a grey fin, so that a side or lower view would rather blend with the sky than the ground below.

 

Another creative field were the national markings: how could fictional Scottish roundels look like, and how to create them so that they are easy to make and replicate (for a full set for this kit, as well as for potential future builds…)? Designing and printing marking decals myself was an option, but I eventually settled for a composite solution which somewhat influenced the roundels’ design, too.

My Scottish roundel interpretationconsists of a blue disk with a white cross – it’s simple, different from any other contemporary national marking, esp. the UK roundel, and easy to create from single decal parts. In fact, the blue roundels were die-punched from blue decal sheet, and the cross consists of two thin white decal strips, cut into the correct length with the same stencil, using generic sheet material from TL Modellbau.

 

Another issue was the potential tactical code, and a small fleet only needs a simple system. Going back to a WWII system with letter codes for squadrons and individual aircraft was one option, but, IMHO, too complicated. I adopted the British single letter aircraft code, though, since this system is very traditional, but since the RoScAC would certainly not operate too many squadrons, I rather adapted a system similar to the Swedish or Spanish format with a single number representing the squadron. The result is a simple 2-digit code, and I adapted the German system of placing the tactical code on the fuselage, separated by the roundel. Keeping British traditions up I repeated the individual aircraft code letter on the fin, where a Scottish flag, a small, self-printed Fife coat-or-arms and a serial number were added, too.

 

The kit saw only light weathering and shading, and the kit was finally sealed with matt acrylic varnish (Italeri).

  

Creating this whif, based on an alternative historic timeline with a near future perspective, was fun – and it might spawn more models that circle around the story. A Scottish Sk 90 and a Gripen are certain options (and for both I have kits in the stash…), but there might also be an entry level trainer, some helicopters for the army and SAR duties, as well as a transport aircraft. The foundation has been laid out, now it’s time to fill Scotland’s history to come with detail and proof. ;-)

 

Besides, despite being a snap-fit kit, Academy’s T-50 is a nice basis, reminding me of some Hobby Boss kits but with less flaws (e .g. most of the interiors), except for the complete lack of a landing gear. But with the F-16 and Jaguar transplants the simple kit developed into something more convincing.

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based historical facts. BEWARE!

  

The KAI T-50 Golden Eagle (골든이글) is a family of South Korean supersonic advanced trainers and light combat aircraft, developed by Korea Aerospace Industries (KAI) with Lockheed Martin. The T-50 is South Korea's first indigenous supersonic aircraft and one of the world's few supersonic trainers.

 

The T-50 program started in the late Nineties and was originally intended to develop an indigenous trainer aircraft capable of supersonic flight, to train and prepare pilots for the KF-16 and F-15K, replacing trainers such as T-38 and A-37 that were then in service with the ROKAF. Prior South Korean aircraft programs include the turboprop KT-1 basic trainer produced by Daewoo Aerospace (now part of KAI), and license-manufactured KF-16.

 

The mother program, code-named KTX-2, began in 1992, but the Ministry of Finance and Economy suspended the original project in 1995 due to financial constraints. The basic design of the aircraft was set by 1999, and eventually the development of the aircraft was funded 70% by the South Korean government, 17% by KAI, and 13% by Lockheed Martin.

 

In general, the T-50 series of aircraft closely resembles the KF-16 in configuration, but it actually is a completely new design: the T-50 is 11% smaller and 23% lighter than an F-16, and in order to create enough space for the two-seat cockpit, the air intake was bifurcated and placed under the wing gloves, resembling the F/A-18's layout.

 

The aircraft was formally designated as the T-50 'Golden Eagle' in February 2000, the T-50A designation had been reserved by the U.S. military to prevent it from being inadvertently assigned to another aircraft model. Final assembly of the first T-50 took place between 15 January and 14 September 2001. The first flight of the T-50 took place in August 2002, and initial operational assessment from 28 July to 14 August 2003.

 

The trainer has a cockpit for two pilots in a tandem arrangement, both crew members sitting in "normal" election seats, not in the F-16's reclined position. The high-mounted canopy is applied with stretched acrylic, providing the pilots with good visibility, and has been tested to offer the canopy with ballistic protection against 4-lb objects impacting at 400 knots.

 

The ROKAF, as original development driver, placed an initial production contract for 25 T-50s in December 2003, with aircraft scheduled to be delivered between 2005 and 2009. Original T-50 aircraft were equipped with the AN/APG-67(v)4 radar from Lockheed Martin. The T-50 trainer is powered by a GE F404 engine built under license by Samsung Techwin. Under the terms of the T-50/F404-102 co-production agreement, GE provides engine kits directly to Samsung Techwin who produces designated parts as well as performing final engine assembly and testing.

 

The T-50 program quickly expanded beyond a pure trainer concept to include the TA-50 armed trainer aircraft, as well as the FA-50 light attack aircraft, which has already similar capabilities as the multirole KF-16. Reconnaissance and electronic warfare variants were also being developed, designated as RA-50 and EA-50.

 

The TA-50 variant is a more heavily armed version of the T-50 trainer, intended for lead-in fighter training and light attack roles. It is equipped with an Elta EL/M-2032 fire control radar and designed to operate as a full-fledged combat platform. This variant mounts a lightweight three-barrel cannon version of the M61 Vulcan internally behind the cockpit, which fires linkless 20 mm ammunition. Wingtip rails can accommodate the AIM-9 Sidewinder missile, a variety of additional weapons can be mounted to underwing hardpoints, including precision-guided weapons, air-to-air missiles, and air-to-ground missiles. The TA-50 can also mount additional utility pods for reconnaissance, targeting assistance, and electronic warfare. Compatible air-to-surface weapons include the AGM-65 Maverick missile, Hydra 70 and LOGIR rocket launchers, CBU-58 and Mk-20 cluster bombs, and Mk-82, -83, and -84 general purpose bombs.

 

Among the operators of the TA-50 are the Philippines, Thailand and the ROKAF, and the type has attracted a global interest, also in Europe. The young Republic of Scotland Air Corps (locally known as Poblachd na h-Alba Adhair an Airm) chose, soon after the country's independence from the United Kingdom, after its departure from the European Union in 2017, the TA-50 as a complement to its initial procurements and add more flexibility to its small and young air arm.

 

According to a White Paper published by the Scottish National Party (SNP) in 2013, an independent Scotland would have an air force equipped with up to 16 air defense aircraft, six tactical transports, utility rotorcraft and maritime patrol aircraft, and be capable of “contributing excellent conventional capabilities” to NATO. Outlining its ambition to establish an air force with an eventual 2,000 uniformed personnel and 300 reservists, the SNP stated the organization would initially be equipped with “a minimum of 12 interceptors in the Eurofighter/Typhoon class, based at Lossiemouth, a tactical air transport squadron, including around six [Lockheed Martin] C-130J Hercules, and a helicopter squadron”.

 

According to the document, “Key elements of air forces in place at independence, equipped initially from a negotiated share of current UK assets, will secure core tasks, principally the ability to police Scotland’s airspace, within NATO.” An in-country air command and control capability would be established within five years of a decision in favor of independence, it continues, with staff also to be “embedded within NATO structures”.

This plan was immediately set into action after the country's independence in late 2017 with the purchase of twelve refurbished Saab JAS 39A Gripen interceptors for Quick Reaction Alert duties and upgraded, former Swedish Air Force Sk 90 trainers for the RoScAC. But these second hand machines were just the initial step in the mid-term procurement plan.

 

The twelve KAI TA-50 aircraft procured as a second step were to fulfill the complex requirement for a light and cost-effective multi-purpose aircraft that could be used in a wide variety of tasks: primarily as an advanced trainer for supersonic flight and as a trainer for the fighter role (since all Scottish Gripens were single seaters and dedicated to the interceptor/air defense role), but also as a light attack and point defense aircraft.

 

Scotland was offered refurbished F-16C and Ds, but this was declined as the type was deemed to be too costly and complex. Beyond the KAI T-50, the Alenia Aermacchi M-346 Master and the BAe Hawk were considered, too, but, eventually, a modified TA-50 that was tailored to the RoScAC’s procurement plans was chosen by the Scottish government.

 

In order to fulfill the complex duty profile, the Scottish TA-50s were upgraded with elements from the FA-50 attack aircraft. They possess more internal fuel capacity, enhanced avionics, a longer radome and a tactical datalink. Its EL/M-2032 pulse-Doppler radar has been modified so that it offers now a range two-thirds greater than the TA-50's standard radar. It enables the aircraft to operate in any weather, detect surface targets and deploy AIM-120 AAMs for BVR interceptions. The machines can also be externally fitted with Rafael's Sky Shield or LIG Nex1's ALQ-200K ECM pods, Sniper or LITENING targeting pods, and Condor 2 reconnaissance pods to further improve the machine’s electronic warfare, reconnaissance, and targeting capabilities.

 

Another unique feature of the Scottish Golden Eagle is its powerplant: even though the machines are originally powered by a single General Electric F404 afterburning turbofan and designed around this engine, the RoScAC TF-50s are powered by a Volvo RM12 low-bypass afterburning turbofan. These are procured and serviced through Saab in Sweden, as a part of the long-term collaboration contract for the RoScAC’s Saab Gripen fleet. This decision was taken in order to decrease overall fleet costs through a unified engine.

 

The RM12 is a derivative of the General Electric F404-400. Changes from the standard F404 includes greater reliability for single-engine operations (including more stringent birdstrike protection) and slightly increased thrust. Several subsystems and components were also re-designed to reduce maintenance demands, and the F404's analogue Engine Control Unit was replaced with the Digital Engine Control – jointly developed by Volvo and GE – which communicates with the cockpit through the digital data buses and, as redundancy, mechanical calculators controlled by a single wire will regulate the fuel-flow into the engine.

 

Another modification of the RoScAC’s TA-50 is the exchange of the original General Dynamics A-50 3-barrel rotary cannon for a single barrel Mauser BK-27 27mm revolver cannon. Being slightly heavier and having a lower cadence, the BK-27 featured a much higher kinetic energy, accuracy and range. Furthermore, the BK-27 is the standard weapon of the other, Sweden-built aircraft in RoScAC service, so that further synergies and cost reductions were expected.

 

The Scottish Department of National Defense announced the selection of the TA-50 in August 2018, after having procured refurbished Saab Sk 90 and JAS 39 Gripen from Sweden as initial outfit of the country's small air arm with No. 1 Squadron based at Lossiemouth AB.

 

Funding for the twelve aircraft was approved by Congress on September 2018 and worth € 420 mio., making the Golden Eagle the young country’s first brand new military aircraft. Deliveries of the Golden Hawk TF.1, how the type was officially designated in Scottish service, began in November 2019, lasting until December 2020.

The first four Scottish Golden Hawk TF.1 aircraft were allocated to the newly established RoScAC No. 2 Squadron, based at Leuchars, where the RoScAC took control from the British Army. The latter had just taken over the former air base from the RAF in 2015, losing its “RAF air base” status and was consequentially re-designated “Leuchars Station”, primarily catering to the Royal Scots Dragoon Guards who have, in the meantime, become part of Scotland’s Army Corps. The brand new machines were publically displayed on the shared army and air corps facility in the RoScAC’s new paint scheme on 1st of December 2019 for the first time, and immediately took up service.

 

General characteristics:

Crew: 2

Length: 13.14 m (43.1 ft)

Wingspan (with wingtip missiles): 9.45 m (31 ft)

Height: 4.94 m (16.2 ft)

Wing area: 23.69 m² (255 ft²)

Empty weight: 6,470 kg (14,285 lb)

Max. takeoff weight: 12,300 kg (27,300 lb)

 

Powerplant:

1× Volvo RM12 afterburning turbofan, rated at 54 kN (12,100 lbf) dry thrust

and 80.5 kN (18,100 lbf) with afterburner

 

Performance:

Maximum speed: Mach 1.5 (1,640 km/h, 1,020 mph at 9,144 m or 30,000 ft)

Range: 1,851 km (1,150 mi)

Service ceiling: 14,630 m (48,000 ft)

Rate of climb: 198 m/s (39,000 ft/min)

Thrust/weight: 0.96

Max g limit: -3 g / +8 g

 

Armament:

1× 27mm Mauser BK-27 revolver cannon with 120 rounds

A total of 7 hardpoints (4 underwing, 2 wingtip and one under fuselage)

for up to 3,740 kg (8,250 lb) of payload

  

The kit and its assembly:

A rare thing concerning my builds: an alternative reality whif. A fictional air force of an independent Scotland crept into my mind after the hysterical “Brexit” events in 2016 and the former (failed) public vote concerning the independence of Scotland from the UK. What would happen to the military, if the independence would take place, nevertheless, and British forces left the country?

 

The aforementioned Scottish National Party (SNP) paper from 2013 is real, and I took it as a benchmark. Primary focus would certainly be set on air space defense, and the Gripen appears as a good and not too expensive choice. The Sk 90 is a personal invention, but would fulfill a good complementary role.

Nevertheless, another multi-role aircraft would make sense as an addition, and both M-346 and T-50 caught my eye (Russian options were ruled out due to the tense political relations), and I gave the TA-50 the “Go” because of its engine and its proximity to the Gripen.

 

The T-50 really looks like the juvenile offspring from a date between an F-16 and an F-18. There’s even a kit available, from Academy – but it’s a Snap-Fit offering without a landing gear but, as an alternative, a clear display that can be attached to the engine nozzle. It also comes with stickers instead of waterslide decals. This sounds crappy and toy-like, but, after taking a close look at kit reviews, I gave it a try.

 

And I am positively surprised. While the kit consists of only few parts, moulded in the colors of a ROCAF trainer as expected, the surfaces have minute, engraved detail. Fit is very good, too, and there’s even a decent cockpit that’s actually better than the offering of some “normal” model kits. The interior comes with multi-part seats, side consoles and dashboards that feature correctly shaped instrument details (no decals). The air intakes are great, too: seamless, with relatively thin walls, nice!

 

So far, so good. But not enough. I could have built the kit OOB with the landing gear tucked up, but I went for the more complicated route and trans-/implanted the complete landing gear from an Intech F-16, which is available for less than EUR 5,- (and not much worth, to be honest). AFAIK, there’s white metal landing gear for the T-50 available from Scale Aircraft Conversions, but it’s 1:48 and for this set’s price I could have bought three Intech F-16s…

 

But back to the conversion. This landing gear transplantation stunt sounds more complicated as it actually turned out to be. For the front wheel well I simply cut a long opening into the fuselage and added inside a styrene sheet as a well roof, attached under the cockpit floor.

For the main landing gear I just opened the flush covers on the T-50 fuselage, cut out the interior from the Intech F-16, tailored it a little and glued it into its new place.

 

This was made easy by the fact that the T-50 is a bit smaller than the F-16, so that the transplants are by tendency a little too large and offer enough “flesh” for adaptations. Once in place, the F-16 struts were mounted (also slightly tailored to fit well) and covers added. The front wheel cover was created with 0.5 mm styrene sheet, for the main covers I used the parts from the Intech F-16 kit because they were thinner than the leftover T-50 fuselage parts and feature some surface detail on the inside. They had to be adapted in size, though. But the operation worked like a charm, highly recommended!

 

Around the hull, some small details like missing air scoops, some pitots and antennae were added. In a bout of boredom (while waiting for ordered parts…) I also added static dischargers on the aerodynamic surfaces’ trailing edges – the kit comes with obvious attachment points, and they are a small detail that improves the modern look of the T-50 even more.

 

Since the Academy kit comes clean with only a ventral drop tank as ordnance, underwing pylons from a SEPECAT Jaguar (resin aftermarket parts from Pavla) and a pair of AGM-65 from the Italeri NATO Weapons set plus launch rails were added, plus a pair of Sidewinders (from a Hasegawa AAM set, painted as blue training rounds) on the wing tip launch rails.

Since the T-50 trainer comes unarmed, a gun nozzle had to be added – its position is very similar to the gun on board of the F-16, on the upper side of the port side LERX. Another addition are conformal chaff/flare dispensers at the fin’s base, adding some beef to the sleek aircraft.

  

Painting and markings:

I did not want a grey-in-grey livery, yet something “different” and rather typical or familiar for the British isles. My approach is actually a compromise, with classic RAF colors and design features inspired by camouflage experiments of the German Luftwaffe on F-4F Phantoms and Alpha Jets in the early Eighties.

 

For the upper sides I went for a classic British scheme, in Dark Green and Dark Sea Grey (Humbrol 163 and 164), colors I deem very appropriate for the Scottish landscape and for potential naval operations. These were combined with elements from late RAF interceptors: Barley Grey (Humbrol 167) for the flanks including the pylons, plus Light Aircraft Grey (Humbrol 166) for the undersides, with a relatively high waterline and a grey fin, so that a side or lower view would rather blend with the sky than the ground below.

 

Another creative field were the national markings: how could fictional Scottish roundels look like, and how to create them so that they are easy to make and replicate (for a full set for this kit, as well as for potential future builds…)? Designing and printing marking decals myself was an option, but I eventually settled for a composite solution which somewhat influenced the roundels’ design, too.

My Scottish roundel interpretationconsists of a blue disk with a white cross – it’s simple, different from any other contemporary national marking, esp. the UK roundel, and easy to create from single decal parts. In fact, the blue roundels were die-punched from blue decal sheet, and the cross consists of two thin white decal strips, cut into the correct length with the same stencil, using generic sheet material from TL Modellbau.

 

Another issue was the potential tactical code, and a small fleet only needs a simple system. Going back to a WWII system with letter codes for squadrons and individual aircraft was one option, but, IMHO, too complicated. I adopted the British single letter aircraft code, though, since this system is very traditional, but since the RoScAC would certainly not operate too many squadrons, I rather adapted a system similar to the Swedish or Spanish format with a single number representing the squadron. The result is a simple 2-digit code, and I adapted the German system of placing the tactical code on the fuselage, separated by the roundel. Keeping British traditions up I repeated the individual aircraft code letter on the fin, where a Scottish flag, a small, self-printed Fife coat-or-arms and a serial number were added, too.

 

The kit saw only light weathering and shading, and the kit was finally sealed with matt acrylic varnish (Italeri).

  

Creating this whif, based on an alternative historic timeline with a near future perspective, was fun – and it might spawn more models that circle around the story. A Scottish Sk 90 and a Gripen are certain options (and for both I have kits in the stash…), but there might also be an entry level trainer, some helicopters for the army and SAR duties, as well as a transport aircraft. The foundation has been laid out, now it’s time to fill Scotland’s history to come with detail and proof. ;-)

 

Besides, despite being a snap-fit kit, Academy’s T-50 is a nice basis, reminding me of some Hobby Boss kits but with less flaws (e .g. most of the interiors), except for the complete lack of a landing gear. But with the F-16 and Jaguar transplants the simple kit developed into something more convincing.

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based historical facts. BEWARE!

  

The KAI T-50 Golden Eagle (골든이글) is a family of South Korean supersonic advanced trainers and light combat aircraft, developed by Korea Aerospace Industries (KAI) with Lockheed Martin. The T-50 is South Korea's first indigenous supersonic aircraft and one of the world's few supersonic trainers.

 

The T-50 program started in the late Nineties and was originally intended to develop an indigenous trainer aircraft capable of supersonic flight, to train and prepare pilots for the KF-16 and F-15K, replacing trainers such as T-38 and A-37 that were then in service with the ROKAF. Prior South Korean aircraft programs include the turboprop KT-1 basic trainer produced by Daewoo Aerospace (now part of KAI), and license-manufactured KF-16.

 

The mother program, code-named KTX-2, began in 1992, but the Ministry of Finance and Economy suspended the original project in 1995 due to financial constraints. The basic design of the aircraft was set by 1999, and eventually the development of the aircraft was funded 70% by the South Korean government, 17% by KAI, and 13% by Lockheed Martin.

 

In general, the T-50 series of aircraft closely resembles the KF-16 in configuration, but it actually is a completely new design: the T-50 is 11% smaller and 23% lighter than an F-16, and in order to create enough space for the two-seat cockpit, the air intake was bifurcated and placed under the wing gloves, resembling the F/A-18's layout.

 

The aircraft was formally designated as the T-50 'Golden Eagle' in February 2000, the T-50A designation had been reserved by the U.S. military to prevent it from being inadvertently assigned to another aircraft model. Final assembly of the first T-50 took place between 15 January and 14 September 2001. The first flight of the T-50 took place in August 2002, and initial operational assessment from 28 July to 14 August 2003.

 

The trainer has a cockpit for two pilots in a tandem arrangement, both crew members sitting in "normal" election seats, not in the F-16's reclined position. The high-mounted canopy is applied with stretched acrylic, providing the pilots with good visibility, and has been tested to offer the canopy with ballistic protection against 4-lb objects impacting at 400 knots.

 

The ROKAF, as original development driver, placed an initial production contract for 25 T-50s in December 2003, with aircraft scheduled to be delivered between 2005 and 2009. Original T-50 aircraft were equipped with the AN/APG-67(v)4 radar from Lockheed Martin. The T-50 trainer is powered by a GE F404 engine built under license by Samsung Techwin. Under the terms of the T-50/F404-102 co-production agreement, GE provides engine kits directly to Samsung Techwin who produces designated parts as well as performing final engine assembly and testing.

 

The T-50 program quickly expanded beyond a pure trainer concept to include the TA-50 armed trainer aircraft, as well as the FA-50 light attack aircraft, which has already similar capabilities as the multirole KF-16. Reconnaissance and electronic warfare variants were also being developed, designated as RA-50 and EA-50.

 

The TA-50 variant is a more heavily armed version of the T-50 trainer, intended for lead-in fighter training and light attack roles. It is equipped with an Elta EL/M-2032 fire control radar and designed to operate as a full-fledged combat platform. This variant mounts a lightweight three-barrel cannon version of the M61 Vulcan internally behind the cockpit, which fires linkless 20 mm ammunition. Wingtip rails can accommodate the AIM-9 Sidewinder missile, a variety of additional weapons can be mounted to underwing hardpoints, including precision-guided weapons, air-to-air missiles, and air-to-ground missiles. The TA-50 can also mount additional utility pods for reconnaissance, targeting assistance, and electronic warfare. Compatible air-to-surface weapons include the AGM-65 Maverick missile, Hydra 70 and LOGIR rocket launchers, CBU-58 and Mk-20 cluster bombs, and Mk-82, -83, and -84 general purpose bombs.

 

Among the operators of the TA-50 are the Philippines, Thailand and the ROKAF, and the type has attracted a global interest, also in Europe. The young Republic of Scotland Air Corps (locally known as Poblachd na h-Alba Adhair an Airm) chose, soon after the country's independence from the United Kingdom, after its departure from the European Union in 2017, the TA-50 as a complement to its initial procurements and add more flexibility to its small and young air arm.

 

According to a White Paper published by the Scottish National Party (SNP) in 2013, an independent Scotland would have an air force equipped with up to 16 air defense aircraft, six tactical transports, utility rotorcraft and maritime patrol aircraft, and be capable of “contributing excellent conventional capabilities” to NATO. Outlining its ambition to establish an air force with an eventual 2,000 uniformed personnel and 300 reservists, the SNP stated the organization would initially be equipped with “a minimum of 12 interceptors in the Eurofighter/Typhoon class, based at Lossiemouth, a tactical air transport squadron, including around six [Lockheed Martin] C-130J Hercules, and a helicopter squadron”.

 

According to the document, “Key elements of air forces in place at independence, equipped initially from a negotiated share of current UK assets, will secure core tasks, principally the ability to police Scotland’s airspace, within NATO.” An in-country air command and control capability would be established within five years of a decision in favor of independence, it continues, with staff also to be “embedded within NATO structures”.

This plan was immediately set into action after the country's independence in late 2017 with the purchase of twelve refurbished Saab JAS 39A Gripen interceptors for Quick Reaction Alert duties and upgraded, former Swedish Air Force Sk 90 trainers for the RoScAC. But these second hand machines were just the initial step in the mid-term procurement plan.

 

The twelve KAI TA-50 aircraft procured as a second step were to fulfill the complex requirement for a light and cost-effective multi-purpose aircraft that could be used in a wide variety of tasks: primarily as an advanced trainer for supersonic flight and as a trainer for the fighter role (since all Scottish Gripens were single seaters and dedicated to the interceptor/air defense role), but also as a light attack and point defense aircraft.

 

Scotland was offered refurbished F-16C and Ds, but this was declined as the type was deemed to be too costly and complex. Beyond the KAI T-50, the Alenia Aermacchi M-346 Master and the BAe Hawk were considered, too, but, eventually, a modified TA-50 that was tailored to the RoScAC’s procurement plans was chosen by the Scottish government.

 

In order to fulfill the complex duty profile, the Scottish TA-50s were upgraded with elements from the FA-50 attack aircraft. They possess more internal fuel capacity, enhanced avionics, a longer radome and a tactical datalink. Its EL/M-2032 pulse-Doppler radar has been modified so that it offers now a range two-thirds greater than the TA-50's standard radar. It enables the aircraft to operate in any weather, detect surface targets and deploy AIM-120 AAMs for BVR interceptions. The machines can also be externally fitted with Rafael's Sky Shield or LIG Nex1's ALQ-200K ECM pods, Sniper or LITENING targeting pods, and Condor 2 reconnaissance pods to further improve the machine’s electronic warfare, reconnaissance, and targeting capabilities.

 

Another unique feature of the Scottish Golden Eagle is its powerplant: even though the machines are originally powered by a single General Electric F404 afterburning turbofan and designed around this engine, the RoScAC TF-50s are powered by a Volvo RM12 low-bypass afterburning turbofan. These are procured and serviced through Saab in Sweden, as a part of the long-term collaboration contract for the RoScAC’s Saab Gripen fleet. This decision was taken in order to decrease overall fleet costs through a unified engine.

 

The RM12 is a derivative of the General Electric F404-400. Changes from the standard F404 includes greater reliability for single-engine operations (including more stringent birdstrike protection) and slightly increased thrust. Several subsystems and components were also re-designed to reduce maintenance demands, and the F404's analogue Engine Control Unit was replaced with the Digital Engine Control – jointly developed by Volvo and GE – which communicates with the cockpit through the digital data buses and, as redundancy, mechanical calculators controlled by a single wire will regulate the fuel-flow into the engine.

 

Another modification of the RoScAC’s TA-50 is the exchange of the original General Dynamics A-50 3-barrel rotary cannon for a single barrel Mauser BK-27 27mm revolver cannon. Being slightly heavier and having a lower cadence, the BK-27 featured a much higher kinetic energy, accuracy and range. Furthermore, the BK-27 is the standard weapon of the other, Sweden-built aircraft in RoScAC service, so that further synergies and cost reductions were expected.

 

The Scottish Department of National Defense announced the selection of the TA-50 in August 2018, after having procured refurbished Saab Sk 90 and JAS 39 Gripen from Sweden as initial outfit of the country's small air arm with No. 1 Squadron based at Lossiemouth AB.

 

Funding for the twelve aircraft was approved by Congress on September 2018 and worth € 420 mio., making the Golden Eagle the young country’s first brand new military aircraft. Deliveries of the Golden Hawk TF.1, how the type was officially designated in Scottish service, began in November 2019, lasting until December 2020.

The first four Scottish Golden Hawk TF.1 aircraft were allocated to the newly established RoScAC No. 2 Squadron, based at Leuchars, where the RoScAC took control from the British Army. The latter had just taken over the former air base from the RAF in 2015, losing its “RAF air base” status and was consequentially re-designated “Leuchars Station”, primarily catering to the Royal Scots Dragoon Guards who have, in the meantime, become part of Scotland’s Army Corps. The brand new machines were publically displayed on the shared army and air corps facility in the RoScAC’s new paint scheme on 1st of December 2019 for the first time, and immediately took up service.

 

General characteristics:

Crew: 2

Length: 13.14 m (43.1 ft)

Wingspan (with wingtip missiles): 9.45 m (31 ft)

Height: 4.94 m (16.2 ft)

Wing area: 23.69 m² (255 ft²)

Empty weight: 6,470 kg (14,285 lb)

Max. takeoff weight: 12,300 kg (27,300 lb)

 

Powerplant:

1× Volvo RM12 afterburning turbofan, rated at 54 kN (12,100 lbf) dry thrust

and 80.5 kN (18,100 lbf) with afterburner

 

Performance:

Maximum speed: Mach 1.5 (1,640 km/h, 1,020 mph at 9,144 m or 30,000 ft)

Range: 1,851 km (1,150 mi)

Service ceiling: 14,630 m (48,000 ft)

Rate of climb: 198 m/s (39,000 ft/min)

Thrust/weight: 0.96

Max g limit: -3 g / +8 g

 

Armament:

1× 27mm Mauser BK-27 revolver cannon with 120 rounds

A total of 7 hardpoints (4 underwing, 2 wingtip and one under fuselage)

for up to 3,740 kg (8,250 lb) of payload

  

The kit and its assembly:

A rare thing concerning my builds: an alternative reality whif. A fictional air force of an independent Scotland crept into my mind after the hysterical “Brexit” events in 2016 and the former (failed) public vote concerning the independence of Scotland from the UK. What would happen to the military, if the independence would take place, nevertheless, and British forces left the country?

 

The aforementioned Scottish National Party (SNP) paper from 2013 is real, and I took it as a benchmark. Primary focus would certainly be set on air space defense, and the Gripen appears as a good and not too expensive choice. The Sk 90 is a personal invention, but would fulfill a good complementary role.

Nevertheless, another multi-role aircraft would make sense as an addition, and both M-346 and T-50 caught my eye (Russian options were ruled out due to the tense political relations), and I gave the TA-50 the “Go” because of its engine and its proximity to the Gripen.

 

The T-50 really looks like the juvenile offspring from a date between an F-16 and an F-18. There’s even a kit available, from Academy – but it’s a Snap-Fit offering without a landing gear but, as an alternative, a clear display that can be attached to the engine nozzle. It also comes with stickers instead of waterslide decals. This sounds crappy and toy-like, but, after taking a close look at kit reviews, I gave it a try.

 

And I am positively surprised. While the kit consists of only few parts, moulded in the colors of a ROCAF trainer as expected, the surfaces have minute, engraved detail. Fit is very good, too, and there’s even a decent cockpit that’s actually better than the offering of some “normal” model kits. The interior comes with multi-part seats, side consoles and dashboards that feature correctly shaped instrument details (no decals). The air intakes are great, too: seamless, with relatively thin walls, nice!

 

So far, so good. But not enough. I could have built the kit OOB with the landing gear tucked up, but I went for the more complicated route and trans-/implanted the complete landing gear from an Intech F-16, which is available for less than EUR 5,- (and not much worth, to be honest). AFAIK, there’s white metal landing gear for the T-50 available from Scale Aircraft Conversions, but it’s 1:48 and for this set’s price I could have bought three Intech F-16s…

 

But back to the conversion. This landing gear transplantation stunt sounds more complicated as it actually turned out to be. For the front wheel well I simply cut a long opening into the fuselage and added inside a styrene sheet as a well roof, attached under the cockpit floor.

For the main landing gear I just opened the flush covers on the T-50 fuselage, cut out the interior from the Intech F-16, tailored it a little and glued it into its new place.

 

This was made easy by the fact that the T-50 is a bit smaller than the F-16, so that the transplants are by tendency a little too large and offer enough “flesh” for adaptations. Once in place, the F-16 struts were mounted (also slightly tailored to fit well) and covers added. The front wheel cover was created with 0.5 mm styrene sheet, for the main covers I used the parts from the Intech F-16 kit because they were thinner than the leftover T-50 fuselage parts and feature some surface detail on the inside. They had to be adapted in size, though. But the operation worked like a charm, highly recommended!

 

Around the hull, some small details like missing air scoops, some pitots and antennae were added. In a bout of boredom (while waiting for ordered parts…) I also added static dischargers on the aerodynamic surfaces’ trailing edges – the kit comes with obvious attachment points, and they are a small detail that improves the modern look of the T-50 even more.

 

Since the Academy kit comes clean with only a ventral drop tank as ordnance, underwing pylons from a SEPECAT Jaguar (resin aftermarket parts from Pavla) and a pair of AGM-65 from the Italeri NATO Weapons set plus launch rails were added, plus a pair of Sidewinders (from a Hasegawa AAM set, painted as blue training rounds) on the wing tip launch rails.

Since the T-50 trainer comes unarmed, a gun nozzle had to be added – its position is very similar to the gun on board of the F-16, on the upper side of the port side LERX. Another addition are conformal chaff/flare dispensers at the fin’s base, adding some beef to the sleek aircraft.

  

Painting and markings:

I did not want a grey-in-grey livery, yet something “different” and rather typical or familiar for the British isles. My approach is actually a compromise, with classic RAF colors and design features inspired by camouflage experiments of the German Luftwaffe on F-4F Phantoms and Alpha Jets in the early Eighties.

 

For the upper sides I went for a classic British scheme, in Dark Green and Dark Sea Grey (Humbrol 163 and 164), colors I deem very appropriate for the Scottish landscape and for potential naval operations. These were combined with elements from late RAF interceptors: Barley Grey (Humbrol 167) for the flanks including the pylons, plus Light Aircraft Grey (Humbrol 166) for the undersides, with a relatively high waterline and a grey fin, so that a side or lower view would rather blend with the sky than the ground below.

 

Another creative field were the national markings: how could fictional Scottish roundels look like, and how to create them so that they are easy to make and replicate (for a full set for this kit, as well as for potential future builds…)? Designing and printing marking decals myself was an option, but I eventually settled for a composite solution which somewhat influenced the roundels’ design, too.

My Scottish roundel interpretationconsists of a blue disk with a white cross – it’s simple, different from any other contemporary national marking, esp. the UK roundel, and easy to create from single decal parts. In fact, the blue roundels were die-punched from blue decal sheet, and the cross consists of two thin white decal strips, cut into the correct length with the same stencil, using generic sheet material from TL Modellbau.

 

Another issue was the potential tactical code, and a small fleet only needs a simple system. Going back to a WWII system with letter codes for squadrons and individual aircraft was one option, but, IMHO, too complicated. I adopted the British single letter aircraft code, though, since this system is very traditional, but since the RoScAC would certainly not operate too many squadrons, I rather adapted a system similar to the Swedish or Spanish format with a single number representing the squadron. The result is a simple 2-digit code, and I adapted the German system of placing the tactical code on the fuselage, separated by the roundel. Keeping British traditions up I repeated the individual aircraft code letter on the fin, where a Scottish flag, a small, self-printed Fife coat-or-arms and a serial number were added, too.

 

The kit saw only light weathering and shading, and the kit was finally sealed with matt acrylic varnish (Italeri).

  

Creating this whif, based on an alternative historic timeline with a near future perspective, was fun – and it might spawn more models that circle around the story. A Scottish Sk 90 and a Gripen are certain options (and for both I have kits in the stash…), but there might also be an entry level trainer, some helicopters for the army and SAR duties, as well as a transport aircraft. The foundation has been laid out, now it’s time to fill Scotland’s history to come with detail and proof. ;-)

 

Besides, despite being a snap-fit kit, Academy’s T-50 is a nice basis, reminding me of some Hobby Boss kits but with less flaws (e .g. most of the interiors), except for the complete lack of a landing gear. But with the F-16 and Jaguar transplants the simple kit developed into something more convincing.

French public debt at record high French debt in percentage of GDP value. French public debt decreased in 2013, but is still higher than expected. Total debt continues to climb and fails to meet the Maastricht criteria. EurActiv France reports. Despite austerity measures, France's public deficit did not meet its government targets for 2013. The French National Institute of Statistics and Economic Studies (INSEE) published figures showing that it currently stands at 4.3% of GDP.The French government expected this percentage to be 4.1%, whilst the European Commission predicted 4.2%. However timid, the reduction of public deficit from its previous level of 4.9%, in 2013, is still a significant improvement. Struggling with revenue On closer inspection, the statistics should worry the French government. Although expenses reached target reductions from 3% in 2012 to 2%¨in 2013, revenue is lower than expected. Revenue has decreased from 3.3% compared to 3.7% in 2012. The state has reduced its financial needs, but those of local administrations have increased. According to a press release from the French Ministry of Budget, Public Accounts and Civil Administration, “measures to restore public accounts recorded a historical 2.5 percentage points of GDP, whereas unfavourable economic conditions adversely affected revenues by 1.5 percentage points. The implementation of expenditure, consistent with expectations, proves the government’s ability to meet spending targets set by the parliament”. Almost €2000 billion of debt France's Ministry of Finance criticised the debt-to-GDP ratio, and called for a change in the calculation. According to the INSEE, public debt was 93%, or €1925 billion, in 2013, a new record, and higher than the €1841 billion recorded in 2012. The French Ministry of Finance argues that this number should not include financial support provided to European states like Greece, Spain or Portugal. It should also exclude the contributions made to the European Stability Mechanism, the measure put in place to help ailing banks. When excluding financial support to troubled countries, and the capitalisation of the European Stability Mechanism, the debt ratio is 90.4% of GDP. The Minister of Economy highlights that “it would then be in line with government forecasts,” and effectively blames the EU for another French mishandling of public accounts. Socialist leaders in concerted push to relax EU budgetary constraints

Le Pen eyes VP role in new far-right EU Parliament group Brussels wages new battle against VAT fraud. ECB rate cut boosts Spanish, Italian yields Insurance companies push forward with European investment EU fines SIM card chip cartel €138 million UK government: Independent Scotland can't both rejoin the EU and keep the pound

French bosses rally around Juncker's 300 billion investment plan France is one of the countries of which the public debt exceeds economic convergence criteria set out by the Treaty of Maastricht, both in terms of annual deficit and total volume of debt. According to the treaty, public deficit should not exceed 3% of GDP, and public debt should be limited to 60% of GDP.Macroeconomic and public finance predictions for 2014-2017 should be provided to the parliament within the stability programme in mid-April and to the Commission before 30 April.The Juncker team revealed Ukraine to request NATO membership Putin: ‘I can take Kiev in two weeks if I want’ Britain handed climate and energy portfolio in draft Juncker Commission line-up Parliament reacts to Juncker’s plan to merge energy and climate portfolios Poroshenko: The EU's agenda now revolves around Ukraine Bildt slams Juncker over absence of enlargement portfolio Cyber threat now ‘real and growing’, EU official warns Commission cautiously welcomes news of Ukraine ‘ceasefire’ EU considers ban on Russian bond-buying as part of new sanctions package

Efficacité et Transparence des Acteurs Européens © 1999-2014 EurActiv.com PLC | Terms and Conditions...As history has shown, France is capable of the best and the worst, and often in short periods of time. On the day following Marine Le Pen's Front National victory in the European elections, however, France made a decisive contribution to the reinvention of a radical politics for the 21st century. On that day, the committee for a citizen's audit on the public debt issued a 30-page report on French public debt, its origins and evolution in the past decades. The report was written by a group of experts in public finances under the coordination of Michel Husson, one of France's finest critical economists. Its conclusion is straightforward: 60% of French public debt is illegitimate. Anyone who has read a newspaper in recent years knows how important debt is to contemporary politics. As David Graeber among others has shown, we live in debtocracies, not democracies. Debt, rather than popular will, is the governing principle of our societies, through the devastating austerity policies implemented in the name of debt reduction. Debt was also a triggering cause of the most innovative social movements in recent years, the Occupy movement. If it were shown that public debts were somehow illegitimate, that citizens had a right to demand a moratorium – and even the cancellation of part of these debts – the political implications would be huge. It is hard to think of an event that would transform social life as profoundly and rapidly as the emancipation of societies from the constraints of debt. And yet this is precisely what the French report aims to do. The audit is part of a wider movement of popular debt audits in more than 18 countries. Ecuador and Brazil have had theirs, the former at the initiative of Rafael Correa's government, the latter organised by civil society. European social movements have also put in place debt audits, especially in countries harder hit by the sovereign debt crisis, such as Greece and Spain. In Tunisia, the post-revolutionary government declared the debt taken out during Ben Ali's dictatorship an "odious" debt: one that served to enrich the clique in power, rather than improving the living conditions of the people. The report on French debt contains several key findings. Primarily, the rise in the state's debt in the past decades cannot be explained by an increase in public spending. The neoliberal argument in favour of austerity policies claims that debt is due to unreasonable public spending levels; that societies in general, and popular classes in particular, live above their means. This is plain false. In the past 30 years, from 1978 to 2012 more precisely, French public spending has in fact decreased by two GDP points. What, then, explains the rise in public debt? First, a fall in the tax revenues of the state. Massive tax reductions for the wealthy and big corporations have been carried out since 1980. In line with the neoliberal mantra, the purpose of these reductions was to favour investment and employment. Well, unemployment is at its highest today, whereas tax revenues have decreased by five points of GDP.The second factor is the increase in interest rates, especially in the 1990s. This increase favoured creditors and speculators, to the detriment of debtors. Instead of borrowing on financial markets at prohibitive interest rates, had the state financed itself by appealing to household savings and banks, and borrowed at historically normal rates, the public debt would be inferior to current levels by 29 GDP points. Tax reductions for the wealthy and interest rates increases are political decisions. What the audit shows is that public deficits do not just grow naturally out of the normal course of social life. They are deliberately inflicted on society by the dominant classes, to legitimise austerity policies that will allow the transfer of value from the working classes to the wealthy ones. A stunning finding of the report is that no one actually knows who holds the French debt. To finance its debt, the French state, like any other state, issues bonds, which are bought by a set of authorised banks. These banks then sell the bonds on the global financial markets. Who owns these titles is one of the world's best kept secrets. The state pays interests to the holders, so technically it could know who owns them. Yet a legally organised ignorance forbids the disclosure of the identity of the bond holders. This deliberate organisation of ignorance – agnotology – in neoliberal economies intentionally renders the state powerless, even when it could have the means to know and act. This is what permits tax evasion in its various forms – which last year cost about €50bn to European societies, and €17bn to France alone. Hence, the audit on the debt concludes, some 60% of the French public debt is illegitimate. An illegitimate debt is one that grew in the service of private interests, and not the wellbeing of the people. Therefore the French people have a right to demand a moratorium on the payment of the debt, and the cancellation of at least part of it. There is precedent for this: in 2008 Ecuador declared 70% of its debt illegitimate. The nascent global movement for debt audits may well contain the seeds of a new internationalism – an internationalism for today – in the working classes throughout the world. This is, among other things, a consequence of financialisation. Thus debt audits might provide a fertile ground for renewed forms of international mobilisations and solidarity.

This new internationalism could start with three easy steps. 1) Debt audits in all countries The crucial point is to demonstrate, as the French audit did, that debt is a political construction, that it doesn't just happen to societies when they supposedly live above their means. This is what justifies calling it illegitimate, and may lead to cancellation procedures. Audits on private debts are also possible, as the Chilean artist Francisco Tapia has recently shown by auditing student loans in an imaginative way. 2) The disclosure of the identity of debt holders A directory of creditors at national and international levels could be assembled. Not only would such a directory help fight tax evasion, it would also reveal that while the living conditions of the majority are worsening, a small group of individuals and financial institutions has consistently taken advantage of high levels of public indebtedness. Hence, it would reveal the political nature of debt. 3) The socialisation of the banking system The state should cease to borrow on financial markets, instead financing itself through households and banks at reasonable and controllable interest rates. The banks themselves should be put under the supervision of citizens' committees, hence rendering the audit on the debt permanent. In short, debt should be democratised. This, of course, is the harder part, where elements of socialism are introduced at the very core of the system. Yet, to counter the tyranny of debt on every aspect of our lives, there is no alternative.

  

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based historical facts. BEWARE!

  

The KAI T-50 Golden Eagle (골든이글) is a family of South Korean supersonic advanced trainers and light combat aircraft, developed by Korea Aerospace Industries (KAI) with Lockheed Martin. The T-50 is South Korea's first indigenous supersonic aircraft and one of the world's few supersonic trainers.

 

The T-50 program started in the late Nineties and was originally intended to develop an indigenous trainer aircraft capable of supersonic flight, to train and prepare pilots for the KF-16 and F-15K, replacing trainers such as T-38 and A-37 that were then in service with the ROKAF. Prior South Korean aircraft programs include the turboprop KT-1 basic trainer produced by Daewoo Aerospace (now part of KAI), and license-manufactured KF-16.

 

The mother program, code-named KTX-2, began in 1992, but the Ministry of Finance and Economy suspended the original project in 1995 due to financial constraints. The basic design of the aircraft was set by 1999, and eventually the development of the aircraft was funded 70% by the South Korean government, 17% by KAI, and 13% by Lockheed Martin.

 

In general, the T-50 series of aircraft closely resembles the KF-16 in configuration, but it actually is a completely new design: the T-50 is 11% smaller and 23% lighter than an F-16, and in order to create enough space for the two-seat cockpit, the air intake was bifurcated and placed under the wing gloves, resembling the F/A-18's layout.

 

The aircraft was formally designated as the T-50 'Golden Eagle' in February 2000, the T-50A designation had been reserved by the U.S. military to prevent it from being inadvertently assigned to another aircraft model. Final assembly of the first T-50 took place between 15 January and 14 September 2001. The first flight of the T-50 took place in August 2002, and initial operational assessment from 28 July to 14 August 2003.

 

The trainer has a cockpit for two pilots in a tandem arrangement, both crew members sitting in "normal" election seats, not in the F-16's reclined position. The high-mounted canopy is applied with stretched acrylic, providing the pilots with good visibility, and has been tested to offer the canopy with ballistic protection against 4-lb objects impacting at 400 knots.

 

The ROKAF, as original development driver, placed an initial production contract for 25 T-50s in December 2003, with aircraft scheduled to be delivered between 2005 and 2009. Original T-50 aircraft were equipped with the AN/APG-67(v)4 radar from Lockheed Martin. The T-50 trainer is powered by a GE F404 engine built under license by Samsung Techwin. Under the terms of the T-50/F404-102 co-production agreement, GE provides engine kits directly to Samsung Techwin who produces designated parts as well as performing final engine assembly and testing.

 

The T-50 program quickly expanded beyond a pure trainer concept to include the TA-50 armed trainer aircraft, as well as the FA-50 light attack aircraft, which has already similar capabilities as the multirole KF-16. Reconnaissance and electronic warfare variants were also being developed, designated as RA-50 and EA-50.

 

The TA-50 variant is a more heavily armed version of the T-50 trainer, intended for lead-in fighter training and light attack roles. It is equipped with an Elta EL/M-2032 fire control radar and designed to operate as a full-fledged combat platform. This variant mounts a lightweight three-barrel cannon version of the M61 Vulcan internally behind the cockpit, which fires linkless 20 mm ammunition. Wingtip rails can accommodate the AIM-9 Sidewinder missile, a variety of additional weapons can be mounted to underwing hardpoints, including precision-guided weapons, air-to-air missiles, and air-to-ground missiles. The TA-50 can also mount additional utility pods for reconnaissance, targeting assistance, and electronic warfare. Compatible air-to-surface weapons include the AGM-65 Maverick missile, Hydra 70 and LOGIR rocket launchers, CBU-58 and Mk-20 cluster bombs, and Mk-82, -83, and -84 general purpose bombs.

 

Among the operators of the TA-50 are the Philippines, Thailand and the ROKAF, and the type has attracted a global interest, also in Europe. The young Republic of Scotland Air Corps (locally known as Poblachd na h-Alba Adhair an Airm) chose, soon after the country's independence from the United Kingdom, after its departure from the European Union in 2017, the TA-50 as a complement to its initial procurements and add more flexibility to its small and young air arm.

 

According to a White Paper published by the Scottish National Party (SNP) in 2013, an independent Scotland would have an air force equipped with up to 16 air defense aircraft, six tactical transports, utility rotorcraft and maritime patrol aircraft, and be capable of “contributing excellent conventional capabilities” to NATO. Outlining its ambition to establish an air force with an eventual 2,000 uniformed personnel and 300 reservists, the SNP stated the organization would initially be equipped with “a minimum of 12 interceptors in the Eurofighter/Typhoon class, based at Lossiemouth, a tactical air transport squadron, including around six [Lockheed Martin] C-130J Hercules, and a helicopter squadron”.

 

According to the document, “Key elements of air forces in place at independence, equipped initially from a negotiated share of current UK assets, will secure core tasks, principally the ability to police Scotland’s airspace, within NATO.” An in-country air command and control capability would be established within five years of a decision in favor of independence, it continues, with staff also to be “embedded within NATO structures”.

This plan was immediately set into action after the country's independence in late 2017 with the purchase of twelve refurbished Saab JAS 39A Gripen interceptors for Quick Reaction Alert duties and upgraded, former Swedish Air Force Sk 90 trainers for the RoScAC. But these second hand machines were just the initial step in the mid-term procurement plan.

 

The twelve KAI TA-50 aircraft procured as a second step were to fulfill the complex requirement for a light and cost-effective multi-purpose aircraft that could be used in a wide variety of tasks: primarily as an advanced trainer for supersonic flight and as a trainer for the fighter role (since all Scottish Gripens were single seaters and dedicated to the interceptor/air defense role), but also as a light attack and point defense aircraft.

 

Scotland was offered refurbished F-16C and Ds, but this was declined as the type was deemed to be too costly and complex. Beyond the KAI T-50, the Alenia Aermacchi M-346 Master and the BAe Hawk were considered, too, but, eventually, a modified TA-50 that was tailored to the RoScAC’s procurement plans was chosen by the Scottish government.

 

In order to fulfill the complex duty profile, the Scottish TA-50s were upgraded with elements from the FA-50 attack aircraft. They possess more internal fuel capacity, enhanced avionics, a longer radome and a tactical datalink. Its EL/M-2032 pulse-Doppler radar has been modified so that it offers now a range two-thirds greater than the TA-50's standard radar. It enables the aircraft to operate in any weather, detect surface targets and deploy AIM-120 AAMs for BVR interceptions. The machines can also be externally fitted with Rafael's Sky Shield or LIG Nex1's ALQ-200K ECM pods, Sniper or LITENING targeting pods, and Condor 2 reconnaissance pods to further improve the machine’s electronic warfare, reconnaissance, and targeting capabilities.

 

Another unique feature of the Scottish Golden Eagle is its powerplant: even though the machines are originally powered by a single General Electric F404 afterburning turbofan and designed around this engine, the RoScAC TF-50s are powered by a Volvo RM12 low-bypass afterburning turbofan. These are procured and serviced through Saab in Sweden, as a part of the long-term collaboration contract for the RoScAC’s Saab Gripen fleet. This decision was taken in order to decrease overall fleet costs through a unified engine.

 

The RM12 is a derivative of the General Electric F404-400. Changes from the standard F404 includes greater reliability for single-engine operations (including more stringent birdstrike protection) and slightly increased thrust. Several subsystems and components were also re-designed to reduce maintenance demands, and the F404's analogue Engine Control Unit was replaced with the Digital Engine Control – jointly developed by Volvo and GE – which communicates with the cockpit through the digital data buses and, as redundancy, mechanical calculators controlled by a single wire will regulate the fuel-flow into the engine.

 

Another modification of the RoScAC’s TA-50 is the exchange of the original General Dynamics A-50 3-barrel rotary cannon for a single barrel Mauser BK-27 27mm revolver cannon. Being slightly heavier and having a lower cadence, the BK-27 featured a much higher kinetic energy, accuracy and range. Furthermore, the BK-27 is the standard weapon of the other, Sweden-built aircraft in RoScAC service, so that further synergies and cost reductions were expected.

 

The Scottish Department of National Defense announced the selection of the TA-50 in August 2018, after having procured refurbished Saab Sk 90 and JAS 39 Gripen from Sweden as initial outfit of the country's small air arm with No. 1 Squadron based at Lossiemouth AB.

 

Funding for the twelve aircraft was approved by Congress on September 2018 and worth € 420 mio., making the Golden Eagle the young country’s first brand new military aircraft. Deliveries of the Golden Hawk TF.1, how the type was officially designated in Scottish service, began in November 2019, lasting until December 2020.

The first four Scottish Golden Hawk TF.1 aircraft were allocated to the newly established RoScAC No. 2 Squadron, based at Leuchars, where the RoScAC took control from the British Army. The latter had just taken over the former air base from the RAF in 2015, losing its “RAF air base” status and was consequentially re-designated “Leuchars Station”, primarily catering to the Royal Scots Dragoon Guards who have, in the meantime, become part of Scotland’s Army Corps. The brand new machines were publically displayed on the shared army and air corps facility in the RoScAC’s new paint scheme on 1st of December 2019 for the first time, and immediately took up service.

 

General characteristics:

Crew: 2

Length: 13.14 m (43.1 ft)

Wingspan (with wingtip missiles): 9.45 m (31 ft)

Height: 4.94 m (16.2 ft)

Wing area: 23.69 m² (255 ft²)

Empty weight: 6,470 kg (14,285 lb)

Max. takeoff weight: 12,300 kg (27,300 lb)

 

Powerplant:

1× Volvo RM12 afterburning turbofan, rated at 54 kN (12,100 lbf) dry thrust

and 80.5 kN (18,100 lbf) with afterburner

 

Performance:

Maximum speed: Mach 1.5 (1,640 km/h, 1,020 mph at 9,144 m or 30,000 ft)

Range: 1,851 km (1,150 mi)

Service ceiling: 14,630 m (48,000 ft)

Rate of climb: 198 m/s (39,000 ft/min)

Thrust/weight: 0.96

Max g limit: -3 g / +8 g

 

Armament:

1× 27mm Mauser BK-27 revolver cannon with 120 rounds

A total of 7 hardpoints (4 underwing, 2 wingtip and one under fuselage)

for up to 3,740 kg (8,250 lb) of payload

  

The kit and its assembly:

A rare thing concerning my builds: an alternative reality whif. A fictional air force of an independent Scotland crept into my mind after the hysterical “Brexit” events in 2016 and the former (failed) public vote concerning the independence of Scotland from the UK. What would happen to the military, if the independence would take place, nevertheless, and British forces left the country?

 

The aforementioned Scottish National Party (SNP) paper from 2013 is real, and I took it as a benchmark. Primary focus would certainly be set on air space defense, and the Gripen appears as a good and not too expensive choice. The Sk 90 is a personal invention, but would fulfill a good complementary role.

Nevertheless, another multi-role aircraft would make sense as an addition, and both M-346 and T-50 caught my eye (Russian options were ruled out due to the tense political relations), and I gave the TA-50 the “Go” because of its engine and its proximity to the Gripen.

 

The T-50 really looks like the juvenile offspring from a date between an F-16 and an F-18. There’s even a kit available, from Academy – but it’s a Snap-Fit offering without a landing gear but, as an alternative, a clear display that can be attached to the engine nozzle. It also comes with stickers instead of waterslide decals. This sounds crappy and toy-like, but, after taking a close look at kit reviews, I gave it a try.

 

And I am positively surprised. While the kit consists of only few parts, moulded in the colors of a ROCAF trainer as expected, the surfaces have minute, engraved detail. Fit is very good, too, and there’s even a decent cockpit that’s actually better than the offering of some “normal” model kits. The interior comes with multi-part seats, side consoles and dashboards that feature correctly shaped instrument details (no decals). The air intakes are great, too: seamless, with relatively thin walls, nice!

 

So far, so good. But not enough. I could have built the kit OOB with the landing gear tucked up, but I went for the more complicated route and trans-/implanted the complete landing gear from an Intech F-16, which is available for less than EUR 5,- (and not much worth, to be honest). AFAIK, there’s white metal landing gear for the T-50 available from Scale Aircraft Conversions, but it’s 1:48 and for this set’s price I could have bought three Intech F-16s…

 

But back to the conversion. This landing gear transplantation stunt sounds more complicated as it actually turned out to be. For the front wheel well I simply cut a long opening into the fuselage and added inside a styrene sheet as a well roof, attached under the cockpit floor.

For the main landing gear I just opened the flush covers on the T-50 fuselage, cut out the interior from the Intech F-16, tailored it a little and glued it into its new place.

 

This was made easy by the fact that the T-50 is a bit smaller than the F-16, so that the transplants are by tendency a little too large and offer enough “flesh” for adaptations. Once in place, the F-16 struts were mounted (also slightly tailored to fit well) and covers added. The front wheel cover was created with 0.5 mm styrene sheet, for the main covers I used the parts from the Intech F-16 kit because they were thinner than the leftover T-50 fuselage parts and feature some surface detail on the inside. They had to be adapted in size, though. But the operation worked like a charm, highly recommended!

 

Around the hull, some small details like missing air scoops, some pitots and antennae were added. In a bout of boredom (while waiting for ordered parts…) I also added static dischargers on the aerodynamic surfaces’ trailing edges – the kit comes with obvious attachment points, and they are a small detail that improves the modern look of the T-50 even more.

 

Since the Academy kit comes clean with only a ventral drop tank as ordnance, underwing pylons from a SEPECAT Jaguar (resin aftermarket parts from Pavla) and a pair of AGM-65 from the Italeri NATO Weapons set plus launch rails were added, plus a pair of Sidewinders (from a Hasegawa AAM set, painted as blue training rounds) on the wing tip launch rails.

Since the T-50 trainer comes unarmed, a gun nozzle had to be added – its position is very similar to the gun on board of the F-16, on the upper side of the port side LERX. Another addition are conformal chaff/flare dispensers at the fin’s base, adding some beef to the sleek aircraft.

  

Painting and markings:

I did not want a grey-in-grey livery, yet something “different” and rather typical or familiar for the British isles. My approach is actually a compromise, with classic RAF colors and design features inspired by camouflage experiments of the German Luftwaffe on F-4F Phantoms and Alpha Jets in the early Eighties.

 

For the upper sides I went for a classic British scheme, in Dark Green and Dark Sea Grey (Humbrol 163 and 164), colors I deem very appropriate for the Scottish landscape and for potential naval operations. These were combined with elements from late RAF interceptors: Barley Grey (Humbrol 167) for the flanks including the pylons, plus Light Aircraft Grey (Humbrol 166) for the undersides, with a relatively high waterline and a grey fin, so that a side or lower view would rather blend with the sky than the ground below.

 

Another creative field were the national markings: how could fictional Scottish roundels look like, and how to create them so that they are easy to make and replicate (for a full set for this kit, as well as for potential future builds…)? Designing and printing marking decals myself was an option, but I eventually settled for a composite solution which somewhat influenced the roundels’ design, too.

My Scottish roundel interpretationconsists of a blue disk with a white cross – it’s simple, different from any other contemporary national marking, esp. the UK roundel, and easy to create from single decal parts. In fact, the blue roundels were die-punched from blue decal sheet, and the cross consists of two thin white decal strips, cut into the correct length with the same stencil, using generic sheet material from TL Modellbau.

 

Another issue was the potential tactical code, and a small fleet only needs a simple system. Going back to a WWII system with letter codes for squadrons and individual aircraft was one option, but, IMHO, too complicated. I adopted the British single letter aircraft code, though, since this system is very traditional, but since the RoScAC would certainly not operate too many squadrons, I rather adapted a system similar to the Swedish or Spanish format with a single number representing the squadron. The result is a simple 2-digit code, and I adapted the German system of placing the tactical code on the fuselage, separated by the roundel. Keeping British traditions up I repeated the individual aircraft code letter on the fin, where a Scottish flag, a small, self-printed Fife coat-or-arms and a serial number were added, too.

 

The kit saw only light weathering and shading, and the kit was finally sealed with matt acrylic varnish (Italeri).

  

Creating this whif, based on an alternative historic timeline with a near future perspective, was fun – and it might spawn more models that circle around the story. A Scottish Sk 90 and a Gripen are certain options (and for both I have kits in the stash…), but there might also be an entry level trainer, some helicopters for the army and SAR duties, as well as a transport aircraft. The foundation has been laid out, now it’s time to fill Scotland’s history to come with detail and proof. ;-)

 

Besides, despite being a snap-fit kit, Academy’s T-50 is a nice basis, reminding me of some Hobby Boss kits but with less flaws (e .g. most of the interiors), except for the complete lack of a landing gear. But with the F-16 and Jaguar transplants the simple kit developed into something more convincing.

"Although I am quite capable of traversing the whole of time and space under my own resources."

 

"I'm not a genius, but you pick up things when you frequently find yourself in the 30th Century, in Kryptonian cities or wandering with the Gods of Apokolips and New Genesis."

 

"Why do you think I'm kidnapped by mad scientists and alien warlords so often?"

 

In the late 1950s, when she was living in a one-bedroom flat near Harrods, the Marchesa Luisa Casati believed she was capable of communicating by telepathy. She stopped writing cards and letters, and spent her days indulging in spiritualist sessions with her few remaining friends. Cecil Beaton came to visit one afternoon and took a few ill-conceived snaps, where she appears blurred and cowering with her arm over her face, horrified she might be captured in her jowly, lace-veiled dotage.

 

Not long afterwards she died of a stroke. When he heard, a friend with whom she had conducted a séance earlier that morning let himself back into her flat to fetch her taxidermied Pekinese and a fresh pair of her false eyelashes. She was buried with both, in Brompton Cemetery, five days later. It was a miserable occasion, on an unseasonably cool, unsettled June day, and only a handful of family and friends attended. One of them came all the way from Venice, where half a century earlier he had been her personal gondolier, ferrying her jewel-collared cheetahs, her blue-painted greyhounds and her own decadently costumed form across the murky shimmer of the city’s lagoon.

 

Back then, Luisa Casati – heiress, socialite, artists’ muse – was a beacon of the belle époque, a legion of poets, artists, sculptors, designers and occultists trailing in her wake. She stuffed her palazzo on the Grand Canal (today the site of the Guggenheim Museum) with gold-painted servants, mechanical birds in gilded cages, a boa-constrictor and a pride of white peacocks that she tied to the windows, in the shade of her cypress trees. She once plundered their feathers for a costume, accessorising its white plumage with a dash of fresh chicken blood. Lady Gaga’s meat dress would have seemed quite dowdy.

 

The tendrils of Casati’s signature and often nonsensical style reach confidently into the present day. Georgina Chapman named her fashion label Marchesa after the Italian heiress, and over the years both Alexander McQueen and Tom Ford have cited her as inspiration for their collections, the latter christening Casati “the first European dandy of the early 20th century”.

 

At six feet and cadaverously skinny, Casati was not considered a beauty, but she made herself unforgettable all the same. Her hair was cut and dyed a fiery red, her skin bleached white with powder. She kept her pupils dark with doses of belladonna, and rimmed their lids in thick black kohl, adding false eyelashes and strips of glued black velvet when the mood took her. It was not uncommon to see her prowling Venice with her cheetahs after dark, dressed in a cloak of silk velvet, mother-of-pearl heels and little else.

 

As a link between East and West and a symbol of shadowy, romantic beauty, Venice was a magnet for the era’s lost, often opium-soaked souls who flitted between its salons and balls, mixing with Europe’s élite.

 

It was here Casati began to realise her aim of becoming “a living work of art” and it so shaped her style that organisers have chosen to hold the exhibition at the former home and studio of the designer Mariano Fortuny. Casati was one of the first to wear the exquisitely pleated Delphos dress that made Fortuny’s name.

It was meant to be worn without underwear, which wasn’t too much of a problem for a woman who regularly appeared in public in see-through shifts and who once wore a dress covered in light bulbs with a generator attached.

 

Before all this, she was of course, a young girl, growing up between Monza and Lake Como, the daughter of rich parents who had made their fortune in cotton. Her father was ennobled in 1887, but eight years later he and his wife died within 12 months of each other, leaving 15-year-old Luisa and her sister Francesca sought-after heiresses.

 

Although Francesca was considered the better catch, Luisa made a suitably decorous débutante and in 1900, aged 19, she married Count Camillo Casati Stampa di Soncino, providing him with an heir, Cristina, a year later.

 

Neglected from a young age while her parents followed the hunting circuit from Rome to Paris and London, Cristina eloped with an English lord. Their daughter, Moorea, married the politician and royal hanger-on Woodrow Wyatt, and later Brinsley Black (their son is Octavius Black, founder of The Mind Gym).

 

Photographs of Casati taken not long after her marriage show a doe-eyed, typically Edwardian-looking girl. Everything changed when she met the poet Gabriele d’Annunzio at one of the hunts. The famously louche, debt-ridden lothario, who bedded most of Europe’s great beauties, made Casati his muse and lover. The two wrote cryptic notes to each other and christened themselves as Ariel and Core/Persephone.

 

The count ignored their affair, leaving Casati to transform herself from petulant, rule-abiding heiress into a devastating femme fatale – “To Core, destroyer of mediocrity” read one of d’Annunzio’s dedications. Supplicants at her Venice, Rome and later Paris courts included many of the avant-garde. Diaghilev, Picasso, Man Ray, Proust, Erté – all of them danced to her tune. She patronised the Futurists and the Ballets Russes and counted Kaiser Wilhelm II as one of her most dedicated admirers.

 

Brompton Cemetery, Fulham Road, London

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based historical facts. BEWARE!

 

Some background:

The Mikoyan-Gurevich MiG-19 (NATO reporting name: "Farmer") was a Soviet second-generation, single-seat, twin jet-engine fighter aircraft. It was the first Soviet production aircraft capable of supersonic speeds in level flight. A comparable U.S. "Century Series" fighter was the North American F-100 Super Sabre, although the MiG-19 would primarily oppose the more modern McDonnell Douglas F-4 Phantom II and Republic F-105 Thunderchief over North Vietnam. Furthermore, the North American YF-100 Super Sabre prototype appeared approximately one year after the MiG-19, making the MiG-19 the first operational supersonic jet in the world.

 

On 20 April 1951, OKB-155 was given the order to develop the MiG-17 into a new fighter called "I-340", also known as "SM-1". It was to be powered by two Mikulin AM-5 non-afterburning jet engines, a scaled-down version of the Mikulin AM-3, with 19.6 kN (4,410 lbf) of thrust. The I-340 was supposed to attain 1,160 km/h (725 mph, Mach 0.97) at 2,000 m (6,562 ft), 1,080 km/h (675 mph, Mach 1.0) at 10,000 m (32,808 ft), climb to 10,000 m (32,808 ft) in 2.9 minutes, and have a service ceiling of no less than 17,500 m (57,415 ft).

After several prototypes with many detail improvements, the ministers of the Soviet Union issued the order #286-133 to start serial production on February 17, 1954, at the factories in Gorkiy and Novosibirsk. Factory trials were completed on September 12 the same year, and government trials started on September 30.

 

Initial enthusiasm for the aircraft was dampened by several problems. The most alarming of these was the danger of a midair explosion due to overheating of the fuselage fuel tanks located between the engines. Deployment of airbrakes at high speeds caused a high-g pitch-up. Elevators lacked authority at supersonic speeds. The high landing speed of 230 km/h (145 mph), compared to 160 km/h (100 mph) for the MiG-15, combined with the lack of a two-seat trainer version, slowed pilot transition to the type. Handling problems were addressed with the second prototype, "SM-9/2", which added a third ventral airbrake and introduced all-moving tailplanes with a damper to prevent pilot-induced oscillations at subsonic speeds. It flew on 16 September 1954, and entered production as the MiG-19S.

 

Approximately 5,500 MiG-19's were produced, first in the USSR and in Czechoslovakia as the Avia S-105, but mainly in the People's Republic of China as the Shenyang J-6. The aircraft saw service with a number of other national air forces, including those of Cuba, North Vietnam, Egypt, Pakistan, and North Korea. The aircraft saw combat during the Vietnam War, the 1967 Six Day War, and the 1971 Bangladesh War.

 

However, jet fighter development made huge leaps in the 1960s, and OKB MiG was constantly trying to improve the MiG-19's performance, esp. against fast and high-flying enemies, primarily bombers but also spy planes like the U-2.

 

As the MiG-19S was brought into service with the Soviet air forces in mid-1956, the OKB MiG was continuing the refinement of the SM-1/I-340 fighter. One of these evolutionary paths was the SM-12 (literally, “SM-1, second generation”) family of prototypes, the ultimate extrapolation of the basic MiG-19 design, which eventually led to the MiG-19bis interceptor that filled the gap between the MiG-19S and the following, highly successful MiG-21.

 

The SM-12 first saw life as an exercise in drag reduction by means of new air intake configurations, since the MiG-19’s original intake with rounded lips became inefficient at supersonic speed (its Western rival, the North American F-100, featured a sharp-lipped nose air intake from the start). The first of three prototypes, the SM-12/1, was essentially a MiG-19S with an extended and straight-tapered nose with sharp-lipped orifice and a pointed, two-position shock cone on the intake splitter. The simple arrangement proved to be successful and was further refined.

 

The next evolutionary step, the SM-12/3, differed from its predecessors primarily in two new R3-26 turbojets developed from the earlier power plant by V. N. Sorokin. These each offered an afterburning thrust of 3,600kg, enabling the SM-12/3 to attain speeds ranging between 1,430km/h at sea level, or Mach=1.16, and 1,930km/h at 12,000m, or Mach=1.8, and an altitude of between 17,500 and 18,000m during its test program. This outstanding performance prompted further development with a view to production as a point defense interceptor.

 

Similarly powered by R3-26 engines, and embodying major nose redesign with a larger orifice permitting introduction of a substantial two-position conical centerbody for a TsD-30 radar, a further prototype was completed as the SM-12PM. Discarding the wing root NR-30 cannon of preceding prototypes, the SM-12PM was armed with only two K-5M (RS-2U) beam-riding missiles and entered flight test in 1957. This configuration would become the basis for the MiG-19bis interceptor that eventually was ordered into limited production (see below).

 

However, the SM-12 development line did not stop at this point. At the end of 1958, yet another prototype, the SM-12PMU, joined the experimental fighter family. This had R3M-26 turbojets uprated to 3.800kg with afterburning, but these were further augmented by a U-19D accelerator, which took the form of a permanent ventral pack containing an RU-013 rocket motor and its propellant tanks. Developed by D. D. Sevruk, the RU-013 delivered 3,000kg of additional thrust, and with the aid of this rocket motor, the SM-12PMU attained an altitude of 24,000m and a speed of Mach=1.69. But this effort was to no avail: the decision had been taken meanwhile to manufacture the Ye-7 in series as the MiG-21, and further development of the SM-12 series was therefore discontinued.

 

Nevertheless, since full operational status of the new MiG-21 was expected to remain pending for some time, production of a modified SM-12PM was ordered as a gap filler. Not only would this fighter bridge the performance gap to the Mach 2-capable MiG-21, it also had the benefit of being based on proven technologies and would not require a new basic pilot training.

 

The new aircraft received the official designation MiG-19bis. Compared with the SM-12PM prototype, the MiG-19bis differed in some details and improvements. The SM-12PM’s most significant shortfall was its short range – at full power, it had only a range of 750 km! This could be mended through an additional fuel tank in an enlarged dorsal fairing behind the cockpit. With this internal extra fuel, range could be extended by a further 200 - 250km range, but drop tanks had typically to be carried, too, in order to extend the fighter’ combat radius with two AAMs to 500 km. Specifically for the MiG-19bis, new, supersonic drop tanks (PTB-490) were designed, and these were later adapted for the MiG-21, too.

 

The air intake shock cone was re-contoured and the shifting mechanism improved: Instead of a simple, conical shape, the shock cone now had a more complex curvature with two steps and the intake orifice area was widened to allow a higher airflow rate. The air intake’s efficiency was further optimized through gradual positions of the shock cone.

As a positive side effect, the revised shock cone offered space for an enlarged radar dish, what improved detection range and resolution. The TsD-30 radar for the fighter’s missile-only armament was retained, even though the K-5’s effective range of only 2–6 km (1¼ – 3¾ mi) made it only suitable against slow and large targets like bombers. All guns were deleted in order to save weight or make room for the electronic equipment. The tail section was also changed because the R3M-26 engines and their afterburners were considerably longer than the MiG-19's original RM-5 engines. The exhausts now markedly protruded from the tail section, and the original, characteristic pen nib fairing between the two engines had been modified accordingly.

 

Production started in 1960, but only a total of roundabout 180 MiG-19bis, which received the NATO code "Farmer F", were built and the Soviet Union remained the only operator of the type. The first aircraft entered Soviet Anti-Air Defense in early 1961, and the machines were concentrated in PVO interceptor units around major sites like Moscow, Sewastopol at the Black Sea and Vladivostok in the Far East.

 

With the advent of the MiG-21, though, their career did not last long. Even though many machines were updated to carry the K-13 (the IR-guided AA-2 "Atoll") as well as the improved K-55 AAMs, with no change of the type’s designation, most MiG-19bis were already phased out towards the late 1960s and quickly replaced by 2nd generation MiG-21s as well as heavier and more capable Suchoj interceptors like the Su-9, -11 and -15. By 1972, all MiG-19bis had been retired.

  

General characteristics:

Crew: 1

Length: 13.54 m (44 ft 4 in), fuselage only with shock cone in forward position

15.48 m (50 8 ½ in) including pitot

Wingspan: 9 m (29 ft 6 in)

Height: 3.8885 m (12 ft 9 in)

Wing area: 25 m² (269 ft²)

Empty weight: 5,210 kg (11,475 lb)

Loaded weight: 7,890 kg (17,380 lb)

Max. takeoff weight: 9,050 kg (19,935 lb)

Fuel capacity: 2,450 l (556 imp gal; 647 US gal) internal;

plus 760 l (170 imp gal; 200 US gal) with 2 drop tanks

 

Powerplant:

2× Sorokin R3M-26 turbojets, rated at 37.2 kN (8,370 lbf) thrust each with afterburning

 

Performance:

Maximum speed: 1,380km/h at sea level (Mach=1.16)

1,850km/h at 12,000m (Mach=1.8)

Range: 1,250 km (775 mi; 750 nmi) at 14,000 m (45,000 ft) with 2 × 490 l drop tanks

Combat range: 500 km (312 mi; 270 nmi)

Ferry range: 2,000 km (1,242 mi; 690 nmi)

Service ceiling: 19,750 m (64,690 ft)

Rate of climb: 180 m/s (35,000 ft/min)

Wing loading: 353.3 kg/m² (72.4 lb/ft²)

Thrust/weight: 0.86

 

Armament:

No internal guns.

4× underwing pylons; typically, a pair of PTB-490 drop tanks were carried on the outer pylon pair,

plus a pair of air-to air missiles on the inner pair: initially two radar-guided Kaliningrad K-5M (RS-2US)

AAMs, later two radar-guided K-55 or IR-guided Vympel K-13 (AA-2 'Atoll') AAMs

  

The kit and its assembly:

Another submission for the 2018 Cold War Group Build at whatifmodelers.com, and again the opportunity to build a whiffy model from the project list. But it’s as fictional as one might think, since the SM-12 line of experimental “hybrid” fighters between the MiG-19 and the MiG-21 was real. But none of these aircraft ever made it into serial production, and in real life the MiG-21 showed so much potential that the attempts to improve the MiG-19 were stopped and no operational fighter entered production or service.

 

However, the SM-12, with its elongated nose and the central shock cone, makes a nice model subject, and I imagined what a service aircraft might have looked like? It would IMHO have been close, if not identical, to the SM-12PM, since this was the most refined pure jet fighter in the development family.

 

The basis for the build was a (dead cheap) Mastercraft MiG-19, which is a re-edition of the venerable Kovozávody Prostějov (KP) kit – as a tribute to modern tastes, it comes with (crudely) engraved panel, but it has a horrible fit all over. For instance, there was a 1mm gap between the fuselage and the right wing, the wing halves’ outlines did not match at all and it is questionable if the canopy actually belongs to the kit at all? PSR everywhere. I also had a Plastyk version of this kit on the table some time ago, but it was of a much better quality! O.K., the Mastercraft kit comes cheap, but it’s, to be honest, not a real bargain.

 

Even though the result would not be crisp I did some mods and changes. Internally, a cockpit tub was implanted (OOB there’s just a wacky seat hanging in mid air) plus some serious lead weight in the nose section for a proper stance.

On the outside, the new air intake is the most obvious change. I found a Su-17 intake (from a Mastercraft kit, too) and used a piece from a Matchbox B-17G’s dorsal turret to elongate the nose – it had an almost perfect diameter and a mildly conical shape. Some massive PSR work was necessary to blend the parts together, though.

The tail received new jet nozzles, scratched from steel needle protection covers, and the tail fairing was adjusted according to the real SM-12’s shape.

 

Ordnance was adapted, too: the drop tanks come from a Mastercraft MiG-21, and these supersonic PTB-490 tanks were indeed carried by the real SM-12 prototypes because the uprated engines were very thirsty and the original, teardrop-shaped MiG-19 tanks simply too draggy for the much faster SM-12. As a side note, the real SM-12’s short range was one of the serious factors that prevented the promising type’s production in real life. In order to overcome the poor range weakness I added an enlarged spine (half of a drop tank), inspired by the MiG-21 SMT, that would house an additional internal fuel tank.

 

The R2-SU/K-5 AAMs come from a vintage Mastercraft Soviet aircraft weapon set, which carries a pair of these 1st generation AAMs. While the molds seem to be a bit soft, the missiles look pretty convincing. Their pylons were taken from the kit (OOB they carry unguided AAM pods and are placed behind the main landing gear wells), just reversed and placed on the wings’ leading edges – similar to the real SM-12’s arrangement.

  

Painting and markings:

No surprises. In the Sixties, any PVO aircraft was left in bare metal, so there was hardly an alternative to a NMF finish.

 

Painting started with an all-over coat with acrylic Revell 99 (Aluminum), just the spine tank became light grey (Revell 371) for some contrast, and I painted some di-electric covers in a deep green (Revell 48).

The cockpit interior was painted with a bright mix of Revell 55 and some 48, while the landing gear wells and the back section of the cockpit were painted in a bluish grey (Revell 57).

The landing gear was painted in Steel (unpolished Modelmaster metallizer) and received classic, bright green wheel discs (Humbrol 2). As a small, unusual highlight the pitot boom under the chin received red and white stripes – seen on occasional MiG-19S fighters in Soviet service, and the anti-flutter booms on the stabilizers became bright red, too.

 

After the basic painting was done the kit received a black ink wash. Once this had dried and wiped off with a soft cotton cloth, post shading with various metallizer tones was added in order to liven up the uniform aircraft (including Humbrol’s matt and polished aluminum, and the exhaust section was treated with steel). Some panel lines were emphasized with a thin pencil.

 

Decals were puzzled together from various sources, a Guards badge and a few Russian stencils were added, too. Finally, the kit was sealed with a coat of sheen acrylic varnish (a 2:1 mix of Italeri matt and semi-gloss varnish).

 

The K-5 missiles, last but not least, were painted in aluminum, too, but their end caps (both front and tail section) became off-white.

  

The Mastercraft kit on which this conversion was based is crude, so I did not have high expectations concerning the outcome. But the new nose blends nicely into the MiG-19 fuselage, and the wide spine is a subtle detail that makes the aircraft look more “beefy” and less MiG-19-ish. The different drop tanks – even though they are authentic – visually add further speed. And despite many flaws, I am quite happy with the result of roundabout a week’s work.

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based on historical facts. BEWARE!

  

Some background:

The McDonnell Douglas (now Boeing) T-45 Goshawk was a highly modified version of the BAe Hawk land-based training jet aircraft. Manufactured by McDonnell Douglas (now Boeing) and British Aerospace (now BAe Systems), the T-45 was used by the United States Navy and the United States Marine Corps (USMC) as an aircraft carrier-capable trainer.

The Goshawk's origins began in the mid-1970s, when the US Navy began looking for a single aircraft replacement for both its T-2 and TA-4 jet trainers. The US Navy started the VTXTS advanced trainer program in 1978. Several companies made submissions, e. g. North American or Northrop/Vought. Due to the size of the potential contract, European companies made submissions, too, including a navalized Alpha Jet from Dassault/Dornier and a fully carrier-capable version of the BAe Hawk Mk.60, mutually proposed by British Aerospace (BAe) and McDonnell Douglas (MDC). The latter eventually won the competition and BAe and MDC were awarded the T-45 contract in 1981.

 

The Hawk had not been designed for carrier operations and numerous modifications were required to make it suitable for use on carriers. These included improvements to the low-speed handling characteristics and a reduction in the approach speed. It was found that the aircraft was apt to stall at the low approach speed required. Modifications were designed by BAe in England; most notably a simple slat system was devised, operated by an actuator and linkage mechanism to fit into the small space available. Strakes were also added on the fuselage to improve airflow. Other changes were a strengthened airframe, a more robust and wider landing gear with a two-wheel nose landing gear, a catapult tow bar attachment and an arresting hook. The modified aircraft was christened “Goshawk”, flew in 1988 for the first time and became operational in 1991.

 

Beyond being a naval trainer the T-45 was also adapted for first-line duty with strike capabilities, in the form of the OA-45 for the USMC. The role of this aircraft dated back to the Vietnam War when twenty-three A-4 two-seaters were converted into OA-4Ms for “FastFAC” (Fast Forward Air Controller) missions, in order to control interdiction sorties dedicated to shaping the battlefield for future operations. Basically, the OA-4M was a TA-4F equipped with A-4M electronics. The most visible and characteristic change was the fitting of the A-4M’s dorsal electronics hump, neatly faired into the rear of the two-seat canopy. The nose sensor group of the OA-4M was basically the same as that of the A-4M, but the Angle/Rate Bombing system was not installed as it would not be needed.

 

When the T-45 was introduced in the early Nineties, the USMCs OA-4Ms had reached the end of their service life and the USMC started looking for a replacement, wanting a comparable, light and fast fixed-wing aircraft. The USMC did not accept the LTV A-7 as an A-4 replacement (even though a two-seater version was available), because it was already dated, too, and not part of the USMC inventory. The USMC's A-4Ms were supposed to be replaced by the VTOL AV-8 by the mid-nineties, but the AV-8, even as a two-seater, was deemed unsuitable for FFAC duties. The new T-45 looked like a good and economical alternative with future potential, since the airframe was brand new and the type's infrastructure was fully established, so that a small number of specialized aircraft could easily be supported without much extra cost.

 

With fresh experience from the 1st Gulf War in 1990-91 the decision was made to buy 25 extra T-45A airframes and convert them to OA-45A standard. Most important change were modified wings, using structures and systems from the BAe Hawk 100 series. While the T-45 only had two underwing and a single ventral hardpoint, the OA-45A featured a total of seven: four underwing and one ventral hardpoints, plus wingtip stations for defensive air-to-air missiles. Upgraded avionics allowed the deployment of a wide range of external stores, including air-to-ground missiles and rocket launchers, a reconnaissance pod, retarded and free-fall bombs of up to 1,000 pounds (450 kg) caliber, runway cratering, anti-personnel and light armor bombs, cluster bombs, practice bombs as well as external fuel tanks and ECM pods. This was a vital asset, since Desert Storm had proved that FFAC aircraft had to have an offensive capability to handle targets of opportunity on their own, when no air assets to control were available. A total ordnance load of up to 6,800 lb (3,085 kg) was possible, even though the aircraft was not supposed to play an offensive role and rather act from a distance, relying on its small size and agility.

 

Communication modifications for the FastFAC role included a KY-28 secure voice system, an ARC-159 radio and an ARC-114 VHF radio. Similar to the Skyhawk, a hump behind the cockpit had to be added to make room for the additional electronic equipment and a heat exchanger. Other additions were a continuous-wave Doppler navigation radar under a shallow ventral radome underneath the cockpit, a ground control bombing system, an APN-194 altimeter, an ALR-45 radar warning suite, a retrofitted, fixed midair refueling probe and cockpit armor plating that included Kevlar linings on the floor and the lower side walls as well as externally mounted armor plates for the upper areas.

 

VMA-131 of Marine Aircraft Group 49 (the Diamondbacks) retired its last four OA-4Ms on 22 June 1994, and the new OA-45A arrived just in time to replace the venerable Skyhawk two-seaters in the FastFAC role. Trainer versions of the Skyhawk remained in Navy service, however, finding a new lease on life with the advent of "adversary training". OA-45A deliveries were finished in 1996 and the 25 aircraft were distributed among the newly established Marine Aviation Logistics Squadron (MALS, formerly Headquarters & Maintenance Squadron/H&MS) 12 & 13. The USMC crews soon nicknamed their new mounts "GosHog", to underlöine ist offensive capabilities and to set themselves apart from the USN's "tame" trainers. Even though thos name was never officially approved it caught on quickly.

 

After initial experience with the new aircraft and in the wake of technological advances, the USMC decided to upgrade the OA-45As in 2000 to improve its effectiveness and interaction capabilities with ground troops. This primarily resulted in the addition of a forward-looking infrared camera laser in the aircraft’s nose section, which enabled the aircraft to execute all-weather/night reconnaissance and to illuminate targets for laser-guided infantry shells or ordnance launched by the OA-45 itself or by other aircraft. Through this measure the OA-45 became capable of carrying and independently deploying light laser-guided smart weapons like the GBU-12 and -16 “Paveway II” glide bombs or the laser-guided AGM-65E “Maverick” variant. The update was gradually executed during regular overhauls in the course of 2001 and 2002 (no new airframes were built/converted), the modified machines received the new designation OA-45B.

 

After this update phase, the OA-45Bs were deployed in several global conflicts and saw frequent use in the following years. For instance, MALS 13 used its OA-45Bs operationally for the first time in October 2002 when the squadron was tasked with providing support to six AV-8B Harrier aircraft in combat operations in Afghanistan during Operation Enduring Freedom. This mission lasted until October 2003, four aircraft were allocated and one OA-45B was lost during a landing accident.

On 15 January 2003, MALS 13 embarked 205 Marines and equipment aboard the USS Bonhomme Richard in support of combat operations in Southwest Asia during Operation Southern Watch. Four OA-45Bs successfully supported these troops from land bases, marking targets and flying reconnaissance missions.

Furthermore, six MALS 13 OA-45Bs took actively part in Operation Iraqi Freedom from Al Jaber Air Base, Kuwait, and An Numiniyah Expeditionary Air Field, Iraq, where the aircraft worked closely together with the advancing ground troops of the USMC’s 15th Marine Expeditionary Unit. They successfully illuminated targets for US Navy fighter bombers, which were launched from USS Abraham Lincoln (CVN-72) in the Persian Gulf, and effectively guided these aircraft to their targets. Two OA-45Bs were lost during this conflict, one through enemy MANPADS, the other through friendly AA fire. In late May 2003 the surviving machines and their crews returned to MCAS Yuma.

 

On 16 March 2007, the 200th T-45 airframe was delivered to the US Navy. From this final batch, six airframes were set aside and modified into OA-45Bs in order to fill the losses over the past years.

Later T-45 production aircraft were built with enhanced avionics systems for a heads-up display (HUD) and glass cockpit standard, while all extant T-45A aircraft were eventually converted to a T-45C configuration under the T-45 Required Avionics Modernization Program (T-45 RAMP), bringing all aircraft to same HUD plus glass cockpit standard. These updates, esp. concerning the cockpit, were introduced to the OA-45Bs, too, and they were re-designated again, now becoming OA-45Cs, to reflect the commonality with the Navy’s Goshawk trainers. Again, these modifications were gradually introduced in the course of the OA-45s’ normal maintenance program.

 

In 2007, an engine update of the whole T-45 fleet, including the OA-45s, with the Adour F405-RR-402 was considered. This new engine was based on the British Adour Mk 951, designed for the latest versions of the BAe Hawk and powering the BAe Taranis and Dassault nEUROn UCAV technology demonstrators. The Adour Mk 951 offered 6,500 lbf (29 kN) thrust and up to twice the service life of the F405-RR-401. It featured an all-new fan and combustor, revised HP and LP turbines, and introduced Full Authority Digital Engine Control (FADEC). The Mk 951 was certified in 2005, the F405-RR-402 derived from it was certified in 2008, but it did not enter service due to funding issues, so that this upgrade was not carried out.

 

The final delivery of the 246th T-45 airframe took place in November 2009, and both T-45 and the OA-45 "GosHog" are supposed to remain in service until 2035.

  

General characteristics:

Crew: 2 (pilot, observer)

Length: 39 ft 4 in (11.99 m)

Wingspan: 30 ft 10 in (9.39 m)

Height: 13 ft 5 in (4.08 m)

Wing area: 190.1 ft² (17.7 m²)

Empty weight: 10,403 lb (4,460 kg)

Max. takeoff weight: 14,081 lb (6,387 kg)

 

Powerplant:

1× Rolls-Royce Turbomeca F405-RR-401 (Adour) non-afterburning turbofan with 5,527 lbf (26 kN)

 

Performance:

Maximum speed: Mach 2 (2,204 km/h (1,190 kn; 1,370 mph) at high altitude

Combat radius: 800 km (497 mi, 432 nmi)

Ferry range: 3,200 km (1,983 mi) with drop tanks

Service ceiling: 15,240 m (50,000 ft)

Wing loading: 283 kg/m² (58 lb/ft²)

Thrust/weight: 0.97

Maximum g-load: +9 g

 

Armament:

No internal gun; seven external hardpoints (three on each wing and one under fuselage)

for a wide range of ordnance of up to 6,800 lb (3,085 kg), including up to six AIM-9 Sidewinder for

self-defense, pods with unguided rockets for target marking or ECM pods, but also offensive weapons

of up to 1.000 lb (454 kg) weight, including iron/cluster bombs and guided AGM-65, GBU-12 and -16.

  

The kit and its assembly:

This fictional T-45 variant is actually the result of a long idea evolution, and simply rooted in the idea of a dedicated OA-4M replacement for the USMC; in real life, the FFAC role has been transferred to F-18 two-seaters, though, but the T-45 appeared like a sound alternative to me.

 

There's only one T-45 kit available, a dubious T-45A from Italeri with poor wings and stabilizers. Wolfpack also offers a T-45, but it’s just a re-boxing of the Italeri kit with some PE parts and a price tag twice as big – but it does not mend the original kit’s issues… After reading the A-4 Skyhawk book from the French "Planes & Pilots" series, I was reminded of the USMC's special OA-4M FAC two-seaters (and the fact that it is available in kit form from Italeri and Hasegawa), and, cross-checking the real-world timeline of the T-45, I found that it could have been a suitable successor. The ide of the USMC’s OA-45 was born! :D

 

Building-wise the Italeri T-45 remained close to OOB, even though I transplanted several parts from an Italeri BAe Hawk Mk. 100 to create a different look. I modified the nose with the Mk. 100’s laser fairing and added some radar warning sensor bumps. This transplantation was not as easy as it might seem because the T-45’s nose is, due to the different and more massive front landing gear quite different from the Hawk’s. Took some major PSR to integrate the laser nose.

An ALR-45 “hot dog” fairing from a late A-4M (Italeri kit) was added to the fin, together with a small styrene wedge extending the fin’s leading edge. This small detail markedly changes the aircraft’s look. I furthermore added a refueling probe, scratched from coated wire and some white glue, as well as a low “camel back” fairing behind the cockpit, created from a streamlined bomb half with air outlets for an integrated heat exchanger. Blade antennae were relocated and added. A shallow bump for the Doppler radar was added under the fuselage behind the landing gear well – left over from an Airfix A-4B (from an Argentinian A-4P, to be correct, actually a dorsal fairing).

 

On the wings, a tailored pair of pylons and wing tip launch rails from the Italeri BAe Hawk Mk. 100 kit were added, too, as well as the donor kit’s pair of Sidewinders. The rest of the ordnance consists of drop tanks and LAU-19 pods for target marking missiles. The tanks were taken from the Hawk Mk. 100 kit, too, the rocket launchers came from an Italeri NATO aircraft weapons set. The centerline position carries an ALQ-131 ECM pod from a Hasegawa US aircraft weapons set on a pylon from the scrap box.

  

Painting and markings:

The low-viz idea prevailed, since I had some leftover OA-4M decals from Italeri kits in store, as well as some other suitable low-viz decals from a Revell A-4F kit. However, an all-grey livery was IMHO not enough, and when I came across a picture of a USN low-viz A-7E with an improvised desert camouflage in sand and reddish brown applied over the grey (even partly extending over its markings) from Operation Iraqi Freedom, I had that extra twist that would set the OA-45 apart. MALS-13 was chosen as operator because I had matching codes, and, as another benefit, the unit had actually been deployed overseas during the 2003 Iraq War, so that the whif’’s time frame was easily settled, adding to its credibility.

 

The livery was built up just like on the real aircraft: on top of a basic scheme in FS 36320 and 36375 (Humbrol 128 and 127) with a slightly darker anti-glare panel in front of the cockpit (FS 35237, I used Revell 57 as a slightly paler alternative) I applied the low-viz marking decals, which were protected with a coat of acrylic varnish. Next, additional desert camouflage was added with dry-brushed sand and millitary brown (supposedly FS 33711 and 30400 in real life, I used, after consulting pictures of aircraft from both Gulf Wars, Humbrol 103 (Cream) and 234 (Dark Flesh). They were applied with a kind of a dry-brushing technique, for a streaky and worn look, leaving out the codes and other markings. The pattern itself was inspired by an USMC OV-10 Bronco in desert camouflage from the 1st Gulf War.

On top of that a black ink washing was applied. Once things had thoroughly dried over night, I wet-sanded the additional desert camouflage away, carefully from front to back, so that the edges became blurred and the underlying grey became visible again.

 

The cockpit interior was painted in standard Dark Gull Grey (Humbrol 140), while the air intakes and the landing gear became white, the latter with red trim on the covers’ edges – just standard. Finally, the model was sealed with a coat of matt acrylic varnish (Italeri).

  

The upgraded T-45 is an interesting result. The add-ons suit the aircraft, which already looks sturdier than its land-based ancestor, well. The improvised desert paint scheme with the additional two-tone camouflage over the pale grey base really makes the aircraft an unusual sight, adding to its credibility.

Hardware-wise I am really happy how the added dorsal hump blends into the overall lines – in a profile view it extends the canopy’s curve and blends into the fin, much like the A-4F/M’s arrangement. And the modified fin yields a very different look, even though not much was changed. The T-45 looks much beefier now, and from certain angles really reminds of the OA-4M and sometimes even of a diminutive Su-25?

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based historical facts. BEWARE!

  

The KAI T-50 Golden Eagle (골든이글) is a family of South Korean supersonic advanced trainers and light combat aircraft, developed by Korea Aerospace Industries (KAI) with Lockheed Martin. The T-50 is South Korea's first indigenous supersonic aircraft and one of the world's few supersonic trainers.

 

The T-50 program started in the late Nineties and was originally intended to develop an indigenous trainer aircraft capable of supersonic flight, to train and prepare pilots for the KF-16 and F-15K, replacing trainers such as T-38 and A-37 that were then in service with the ROKAF. Prior South Korean aircraft programs include the turboprop KT-1 basic trainer produced by Daewoo Aerospace (now part of KAI), and license-manufactured KF-16.

 

The mother program, code-named KTX-2, began in 1992, but the Ministry of Finance and Economy suspended the original project in 1995 due to financial constraints. The basic design of the aircraft was set by 1999, and eventually the development of the aircraft was funded 70% by the South Korean government, 17% by KAI, and 13% by Lockheed Martin.

 

In general, the T-50 series of aircraft closely resembles the KF-16 in configuration, but it actually is a completely new design: the T-50 is 11% smaller and 23% lighter than an F-16, and in order to create enough space for the two-seat cockpit, the air intake was bifurcated and placed under the wing gloves, resembling the F/A-18's layout.

 

The aircraft was formally designated as the T-50 'Golden Eagle' in February 2000, the T-50A designation had been reserved by the U.S. military to prevent it from being inadvertently assigned to another aircraft model. Final assembly of the first T-50 took place between 15 January and 14 September 2001. The first flight of the T-50 took place in August 2002, and initial operational assessment from 28 July to 14 August 2003.

 

The trainer has a cockpit for two pilots in a tandem arrangement, both crew members sitting in "normal" election seats, not in the F-16's reclined position. The high-mounted canopy is applied with stretched acrylic, providing the pilots with good visibility, and has been tested to offer the canopy with ballistic protection against 4-lb objects impacting at 400 knots.

 

The ROKAF, as original development driver, placed an initial production contract for 25 T-50s in December 2003, with aircraft scheduled to be delivered between 2005 and 2009. Original T-50 aircraft were equipped with the AN/APG-67(v)4 radar from Lockheed Martin. The T-50 trainer is powered by a GE F404 engine built under license by Samsung Techwin. Under the terms of the T-50/F404-102 co-production agreement, GE provides engine kits directly to Samsung Techwin who produces designated parts as well as performing final engine assembly and testing.

 

The T-50 program quickly expanded beyond a pure trainer concept to include the TA-50 armed trainer aircraft, as well as the FA-50 light attack aircraft, which has already similar capabilities as the multirole KF-16. Reconnaissance and electronic warfare variants were also being developed, designated as RA-50 and EA-50.

 

The TA-50 variant is a more heavily armed version of the T-50 trainer, intended for lead-in fighter training and light attack roles. It is equipped with an Elta EL/M-2032 fire control radar and designed to operate as a full-fledged combat platform. This variant mounts a lightweight three-barrel cannon version of the M61 Vulcan internally behind the cockpit, which fires linkless 20 mm ammunition. Wingtip rails can accommodate the AIM-9 Sidewinder missile, a variety of additional weapons can be mounted to underwing hardpoints, including precision-guided weapons, air-to-air missiles, and air-to-ground missiles. The TA-50 can also mount additional utility pods for reconnaissance, targeting assistance, and electronic warfare. Compatible air-to-surface weapons include the AGM-65 Maverick missile, Hydra 70 and LOGIR rocket launchers, CBU-58 and Mk-20 cluster bombs, and Mk-82, -83, and -84 general purpose bombs.

 

Among the operators of the TA-50 are the Philippines, Thailand and the ROKAF, and the type has attracted a global interest, also in Europe. The young Republic of Scotland Air Corps (locally known as Poblachd na h-Alba Adhair an Airm) chose, soon after the country's independence from the United Kingdom, after its departure from the European Union in 2017, the TA-50 as a complement to its initial procurements and add more flexibility to its small and young air arm.

 

According to a White Paper published by the Scottish National Party (SNP) in 2013, an independent Scotland would have an air force equipped with up to 16 air defense aircraft, six tactical transports, utility rotorcraft and maritime patrol aircraft, and be capable of “contributing excellent conventional capabilities” to NATO. Outlining its ambition to establish an air force with an eventual 2,000 uniformed personnel and 300 reservists, the SNP stated the organization would initially be equipped with “a minimum of 12 interceptors in the Eurofighter/Typhoon class, based at Lossiemouth, a tactical air transport squadron, including around six [Lockheed Martin] C-130J Hercules, and a helicopter squadron”.

 

According to the document, “Key elements of air forces in place at independence, equipped initially from a negotiated share of current UK assets, will secure core tasks, principally the ability to police Scotland’s airspace, within NATO.” An in-country air command and control capability would be established within five years of a decision in favor of independence, it continues, with staff also to be “embedded within NATO structures”.

This plan was immediately set into action after the country's independence in late 2017 with the purchase of twelve refurbished Saab JAS 39A Gripen interceptors for Quick Reaction Alert duties and upgraded, former Swedish Air Force Sk 90 trainers for the RoScAC. But these second hand machines were just the initial step in the mid-term procurement plan.

 

The twelve KAI TA-50 aircraft procured as a second step were to fulfill the complex requirement for a light and cost-effective multi-purpose aircraft that could be used in a wide variety of tasks: primarily as an advanced trainer for supersonic flight and as a trainer for the fighter role (since all Scottish Gripens were single seaters and dedicated to the interceptor/air defense role), but also as a light attack and point defense aircraft.

 

Scotland was offered refurbished F-16C and Ds, but this was declined as the type was deemed to be too costly and complex. Beyond the KAI T-50, the Alenia Aermacchi M-346 Master and the BAe Hawk were considered, too, but, eventually, a modified TA-50 that was tailored to the RoScAC’s procurement plans was chosen by the Scottish government.

 

In order to fulfill the complex duty profile, the Scottish TA-50s were upgraded with elements from the FA-50 attack aircraft. They possess more internal fuel capacity, enhanced avionics, a longer radome and a tactical datalink. Its EL/M-2032 pulse-Doppler radar has been modified so that it offers now a range two-thirds greater than the TA-50's standard radar. It enables the aircraft to operate in any weather, detect surface targets and deploy AIM-120 AAMs for BVR interceptions. The machines can also be externally fitted with Rafael's Sky Shield or LIG Nex1's ALQ-200K ECM pods, Sniper or LITENING targeting pods, and Condor 2 reconnaissance pods to further improve the machine’s electronic warfare, reconnaissance, and targeting capabilities.

 

Another unique feature of the Scottish Golden Eagle is its powerplant: even though the machines are originally powered by a single General Electric F404 afterburning turbofan and designed around this engine, the RoScAC TF-50s are powered by a Volvo RM12 low-bypass afterburning turbofan. These are procured and serviced through Saab in Sweden, as a part of the long-term collaboration contract for the RoScAC’s Saab Gripen fleet. This decision was taken in order to decrease overall fleet costs through a unified engine.

 

The RM12 is a derivative of the General Electric F404-400. Changes from the standard F404 includes greater reliability for single-engine operations (including more stringent birdstrike protection) and slightly increased thrust. Several subsystems and components were also re-designed to reduce maintenance demands, and the F404's analogue Engine Control Unit was replaced with the Digital Engine Control – jointly developed by Volvo and GE – which communicates with the cockpit through the digital data buses and, as redundancy, mechanical calculators controlled by a single wire will regulate the fuel-flow into the engine.

 

Another modification of the RoScAC’s TA-50 is the exchange of the original General Dynamics A-50 3-barrel rotary cannon for a single barrel Mauser BK-27 27mm revolver cannon. Being slightly heavier and having a lower cadence, the BK-27 featured a much higher kinetic energy, accuracy and range. Furthermore, the BK-27 is the standard weapon of the other, Sweden-built aircraft in RoScAC service, so that further synergies and cost reductions were expected.

 

The Scottish Department of National Defense announced the selection of the TA-50 in August 2018, after having procured refurbished Saab Sk 90 and JAS 39 Gripen from Sweden as initial outfit of the country's small air arm with No. 1 Squadron based at Lossiemouth AB.

 

Funding for the twelve aircraft was approved by Congress on September 2018 and worth € 420 mio., making the Golden Eagle the young country’s first brand new military aircraft. Deliveries of the Golden Hawk TF.1, how the type was officially designated in Scottish service, began in November 2019, lasting until December 2020.

The first four Scottish Golden Hawk TF.1 aircraft were allocated to the newly established RoScAC No. 2 Squadron, based at Leuchars, where the RoScAC took control from the British Army. The latter had just taken over the former air base from the RAF in 2015, losing its “RAF air base” status and was consequentially re-designated “Leuchars Station”, primarily catering to the Royal Scots Dragoon Guards who have, in the meantime, become part of Scotland’s Army Corps. The brand new machines were publically displayed on the shared army and air corps facility in the RoScAC’s new paint scheme on 1st of December 2019 for the first time, and immediately took up service.

 

General characteristics:

Crew: 2

Length: 13.14 m (43.1 ft)

Wingspan (with wingtip missiles): 9.45 m (31 ft)

Height: 4.94 m (16.2 ft)

Wing area: 23.69 m² (255 ft²)

Empty weight: 6,470 kg (14,285 lb)

Max. takeoff weight: 12,300 kg (27,300 lb)

 

Powerplant:

1× Volvo RM12 afterburning turbofan, rated at 54 kN (12,100 lbf) dry thrust

and 80.5 kN (18,100 lbf) with afterburner

 

Performance:

Maximum speed: Mach 1.5 (1,640 km/h, 1,020 mph at 9,144 m or 30,000 ft)

Range: 1,851 km (1,150 mi)

Service ceiling: 14,630 m (48,000 ft)

Rate of climb: 198 m/s (39,000 ft/min)

Thrust/weight: 0.96

Max g limit: -3 g / +8 g

 

Armament:

1× 27mm Mauser BK-27 revolver cannon with 120 rounds

A total of 7 hardpoints (4 underwing, 2 wingtip and one under fuselage)

for up to 3,740 kg (8,250 lb) of payload

  

The kit and its assembly:

A rare thing concerning my builds: an alternative reality whif. A fictional air force of an independent Scotland crept into my mind after the hysterical “Brexit” events in 2016 and the former (failed) public vote concerning the independence of Scotland from the UK. What would happen to the military, if the independence would take place, nevertheless, and British forces left the country?

 

The aforementioned Scottish National Party (SNP) paper from 2013 is real, and I took it as a benchmark. Primary focus would certainly be set on air space defense, and the Gripen appears as a good and not too expensive choice. The Sk 90 is a personal invention, but would fulfill a good complementary role.

Nevertheless, another multi-role aircraft would make sense as an addition, and both M-346 and T-50 caught my eye (Russian options were ruled out due to the tense political relations), and I gave the TA-50 the “Go” because of its engine and its proximity to the Gripen.

 

The T-50 really looks like the juvenile offspring from a date between an F-16 and an F-18. There’s even a kit available, from Academy – but it’s a Snap-Fit offering without a landing gear but, as an alternative, a clear display that can be attached to the engine nozzle. It also comes with stickers instead of waterslide decals. This sounds crappy and toy-like, but, after taking a close look at kit reviews, I gave it a try.

 

And I am positively surprised. While the kit consists of only few parts, moulded in the colors of a ROCAF trainer as expected, the surfaces have minute, engraved detail. Fit is very good, too, and there’s even a decent cockpit that’s actually better than the offering of some “normal” model kits. The interior comes with multi-part seats, side consoles and dashboards that feature correctly shaped instrument details (no decals). The air intakes are great, too: seamless, with relatively thin walls, nice!

 

So far, so good. But not enough. I could have built the kit OOB with the landing gear tucked up, but I went for the more complicated route and trans-/implanted the complete landing gear from an Intech F-16, which is available for less than EUR 5,- (and not much worth, to be honest). AFAIK, there’s white metal landing gear for the T-50 available from Scale Aircraft Conversions, but it’s 1:48 and for this set’s price I could have bought three Intech F-16s…

 

But back to the conversion. This landing gear transplantation stunt sounds more complicated as it actually turned out to be. For the front wheel well I simply cut a long opening into the fuselage and added inside a styrene sheet as a well roof, attached under the cockpit floor.

For the main landing gear I just opened the flush covers on the T-50 fuselage, cut out the interior from the Intech F-16, tailored it a little and glued it into its new place.

 

This was made easy by the fact that the T-50 is a bit smaller than the F-16, so that the transplants are by tendency a little too large and offer enough “flesh” for adaptations. Once in place, the F-16 struts were mounted (also slightly tailored to fit well) and covers added. The front wheel cover was created with 0.5 mm styrene sheet, for the main covers I used the parts from the Intech F-16 kit because they were thinner than the leftover T-50 fuselage parts and feature some surface detail on the inside. They had to be adapted in size, though. But the operation worked like a charm, highly recommended!

 

Around the hull, some small details like missing air scoops, some pitots and antennae were added. In a bout of boredom (while waiting for ordered parts…) I also added static dischargers on the aerodynamic surfaces’ trailing edges – the kit comes with obvious attachment points, and they are a small detail that improves the modern look of the T-50 even more.

 

Since the Academy kit comes clean with only a ventral drop tank as ordnance, underwing pylons from a SEPECAT Jaguar (resin aftermarket parts from Pavla) and a pair of AGM-65 from the Italeri NATO Weapons set plus launch rails were added, plus a pair of Sidewinders (from a Hasegawa AAM set, painted as blue training rounds) on the wing tip launch rails.

Since the T-50 trainer comes unarmed, a gun nozzle had to be added – its position is very similar to the gun on board of the F-16, on the upper side of the port side LERX. Another addition are conformal chaff/flare dispensers at the fin’s base, adding some beef to the sleek aircraft.

  

Painting and markings:

I did not want a grey-in-grey livery, yet something “different” and rather typical or familiar for the British isles. My approach is actually a compromise, with classic RAF colors and design features inspired by camouflage experiments of the German Luftwaffe on F-4F Phantoms and Alpha Jets in the early Eighties.

 

For the upper sides I went for a classic British scheme, in Dark Green and Dark Sea Grey (Humbrol 163 and 164), colors I deem very appropriate for the Scottish landscape and for potential naval operations. These were combined with elements from late RAF interceptors: Barley Grey (Humbrol 167) for the flanks including the pylons, plus Light Aircraft Grey (Humbrol 166) for the undersides, with a relatively high waterline and a grey fin, so that a side or lower view would rather blend with the sky than the ground below.

 

Another creative field were the national markings: how could fictional Scottish roundels look like, and how to create them so that they are easy to make and replicate (for a full set for this kit, as well as for potential future builds…)? Designing and printing marking decals myself was an option, but I eventually settled for a composite solution which somewhat influenced the roundels’ design, too.

My Scottish roundel interpretationconsists of a blue disk with a white cross – it’s simple, different from any other contemporary national marking, esp. the UK roundel, and easy to create from single decal parts. In fact, the blue roundels were die-punched from blue decal sheet, and the cross consists of two thin white decal strips, cut into the correct length with the same stencil, using generic sheet material from TL Modellbau.

 

Another issue was the potential tactical code, and a small fleet only needs a simple system. Going back to a WWII system with letter codes for squadrons and individual aircraft was one option, but, IMHO, too complicated. I adopted the British single letter aircraft code, though, since this system is very traditional, but since the RoScAC would certainly not operate too many squadrons, I rather adapted a system similar to the Swedish or Spanish format with a single number representing the squadron. The result is a simple 2-digit code, and I adapted the German system of placing the tactical code on the fuselage, separated by the roundel. Keeping British traditions up I repeated the individual aircraft code letter on the fin, where a Scottish flag, a small, self-printed Fife coat-or-arms and a serial number were added, too.

 

The kit saw only light weathering and shading, and the kit was finally sealed with matt acrylic varnish (Italeri).

  

Creating this whif, based on an alternative historic timeline with a near future perspective, was fun – and it might spawn more models that circle around the story. A Scottish Sk 90 and a Gripen are certain options (and for both I have kits in the stash…), but there might also be an entry level trainer, some helicopters for the army and SAR duties, as well as a transport aircraft. The foundation has been laid out, now it’s time to fill Scotland’s history to come with detail and proof. ;-)

 

Besides, despite being a snap-fit kit, Academy’s T-50 is a nice basis, reminding me of some Hobby Boss kits but with less flaws (e .g. most of the interiors), except for the complete lack of a landing gear. But with the F-16 and Jaguar transplants the simple kit developed into something more convincing.

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based on historical facts. BEWARE!

  

Some background:

The Grumman Mohawk began as a joint Army-Marine program through the then-Navy Bureau of Aeronautics (BuAer), for an observation/attack plane that would outperform the light and vulnerable Cessna L-19 Bird Dog. In June 1956, the Army issued Type Specification TS145, which called for the development and procurement of a two-seat, twin turboprop aircraft designed to operate from small, unimproved fields under all weather conditions. It would be faster, with greater firepower, and heavier armor than the Bird Dog, which had proved very vulnerable during the Korean War.

 

The Mohawk's mission would include observation, artillery spotting, air control, emergency resupply, naval target spotting, liaison, and radiological monitoring. The Navy specified that the aircraft had to be capable of operating from small "jeep" escort class carriers (CVEs). The DoD selected Grumman Aircraft Corporation's G-134 design as the winner of the competition in 1957. Marine requirements contributed an unusual feature to the design: since the Marines were authorized to operate fixed-wing aircraft in the close air support (CAS) role, the mockup featured underwing pylons for rockets, bombs, and other stores, and this caused a lot of discord. The Air Force did not like the armament capability of the Mohawk and tried to get it removed. On the other side, the Marines did not want the sophisticated sensors the Army wanted, so when their Navy sponsors opted to buy a fleet oil tanker, they eventually dropped from the program altogether. The Army continued with armed Mohawks (and the resulting competence controversy with the Air Force) and also developed cargo pods that could be dropped from underwing hard points to resupply troops in emergencies.

 

In mid-1961, the first Mohawks to serve with U.S. forces overseas were delivered to the 7th Army at Sandhofen Airfield near Mannheim, Germany. Before its formal acceptance, the camera-carrying AO-1AF was flown on a tour of 29 European airfields to display it to the U.S. Army field commanders and potential European customers. In addition to their Vietnam and European service, SLAR-equipped Mohawks began operational missions in 1963 patrolling the Korean Demilitarized Zone.

 

Germany and France showed early interest in the Mohawk, and two OV-1s were field-tested by both nations over the course of several months. No direct orders resulted, though, but the German Bundesheer (Army) was impressed by the type’s performance and its capability as an observation and reconnaissance platform. Grumman even signed a license production agreement with the French manufacturer Breguet Aviation in exchange for American rights to the Atlantic maritime patrol aircraft, but no production orders followed.

 

This could have been the end of the OV-1 in Europe, but in 1977 the German government, primarily the interior ministry and its intelligence agency, the Bundesnachrichtendienst (BND), showed interest in a light and agile SIGINT/ELINT platform that could fly surveillance missions along the inner-German border to the GDR and also to Czechoslovakia. Beyond visual reconnaissance with cameras and IR sensors, the aircraft was to be specifically able to identify and locate secret radio stations that were frequently operated by Eastern Block agents (esp. by the GDR) all across Western Germany, but primarily close to the inner-German border due to the clandestine stations’ low power. The Bundeswehr already operated a small ELINT/ECM fleet, consisting of converted HFB 320 ‘Hansa’ business jets, but these were not suited for stealthy and inconspicuous low flight level missions that were envisioned, and they also lacked the ability to fly slowly enough to locate potential “radio nests”.

 

The pan and the objective were clear, but the ELINT project caused a long and severe political debate concerning the operator of such an aerial platform. Initially, the Bundesheer, who had already tested the OV-1, claimed responsibility, but the interior ministry in the form of the German customs department as well as the German police’s Federal Border Guard, the Bundesgrenzschutz and the Luftwaffe (the proper operator for fixed-wing aircraft within the German armed forces), wrestled for this competence. Internally, the debate and the project ran under the handle “Schimmelreiter” (literally “The Rider on the White Horse”), after a northern German legendary figure, which eventually became the ELINT system’s semi-official name after it had been revealed to the public. After much tossing, in 1979 the decision was made to procure five refurbished U.S. Army OV-1As, tailored to the German needs and – after long internal debates – operate them by the Luftwaffe.

 

The former American aircraft were hybrids: they still had the OV-1A’s original short wings, but already the OV-1D’s stronger engines and its internal pallet system for interchangeable electronics. The machines received the designation OV-1G (for Germany) and were delivered in early 1980 via ship without any sensors or cameras. These were of Western German origin, developed and fitted locally, tailored to the special border surveillance needs.

 

The installation and testing of the “Schimmelreiter” ELINT suite lasted until 1982. It was based on a Raytheon TI Systems emitter locator system, but it was locally adapted by AEG-Telefunken to the airframe and the Bundeswehr’s special tasks and needs. The system’s hardware was stowed in the fuselage, its sensor arrays were mounted into a pair of underwing nacelles, which occupied the OV-1’s standard hardpoints, allowing a full 360° coverage. In order to cool the electronics suite and regulate the climate in the internal equipment bays, the OV-1G received a powerful heat exchanger, mounted under a wedge-shaped fairing on the spine in front of the tail – the most obvious difference of this type from its American brethren. The exact specifications of the “Schimmelreiter” ELINT suite remained classified, but special emphasis was placed upon COMINT (Communications Intelligence), a sub-category of signals intelligence that engages in dealing with messages or voice information derived from the interception of foreign communications. Even though the “Schimmelreiter” suite was the OV-1Gs’ primary reconnaissance tool, the whole system could be quickly de-installed for other sensor packs and reconnaissance tasks (even though this never happened), or augmented by single modules, what made upgrades and mission specialization easy. Beyond the ELINT suite, the OV-1G could be outfitted with cameras and other sensors on exchangeable pallets in the fuselage, too. This typically included a panoramic camera in a wedge-shaped ventral fairing, which would visually document the emitter sensors’ recordings.

 

A special feature of the German OV-1s was the integration of a brand new, NATO-compatible “Link-16” data link system via a MIDS-LVT (Multifunctional Information Distribution System). Even though this later became a standard for military systems, the OV-1G broke the ground for this innovative technology. The MIDS was an advanced command, control, communications, computing and intelligence (C4I) system incorporating high-capacity, jam-resistant, digital communication links for exchange of near real-time tactical information, including both data and voice, among air, ground, and sea elements. Outwardly, the MIDS was only recognizable through a shallow antenna blister behind the cockpit.

 

Even though the OV-1Gs initially retained their former American uniform olive drab livery upon delivery and outfitting in German service, they soon received a new wraparound camouflage for their dedicated low-level role in green and black (Luftwaffe Norm 83 standard), which was better suited for the European theatre of operations. In Luftwaffe service, the OV-1Gs received the tactical codes 18+01-05 and the small fleet was allocated to the Aufklärungsgeschwader (AG) 51 “Immelmann”, where the machines formed, beyond two squadrons with RF-4E Phantom IIs, an independent 3rd squadron. This small unit was from the start based as a detachment at Lechfeld, located in Bavaria/Southern Germany, instead of AG 51’s home airbase Bremgarten in South-Western Germany, because Lechfeld was closer to the type’s typical theatre of operations along Western Germany’s Eastern borders. Another factor in favor of this different airbase was the fact that Lechfeld was, beyond Tornado IDS fighter bombers, also the home of the Luftwaffe’s seven HFB 320M ECM aircraft, operated by the JaBoG32’s 3rd squadron, so that the local maintenance crews were familiar with complex electronics and aircraft systems, and the base’s security level was appropriate, too.

 

With the end of the Cold War in 1990, the OV-1Gs role and field of operation gradually shifted further eastwards. With the inner-German Iron Curtain gone, the machines were now frequently operated along the Polish and Czech Republic border, as well as in international airspace over the Baltic Sea, monitoring the radar activities along the coastlines and esp. the activities of Russian Navy ships that operated from Kaliningrad and Saint Petersburg. For these missions, the machines were frequently deployed to the “new” air bases Laage and Holzdorf in Eastern Germany.

 

In American service, the OV-1s were retired from Europe in 1992 and from operational U.S. Army service in 1996. In Germany, the OV-1 was kept in service for a considerably longer time – with little problems, since the OV-1 airframes had relatively few flying hours on their clocks. The Luftwaffe’s service level for the aircraft was high and spare parts remained easy to obtain from the USA, and there were still OV-1 parts in USAF storage in Western German bases.

 

The German HFB 320M fleet was retired between 1993 and 1994 and, in part, replaced by the Tornado ECR. At the same time AG 51 was dissolved and the OV-1Gs were nominally re-allocated to JaboG 32/3. With this unit the OV-1Gs remained operational until 2010, undergoing constant updates and equipment changes. For instance, the machines received in 1995 a powerful FLIR sensor in a small turret in the aircraft’s nose, which improved the aircraft’s all-weather reconnaissance capabilities and was intended to spot hidden radio posts even under all-weather/night conditions, once their signal was recognized and located. The aircrafts’ radio emitter locator system was updated several times, too, and, as a passive defensive measure against heat-guided air-to-air missiles/MANPADS, an IR jammer was added, extending the fuselage beyond the tail. These machines received the suffix “Phase II”, even though all five aircraft were updated the same way.

Reports that the OV-1Gs were furthermore retrofitted with the avionics to mount and launch AIM-9 Sidewinder AAMs under the wing tips for self-defense remained unconfirmed, even more so because no aircraft was ever seen carrying arms – neither the AIM-9 nor anything else. Plans to make the OV-1Gs capable of carrying the Luftwaffe’s AGM-65 Maverick never went beyond the drawing board, either. However, BOZ chaff/flare dispenser pods and Cerberus ECM pods were occasionally seen on the ventral pylons from 1998 onwards.

 

No OV-1G was lost during the type’s career in Luftwaffe service, and after the end of the airframes’ service life, all five German OV-1Gs were scrapped in 2011. There was, due to worsening budget restraints, no direct successor, even though the maritime surveillance duties were taken over by Dornier Do 228/NGs operated by the German Marineflieger (naval air arm).

  

General characteristics:

Crew: Two: pilot, observer/systems operator

Length: 44 ft 4 in (13.53 m) overall with FLIR sensor and IR jammer

Wingspan: 42 ft 0 in (12.8 m)

Height: 12 ft 8 in (3.86 m)

Wing area: 330 sq. ft (30.65 m²)

Empty weight: 12,054 lb (5,467 kg)

Loaded weight: 15,544 lb (7,051 kg)

Max. takeoff weight: 18,109 lb (8,214 kg)

 

Powerplant:

2× Lycoming T53-L-701 turboprops, 1,400 shp (1,044 kW) each

 

Performance:

Never exceed speed: 450 mph (390 knots, 724 km/h)

Maximum speed: 305 mph (265 knots, 491 km/h) at 10,000 ft (3,050 m)

Cruise speed: 207 mph (180 knots, 334 km/h) (econ cruise)

Stall speed: 84 mph (73 knots, 135 km/h)

Range: 944 mi (820 nmi, 1,520 km) (SLAR mission)

Service ceiling: 25,000 ft (7,620 m)

Rate of climb: 3,450 ft/min (17.5 m/s)

 

Armament:

A total of eight external hardpoints (two ventral, three under each outer wing)

for external loads; the wing hardpoints were typically occupied with ELINT sensor pods, while the

ventral hardpoints frequently carried 300 l drop tanks to extend loiter time and range;

Typically, no offensive armament was carried, even though bombs or gun/missile pods were possible.

  

The kit and its assembly:

This build became a submission to the “Reconnaissance” Group Build at whatifmodellers.com in July 2021, and it spins further real-world events. Germany actually tested two OV-1s in the Sixties (by the German Army/Bundesheer, not by the air force), but the type was not procured or operated. The test aircraft carried a glossy, olive drab livery (US standard, I think) with German national markings.

However, having a vintage Hasegawa OV-1A in the stash, I wondered what an operational German OV-1 might have looked like, especially if it had been operated into the Eighties and beyond, in the contemporary Norm 83 paint scheme? This led to this purely fictional OV-1G.

 

The kit was mostly built OOB, and the building experience was rather so-so – after all, it’s a pretty old mold/boxing (in my case the Hasegawa/Hales kit is from 1978, the mold is from 1968!). Just a few things were modified/added in order to tweak the standard, short-winged OV-1A into something more modern and sophisticated.

 

When searching for a solution to mount some ELINT sensor arrays, I did not want to copy the OV-1B’s characteristic offset, ventral SLAR fairing. I rather settled for the late RV-1D’s solution with sensor pods under the outer wings. Unfortunately, the OV-1A kit came with the type’s original short wings, so that the pods had to occupy the inner underwing pair of hardpoints. The pods were scratched from square styrene profiles and putty, so that they received a unique look. The Mohawk’s pair of ventral hardpoints were mounted, but – after considering some drop tanks or an ECM pod there - left empty, so that the field of view for the ventral panoramic camera would not be obscured.

 

Other small additions are some radar warning sensor bumps on the nose, some extra antennae, a shallow bulge for the MIDS antenna on the spine, the FLIR turret on the nose (with parts from an Italeri AH-1 and a Kangnam Yak-38!), and I added a tail stinger for a retrofitted (scratched) IR decoy device, inspired by the American AN/ALG-147. This once was a Matchbox SNEB unguided missile pod.

  

Painting and markings:

For the intended era, the German Norm 83 paint scheme, which is still in use today on several Luftwaffe types like the Transall, PAH-2 or CH-53, appeared like a natural choice. It’s a tri-color wraparound scheme, consisting of RAL 6003 (Olivgrün), FS 34097 (Forest Green) and RAL 7021 (Teerschwarz). The paints I used are Humbrol 86 (which is supposed to be a WWI version of RAL 6003, it lacks IMHO yellow but has good contrast to the other tones), Humbrol 116 and Revell 9. The pattern itself was adapted from the German Luftwaffe’s Dornier Do 28D “Skyservants” with Norm 83 camouflage, because of the type’s similar outlines.

 

A black ink washing was applied for light weathering, plus some post-shading of panels with lighter shades of the basic camouflage tones for a more plastic look. The cockpit interior was painted in light grey (Humbrol 167), while the landing gear and the interior of the air brakes became white. The scratched SLAR pods became light grey, with flat di-electric panels in medium grey (created with decal material).

The cockpit interior was painted in a rather light grey (Humbrol 167), the pilots received typical olive drab Luftwaffe overalls, one with a white “bone dome” and the other with a more modern light grey helmet.

 

The decals were improvised. National markings and tactical codes came from TL Modellbau sheets, the AG 51 emblems were taken from a Hasegawa RF-4E sheet. The black walkways were taken from the Mohak’s OOB sheet, the black de-icer leading edges on wings and tail were created with generic black decal material. Finally, the model was sealed with a coat of matt acrylic varnish (Italeri).

  

An interesting result, and the hybrid paint scheme with the additional desert camouflage really makes the aircraft an unusual sight, adding to its credibility.

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based on historical facts. BEWARE!

  

Some background:

The McDonnell Douglas (now Boeing) T-45 Goshawk was a highly modified version of the BAe Hawk land-based training jet aircraft. Manufactured by McDonnell Douglas (now Boeing) and British Aerospace (now BAe Systems), the T-45 was used by the United States Navy and the United States Marine Corps (USMC) as an aircraft carrier-capable trainer.

The Goshawk's origins began in the mid-1970s, when the US Navy began looking for a single aircraft replacement for both its T-2 and TA-4 jet trainers. The US Navy started the VTXTS advanced trainer program in 1978. Several companies made submissions, e. g. North American or Northrop/Vought. Due to the size of the potential contract, European companies made submissions, too, including a navalized Alpha Jet from Dassault/Dornier and a fully carrier-capable version of the BAe Hawk Mk.60, mutually proposed by British Aerospace (BAe) and McDonnell Douglas (MDC). The latter eventually won the competition and BAe and MDC were awarded the T-45 contract in 1981.

 

The Hawk had not been designed for carrier operations and numerous modifications were required to make it suitable for use on carriers. These included improvements to the low-speed handling characteristics and a reduction in the approach speed. It was found that the aircraft was apt to stall at the low approach speed required. Modifications were designed by BAe in England; most notably a simple slat system was devised, operated by an actuator and linkage mechanism to fit into the small space available. Strakes were also added on the fuselage to improve airflow. Other changes were a strengthened airframe, a more robust and wider landing gear with a two-wheel nose landing gear, a catapult tow bar attachment and an arresting hook. The modified aircraft was christened “Goshawk”, flew in 1988 for the first time and became operational in 1991.

 

Beyond being a naval trainer the T-45 was also adapted for first-line duty with strike capabilities, in the form of the OA-45 for the USMC. The role of this aircraft dated back to the Vietnam War when twenty-three A-4 two-seaters were converted into OA-4Ms for “FastFAC” (Fast Forward Air Controller) missions, in order to control interdiction sorties dedicated to shaping the battlefield for future operations. Basically, the OA-4M was a TA-4F equipped with A-4M electronics. The most visible and characteristic change was the fitting of the A-4M’s dorsal electronics hump, neatly faired into the rear of the two-seat canopy. The nose sensor group of the OA-4M was basically the same as that of the A-4M, but the Angle/Rate Bombing system was not installed as it would not be needed.

 

When the T-45 was introduced in the early Nineties, the USMCs OA-4Ms had reached the end of their service life and the USMC started looking for a replacement, wanting a comparable, light and fast fixed-wing aircraft. The USMC did not accept the LTV A-7 as an A-4 replacement (even though a two-seater version was available), because it was already dated, too, and not part of the USMC inventory. The USMC's A-4Ms were supposed to be replaced by the VTOL AV-8 by the mid-nineties, but the AV-8, even as a two-seater, was deemed unsuitable for FFAC duties. The new T-45 looked like a good and economical alternative with future potential, since the airframe was brand new and the type's infrastructure was fully established, so that a small number of specialized aircraft could easily be supported without much extra cost.

 

With fresh experience from the 1st Gulf War in 1990-91 the decision was made to buy 25 extra T-45A airframes and convert them to OA-45A standard. Most important change were modified wings, using structures and systems from the BAe Hawk 100 series. While the T-45 only had two underwing and a single ventral hardpoint, the OA-45A featured a total of seven: four underwing and one ventral hardpoints, plus wingtip stations for defensive air-to-air missiles. Upgraded avionics allowed the deployment of a wide range of external stores, including air-to-ground missiles and rocket launchers, a reconnaissance pod, retarded and free-fall bombs of up to 1,000 pounds (450 kg) caliber, runway cratering, anti-personnel and light armor bombs, cluster bombs, practice bombs as well as external fuel tanks and ECM pods. This was a vital asset, since Desert Storm had proved that FFAC aircraft had to have an offensive capability to handle targets of opportunity on their own, when no air assets to control were available. A total ordnance load of up to 6,800 lb (3,085 kg) was possible, even though the aircraft was not supposed to play an offensive role and rather act from a distance, relying on its small size and agility.

 

Communication modifications for the FastFAC role included a KY-28 secure voice system, an ARC-159 radio and an ARC-114 VHF radio. Similar to the Skyhawk, a hump behind the cockpit had to be added to make room for the additional electronic equipment and a heat exchanger. Other additions were a continuous-wave Doppler navigation radar under a shallow ventral radome underneath the cockpit, a ground control bombing system, an APN-194 altimeter, an ALR-45 radar warning suite, a retrofitted, fixed midair refueling probe and cockpit armor plating that included Kevlar linings on the floor and the lower side walls as well as externally mounted armor plates for the upper areas.

 

VMA-131 of Marine Aircraft Group 49 (the Diamondbacks) retired its last four OA-4Ms on 22 June 1994, and the new OA-45A arrived just in time to replace the venerable Skyhawk two-seaters in the FastFAC role. Trainer versions of the Skyhawk remained in Navy service, however, finding a new lease on life with the advent of "adversary training". OA-45A deliveries were finished in 1996 and the 25 aircraft were distributed among the newly established Marine Aviation Logistics Squadron (MALS, formerly Headquarters & Maintenance Squadron/H&MS) 12 & 13. The USMC crews soon nicknamed their new mounts "GosHog", to underlöine ist offensive capabilities and to set themselves apart from the USN's "tame" trainers. Even though thos name was never officially approved it caught on quickly.

 

After initial experience with the new aircraft and in the wake of technological advances, the USMC decided to upgrade the OA-45As in 2000 to improve its effectiveness and interaction capabilities with ground troops. This primarily resulted in the addition of a forward-looking infrared camera laser in the aircraft’s nose section, which enabled the aircraft to execute all-weather/night reconnaissance and to illuminate targets for laser-guided infantry shells or ordnance launched by the OA-45 itself or by other aircraft. Through this measure the OA-45 became capable of carrying and independently deploying light laser-guided smart weapons like the GBU-12 and -16 “Paveway II” glide bombs or the laser-guided AGM-65E “Maverick” variant. The update was gradually executed during regular overhauls in the course of 2001 and 2002 (no new airframes were built/converted), the modified machines received the new designation OA-45B.

 

After this update phase, the OA-45Bs were deployed in several global conflicts and saw frequent use in the following years. For instance, MALS 13 used its OA-45Bs operationally for the first time in October 2002 when the squadron was tasked with providing support to six AV-8B Harrier aircraft in combat operations in Afghanistan during Operation Enduring Freedom. This mission lasted until October 2003, four aircraft were allocated and one OA-45B was lost during a landing accident.

On 15 January 2003, MALS 13 embarked 205 Marines and equipment aboard the USS Bonhomme Richard in support of combat operations in Southwest Asia during Operation Southern Watch. Four OA-45Bs successfully supported these troops from land bases, marking targets and flying reconnaissance missions.

Furthermore, six MALS 13 OA-45Bs took actively part in Operation Iraqi Freedom from Al Jaber Air Base, Kuwait, and An Numiniyah Expeditionary Air Field, Iraq, where the aircraft worked closely together with the advancing ground troops of the USMC’s 15th Marine Expeditionary Unit. They successfully illuminated targets for US Navy fighter bombers, which were launched from USS Abraham Lincoln (CVN-72) in the Persian Gulf, and effectively guided these aircraft to their targets. Two OA-45Bs were lost during this conflict, one through enemy MANPADS, the other through friendly AA fire. In late May 2003 the surviving machines and their crews returned to MCAS Yuma.

 

On 16 March 2007, the 200th T-45 airframe was delivered to the US Navy. From this final batch, six airframes were set aside and modified into OA-45Bs in order to fill the losses over the past years.

Later T-45 production aircraft were built with enhanced avionics systems for a heads-up display (HUD) and glass cockpit standard, while all extant T-45A aircraft were eventually converted to a T-45C configuration under the T-45 Required Avionics Modernization Program (T-45 RAMP), bringing all aircraft to same HUD plus glass cockpit standard. These updates, esp. concerning the cockpit, were introduced to the OA-45Bs, too, and they were re-designated again, now becoming OA-45Cs, to reflect the commonality with the Navy’s Goshawk trainers. Again, these modifications were gradually introduced in the course of the OA-45s’ normal maintenance program.

 

In 2007, an engine update of the whole T-45 fleet, including the OA-45s, with the Adour F405-RR-402 was considered. This new engine was based on the British Adour Mk 951, designed for the latest versions of the BAe Hawk and powering the BAe Taranis and Dassault nEUROn UCAV technology demonstrators. The Adour Mk 951 offered 6,500 lbf (29 kN) thrust and up to twice the service life of the F405-RR-401. It featured an all-new fan and combustor, revised HP and LP turbines, and introduced Full Authority Digital Engine Control (FADEC). The Mk 951 was certified in 2005, the F405-RR-402 derived from it was certified in 2008, but it did not enter service due to funding issues, so that this upgrade was not carried out.

 

The final delivery of the 246th T-45 airframe took place in November 2009, and both T-45 and the OA-45 "GosHog" are supposed to remain in service until 2035.

  

General characteristics:

Crew: 2 (pilot, observer)

Length: 39 ft 4 in (11.99 m)

Wingspan: 30 ft 10 in (9.39 m)

Height: 13 ft 5 in (4.08 m)

Wing area: 190.1 ft² (17.7 m²)

Empty weight: 10,403 lb (4,460 kg)

Max. takeoff weight: 14,081 lb (6,387 kg)

 

Powerplant:

1× Rolls-Royce Turbomeca F405-RR-401 (Adour) non-afterburning turbofan with 5,527 lbf (26 kN)

 

Performance:

Maximum speed: Mach 2 (2,204 km/h (1,190 kn; 1,370 mph) at high altitude

Combat radius: 800 km (497 mi, 432 nmi)

Ferry range: 3,200 km (1,983 mi) with drop tanks

Service ceiling: 15,240 m (50,000 ft)

Wing loading: 283 kg/m² (58 lb/ft²)

Thrust/weight: 0.97

Maximum g-load: +9 g

 

Armament:

No internal gun; seven external hardpoints (three on each wing and one under fuselage)

for a wide range of ordnance of up to 6,800 lb (3,085 kg), including up to six AIM-9 Sidewinder for

self-defense, pods with unguided rockets for target marking or ECM pods, but also offensive weapons

of up to 1.000 lb (454 kg) weight, including iron/cluster bombs and guided AGM-65, GBU-12 and -16.

  

The kit and its assembly:

This fictional T-45 variant is actually the result of a long idea evolution, and simply rooted in the idea of a dedicated OA-4M replacement for the USMC; in real life, the FFAC role has been transferred to F-18 two-seaters, though, but the T-45 appeared like a sound alternative to me.

 

There's only one T-45 kit available, a dubious T-45A from Italeri with poor wings and stabilizers. Wolfpack also offers a T-45, but it’s just a re-boxing of the Italeri kit with some PE parts and a price tag twice as big – but it does not mend the original kit’s issues… After reading the A-4 Skyhawk book from the French "Planes & Pilots" series, I was reminded of the USMC's special OA-4M FAC two-seaters (and the fact that it is available in kit form from Italeri and Hasegawa), and, cross-checking the real-world timeline of the T-45, I found that it could have been a suitable successor. The ide of the USMC’s OA-45 was born! :D

 

Building-wise the Italeri T-45 remained close to OOB, even though I transplanted several parts from an Italeri BAe Hawk Mk. 100 to create a different look. I modified the nose with the Mk. 100’s laser fairing and added some radar warning sensor bumps. This transplantation was not as easy as it might seem because the T-45’s nose is, due to the different and more massive front landing gear quite different from the Hawk’s. Took some major PSR to integrate the laser nose.

An ALR-45 “hot dog” fairing from a late A-4M (Italeri kit) was added to the fin, together with a small styrene wedge extending the fin’s leading edge. This small detail markedly changes the aircraft’s look. I furthermore added a refueling probe, scratched from coated wire and some white glue, as well as a low “camel back” fairing behind the cockpit, created from a streamlined bomb half with air outlets for an integrated heat exchanger. Blade antennae were relocated and added. A shallow bump for the Doppler radar was added under the fuselage behind the landing gear well – left over from an Airfix A-4B (from an Argentinian A-4P, to be correct, actually a dorsal fairing).

 

On the wings, a tailored pair of pylons and wing tip launch rails from the Italeri BAe Hawk Mk. 100 kit were added, too, as well as the donor kit’s pair of Sidewinders. The rest of the ordnance consists of drop tanks and LAU-19 pods for target marking missiles. The tanks were taken from the Hawk Mk. 100 kit, too, the rocket launchers came from an Italeri NATO aircraft weapons set. The centerline position carries an ALQ-131 ECM pod from a Hasegawa US aircraft weapons set on a pylon from the scrap box.

  

Painting and markings:

The low-viz idea prevailed, since I had some leftover OA-4M decals from Italeri kits in store, as well as some other suitable low-viz decals from a Revell A-4F kit. However, an all-grey livery was IMHO not enough, and when I came across a picture of a USN low-viz A-7E with an improvised desert camouflage in sand and reddish brown applied over the grey (even partly extending over its markings) from Operation Iraqi Freedom, I had that extra twist that would set the OA-45 apart. MALS-13 was chosen as operator because I had matching codes, and, as another benefit, the unit had actually been deployed overseas during the 2003 Iraq War, so that the whif’’s time frame was easily settled, adding to its credibility.

 

The livery was built up just like on the real aircraft: on top of a basic scheme in FS 36320 and 36375 (Humbrol 128 and 127) with a slightly darker anti-glare panel in front of the cockpit (FS 35237, I used Revell 57 as a slightly paler alternative) I applied the low-viz marking decals, which were protected with a coat of acrylic varnish. Next, additional desert camouflage was added with dry-brushed sand and millitary brown (supposedly FS 33711 and 30400 in real life, I used, after consulting pictures of aircraft from both Gulf Wars, Humbrol 103 (Cream) and 234 (Dark Flesh). They were applied with a kind of a dry-brushing technique, for a streaky and worn look, leaving out the codes and other markings. The pattern itself was inspired by an USMC OV-10 Bronco in desert camouflage from the 1st Gulf War.

On top of that a black ink washing was applied. Once things had thoroughly dried over night, I wet-sanded the additional desert camouflage away, carefully from front to back, so that the edges became blurred and the underlying grey became visible again.

 

The cockpit interior was painted in standard Dark Gull Grey (Humbrol 140), while the air intakes and the landing gear became white, the latter with red trim on the covers’ edges – just standard. Finally, the model was sealed with a coat of matt acrylic varnish (Italeri).

  

The upgraded T-45 is an interesting result. The add-ons suit the aircraft, which already looks sturdier than its land-based ancestor, well. The improvised desert paint scheme with the additional two-tone camouflage over the pale grey base really makes the aircraft an unusual sight, adding to its credibility.

Hardware-wise I am really happy how the added dorsal hump blends into the overall lines – in a profile view it extends the canopy’s curve and blends into the fin, much like the A-4F/M’s arrangement. And the modified fin yields a very different look, even though not much was changed. The T-45 looks much beefier now, and from certain angles really reminds of the OA-4M and sometimes even of a diminutive Su-25?

+++ DISCLAIMER +++

Nothing you see here is real, even though the conversion or the presented background story might be based historical facts. BEWARE!

  

The KAI T-50 Golden Eagle (골든이글) is a family of South Korean supersonic advanced trainers and light combat aircraft, developed by Korea Aerospace Industries (KAI) with Lockheed Martin. The T-50 is South Korea's first indigenous supersonic aircraft and one of the world's few supersonic trainers.

 

The T-50 program started in the late Nineties and was originally intended to develop an indigenous trainer aircraft capable of supersonic flight, to train and prepare pilots for the KF-16 and F-15K, replacing trainers such as T-38 and A-37 that were then in service with the ROKAF. Prior South Korean aircraft programs include the turboprop KT-1 basic trainer produced by Daewoo Aerospace (now part of KAI), and license-manufactured KF-16.

 

The mother program, code-named KTX-2, began in 1992, but the Ministry of Finance and Economy suspended the original project in 1995 due to financial constraints. The basic design of the aircraft was set by 1999, and eventually the development of the aircraft was funded 70% by the South Korean government, 17% by KAI, and 13% by Lockheed Martin.

 

In general, the T-50 series of aircraft closely resembles the KF-16 in configuration, but it actually is a completely new design: the T-50 is 11% smaller and 23% lighter than an F-16, and in order to create enough space for the two-seat cockpit, the air intake was bifurcated and placed under the wing gloves, resembling the F/A-18's layout.

 

The aircraft was formally designated as the T-50 'Golden Eagle' in February 2000, the T-50A designation had been reserved by the U.S. military to prevent it from being inadvertently assigned to another aircraft model. Final assembly of the first T-50 took place between 15 January and 14 September 2001. The first flight of the T-50 took place in August 2002, and initial operational assessment from 28 July to 14 August 2003.

 

The trainer has a cockpit for two pilots in a tandem arrangement, both crew members sitting in "normal" election seats, not in the F-16's reclined position. The high-mounted canopy is applied with stretched acrylic, providing the pilots with good visibility, and has been tested to offer the canopy with ballistic protection against 4-lb objects impacting at 400 knots.

 

The ROKAF, as original development driver, placed an initial production contract for 25 T-50s in December 2003, with aircraft scheduled to be delivered between 2005 and 2009. Original T-50 aircraft were equipped with the AN/APG-67(v)4 radar from Lockheed Martin. The T-50 trainer is powered by a GE F404 engine built under license by Samsung Techwin. Under the terms of the T-50/F404-102 co-production agreement, GE provides engine kits directly to Samsung Techwin who produces designated parts as well as performing final engine assembly and testing.

 

The T-50 program quickly expanded beyond a pure trainer concept to include the TA-50 armed trainer aircraft, as well as the FA-50 light attack aircraft, which has already similar capabilities as the multirole KF-16. Reconnaissance and electronic warfare variants were also being developed, designated as RA-50 and EA-50.

 

The TA-50 variant is a more heavily armed version of the T-50 trainer, intended for lead-in fighter training and light attack roles. It is equipped with an Elta EL/M-2032 fire control radar and designed to operate as a full-fledged combat platform. This variant mounts a lightweight three-barrel cannon version of the M61 Vulcan internally behind the cockpit, which fires linkless 20 mm ammunition. Wingtip rails can accommodate the AIM-9 Sidewinder missile, a variety of additional weapons can be mounted to underwing hardpoints, including precision-guided weapons, air-to-air missiles, and air-to-ground missiles. The TA-50 can also mount additional utility pods for reconnaissance, targeting assistance, and electronic warfare. Compatible air-to-surface weapons include the AGM-65 Maverick missile, Hydra 70 and LOGIR rocket launchers, CBU-58 and Mk-20 cluster bombs, and Mk-82, -83, and -84 general purpose bombs.

 

Among the operators of the TA-50 are the Philippines, Thailand and the ROKAF, and the type has attracted a global interest, also in Europe. The young Republic of Scotland Air Corps (locally known as Poblachd na h-Alba Adhair an Airm) chose, soon after the country's independence from the United Kingdom, after its departure from the European Union in 2017, the TA-50 as a complement to its initial procurements and add more flexibility to its small and young air arm.

 

According to a White Paper published by the Scottish National Party (SNP) in 2013, an independent Scotland would have an air force equipped with up to 16 air defense aircraft, six tactical transports, utility rotorcraft and maritime patrol aircraft, and be capable of “contributing excellent conventional capabilities” to NATO. Outlining its ambition to establish an air force with an eventual 2,000 uniformed personnel and 300 reservists, the SNP stated the organization would initially be equipped with “a minimum of 12 interceptors in the Eurofighter/Typhoon class, based at Lossiemouth, a tactical air transport squadron, including around six [Lockheed Martin] C-130J Hercules, and a helicopter squadron”.

 

According to the document, “Key elements of air forces in place at independence, equipped initially from a negotiated share of current UK assets, will secure core tasks, principally the ability to police Scotland’s airspace, within NATO.” An in-country air command and control capability would be established within five years of a decision in favor of independence, it continues, with staff also to be “embedded within NATO structures”.

This plan was immediately set into action after the country's independence in late 2017 with the purchase of twelve refurbished Saab JAS 39A Gripen interceptors for Quick Reaction Alert duties and upgraded, former Swedish Air Force Sk 90 trainers for the RoScAC. But these second hand machines were just the initial step in the mid-term procurement plan.

 

The twelve KAI TA-50 aircraft procured as a second step were to fulfill the complex requirement for a light and cost-effective multi-purpose aircraft that could be used in a wide variety of tasks: primarily as an advanced trainer for supersonic flight and as a trainer for the fighter role (since all Scottish Gripens were single seaters and dedicated to the interceptor/air defense role), but also as a light attack and point defense aircraft.

 

Scotland was offered refurbished F-16C and Ds, but this was declined as the type was deemed to be too costly and complex. Beyond the KAI T-50, the Alenia Aermacchi M-346 Master and the BAe Hawk were considered, too, but, eventually, a modified TA-50 that was tailored to the RoScAC’s procurement plans was chosen by the Scottish government.

 

In order to fulfill the complex duty profile, the Scottish TA-50s were upgraded with elements from the FA-50 attack aircraft. They possess more internal fuel capacity, enhanced avionics, a longer radome and a tactical datalink. Its EL/M-2032 pulse-Doppler radar has been modified so that it offers now a range two-thirds greater than the TA-50's standard radar. It enables the aircraft to operate in any weather, detect surface targets and deploy AIM-120 AAMs for BVR interceptions. The machines can also be externally fitted with Rafael's Sky Shield or LIG Nex1's ALQ-200K ECM pods, Sniper or LITENING targeting pods, and Condor 2 reconnaissance pods to further improve the machine’s electronic warfare, reconnaissance, and targeting capabilities.

 

Another unique feature of the Scottish Golden Eagle is its powerplant: even though the machines are originally powered by a single General Electric F404 afterburning turbofan and designed around this engine, the RoScAC TF-50s are powered by a Volvo RM12 low-bypass afterburning turbofan. These are procured and serviced through Saab in Sweden, as a part of the long-term collaboration contract for the RoScAC’s Saab Gripen fleet. This decision was taken in order to decrease overall fleet costs through a unified engine.

 

The RM12 is a derivative of the General Electric F404-400. Changes from the standard F404 includes greater reliability for single-engine operations (including more stringent birdstrike protection) and slightly increased thrust. Several subsystems and components were also re-designed to reduce maintenance demands, and the F404's analogue Engine Control Unit was replaced with the Digital Engine Control – jointly developed by Volvo and GE – which communicates with the cockpit through the digital data buses and, as redundancy, mechanical calculators controlled by a single wire will regulate the fuel-flow into the engine.

 

Another modification of the RoScAC’s TA-50 is the exchange of the original General Dynamics A-50 3-barrel rotary cannon for a single barrel Mauser BK-27 27mm revolver cannon. Being slightly heavier and having a lower cadence, the BK-27 featured a much higher kinetic energy, accuracy and range. Furthermore, the BK-27 is the standard weapon of the other, Sweden-built aircraft in RoScAC service, so that further synergies and cost reductions were expected.

 

The Scottish Department of National Defense announced the selection of the TA-50 in August 2018, after having procured refurbished Saab Sk 90 and JAS 39 Gripen from Sweden as initial outfit of the country's small air arm with No. 1 Squadron based at Lossiemouth AB.

 

Funding for the twelve aircraft was approved by Congress on September 2018 and worth € 420 mio., making the Golden Eagle the young country’s first brand new military aircraft. Deliveries of the Golden Hawk TF.1, how the type was officially designated in Scottish service, began in November 2019, lasting until December 2020.

The first four Scottish Golden Hawk TF.1 aircraft were allocated to the newly established RoScAC No. 2 Squadron, based at Leuchars, where the RoScAC took control from the British Army. The latter had just taken over the former air base from the RAF in 2015, losing its “RAF air base” status and was consequentially re-designated “Leuchars Station”, primarily catering to the Royal Scots Dragoon Guards who have, in the meantime, become part of Scotland’s Army Corps. The brand new machines were publically displayed on the shared army and air corps facility in the RoScAC’s new paint scheme on 1st of December 2019 for the first time, and immediately took up service.

 

General characteristics:

Crew: 2

Length: 13.14 m (43.1 ft)

Wingspan (with wingtip missiles): 9.45 m (31 ft)

Height: 4.94 m (16.2 ft)

Wing area: 23.69 m² (255 ft²)

Empty weight: 6,470 kg (14,285 lb)

Max. takeoff weight: 12,300 kg (27,300 lb)

 

Powerplant:

1× Volvo RM12 afterburning turbofan, rated at 54 kN (12,100 lbf) dry thrust

and 80.5 kN (18,100 lbf) with afterburner

 

Performance:

Maximum speed: Mach 1.5 (1,640 km/h, 1,020 mph at 9,144 m or 30,000 ft)

Range: 1,851 km (1,150 mi)

Service ceiling: 14,630 m (48,000 ft)

Rate of climb: 198 m/s (39,000 ft/min)

Thrust/weight: 0.96

Max g limit: -3 g / +8 g

 

Armament:

1× 27mm Mauser BK-27 revolver cannon with 120 rounds

A total of 7 hardpoints (4 underwing, 2 wingtip and one under fuselage)

for up to 3,740 kg (8,250 lb) of payload

  

The kit and its assembly:

A rare thing concerning my builds: an alternative reality whif. A fictional air force of an independent Scotland crept into my mind after the hysterical “Brexit” events in 2016 and the former (failed) public vote concerning the independence of Scotland from the UK. What would happen to the military, if the independence would take place, nevertheless, and British forces left the country?

 

The aforementioned Scottish National Party (SNP) paper from 2013 is real, and I took it as a benchmark. Primary focus would certainly be set on air space defense, and the Gripen appears as a good and not too expensive choice. The Sk 90 is a personal invention, but would fulfill a good complementary role.

Nevertheless, another multi-role aircraft would make sense as an addition, and both M-346 and T-50 caught my eye (Russian options were ruled out due to the tense political relations), and I gave the TA-50 the “Go” because of its engine and its proximity to the Gripen.

 

The T-50 really looks like the juvenile offspring from a date between an F-16 and an F-18. There’s even a kit available, from Academy – but it’s a Snap-Fit offering without a landing gear but, as an alternative, a clear display that can be attached to the engine nozzle. It also comes with stickers instead of waterslide decals. This sounds crappy and toy-like, but, after taking a close look at kit reviews, I gave it a try.

 

And I am positively surprised. While the kit consists of only few parts, moulded in the colors of a ROCAF trainer as expected, the surfaces have minute, engraved detail. Fit is very good, too, and there’s even a decent cockpit that’s actually better than the offering of some “normal” model kits. The interior comes with multi-part seats, side consoles and dashboards that feature correctly shaped instrument details (no decals). The air intakes are great, too: seamless, with relatively thin walls, nice!

 

So far, so good. But not enough. I could have built the kit OOB with the landing gear tucked up, but I went for the more complicated route and trans-/implanted the complete landing gear from an Intech F-16, which is available for less than EUR 5,- (and not much worth, to be honest). AFAIK, there’s white metal landing gear for the T-50 available from Scale Aircraft Conversions, but it’s 1:48 and for this set’s price I could have bought three Intech F-16s…

 

But back to the conversion. This landing gear transplantation stunt sounds more complicated as it actually turned out to be. For the front wheel well I simply cut a long opening into the fuselage and added inside a styrene sheet as a well roof, attached under the cockpit floor.

For the main landing gear I just opened the flush covers on the T-50 fuselage, cut out the interior from the Intech F-16, tailored it a little and glued it into its new place.

 

This was made easy by the fact that the T-50 is a bit smaller than the F-16, so that the transplants are by tendency a little too large and offer enough “flesh” for adaptations. Once in place, the F-16 struts were mounted (also slightly tailored to fit well) and covers added. The front wheel cover was created with 0.5 mm styrene sheet, for the main covers I used the parts from the Intech F-16 kit because they were thinner than the leftover T-50 fuselage parts and feature some surface detail on the inside. They had to be adapted in size, though. But the operation worked like a charm, highly recommended!

 

Around the hull, some small details like missing air scoops, some pitots and antennae were added. In a bout of boredom (while waiting for ordered parts…) I also added static dischargers on the aerodynamic surfaces’ trailing edges – the kit comes with obvious attachment points, and they are a small detail that improves the modern look of the T-50 even more.

 

Since the Academy kit comes clean with only a ventral drop tank as ordnance, underwing pylons from a SEPECAT Jaguar (resin aftermarket parts from Pavla) and a pair of AGM-65 from the Italeri NATO Weapons set plus launch rails were added, plus a pair of Sidewinders (from a Hasegawa AAM set, painted as blue training rounds) on the wing tip launch rails.

Since the T-50 trainer comes unarmed, a gun nozzle had to be added – its position is very similar to the gun on board of the F-16, on the upper side of the port side LERX. Another addition are conformal chaff/flare dispensers at the fin’s base, adding some beef to the sleek aircraft.

  

Painting and markings:

I did not want a grey-in-grey livery, yet something “different” and rather typical or familiar for the British isles. My approach is actually a compromise, with classic RAF colors and design features inspired by camouflage experiments of the German Luftwaffe on F-4F Phantoms and Alpha Jets in the early Eighties.

 

For the upper sides I went for a classic British scheme, in Dark Green and Dark Sea Grey (Humbrol 163 and 164), colors I deem very appropriate for the Scottish landscape and for potential naval operations. These were combined with elements from late RAF interceptors: Barley Grey (Humbrol 167) for the flanks including the pylons, plus Light Aircraft Grey (Humbrol 166) for the undersides, with a relatively high waterline and a grey fin, so that a side or lower view would rather blend with the sky than the ground below.

 

Another creative field were the national markings: how could fictional Scottish roundels look like, and how to create them so that they are easy to make and replicate (for a full set for this kit, as well as for potential future builds…)? Designing and printing marking decals myself was an option, but I eventually settled for a composite solution which somewhat influenced the roundels’ design, too.

My Scottish roundel interpretationconsists of a blue disk with a white cross – it’s simple, different from any other contemporary national marking, esp. the UK roundel, and easy to create from single decal parts. In fact, the blue roundels were die-punched from blue decal sheet, and the cross consists of two thin white decal strips, cut into the correct length with the same stencil, using generic sheet material from TL Modellbau.

 

Another issue was the potential tactical code, and a small fleet only needs a simple system. Going back to a WWII system with letter codes for squadrons and individual aircraft was one option, but, IMHO, too complicated. I adopted the British single letter aircraft code, though, since this system is very traditional, but since the RoScAC would certainly not operate too many squadrons, I rather adapted a system similar to the Swedish or Spanish format with a single number representing the squadron. The result is a simple 2-digit code, and I adapted the German system of placing the tactical code on the fuselage, separated by the roundel. Keeping British traditions up I repeated the individual aircraft code letter on the fin, where a Scottish flag, a small, self-printed Fife coat-or-arms and a serial number were added, too.

 

The kit saw only light weathering and shading, and the kit was finally sealed with matt acrylic varnish (Italeri).

  

Creating this whif, based on an alternative historic timeline with a near future perspective, was fun – and it might spawn more models that circle around the story. A Scottish Sk 90 and a Gripen are certain options (and for both I have kits in the stash…), but there might also be an entry level trainer, some helicopters for the army and SAR duties, as well as a transport aircraft. The foundation has been laid out, now it’s time to fill Scotland’s history to come with detail and proof. ;-)

 

Besides, despite being a snap-fit kit, Academy’s T-50 is a nice basis, reminding me of some Hobby Boss kits but with less flaws (e .g. most of the interiors), except for the complete lack of a landing gear. But with the F-16 and Jaguar transplants the simple kit developed into something more convincing.