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Looking north along the footpath and cycleway which has been built on the trackbed of the former single track railway branch line which ran between Lanacster Castle & Green Ayre Stations until its closure in 1966.

 

The line was included the Midland Railway's pioneering electrification scheme of 1908 which provided an efficient rapid transit network between Lancaster, Morecambe & Heysham which used an overhead power supply at 6.6kV AC at 25Hz though changed to the U.K. standard 50Hz cycle in the early 1950s when the system was upgraded as a testbed for future main line electrification schemes in the U.K.

Airbus A380-861

MSN 004 [Engine Alliance testbed]

F-WWDD 'VNO' ['#A380' 'iflyA380.com' decals]

 

iflya380.com/

 

Airbus S.A.S.

 

Copyright © 2016 A380spotter. All rights reserved.

  

www.farnborough.com

 

Experimental, prototype testbed battery electric Alexander Dennis Enviro200 at Hatfield

Yes! Honest to God, yes! After years of searching I have found myself one of the rarest and most strangest cars you ever did see!

 

What you're looking at here is the Rolls Royce Camargue, very much the Rolls Royce that time forgot. What can you even say about it? It's one of the most iconic automotive failures in history, and certainly a car that Rolls Royce fans are always very quick to wince at when I mention it at RREC conventions.

 

So where did this curious car come from? To truly understand this mighty machine you need to go back to 1969, where a massive change in the image and style of the world was starting to hold sway. In the world of autos, the curvature of the 1950's and early 60's was giving way to the angles of the 1970's, the decade that gave us the 'Wedge' sportsers and boxy saloon cars.

 

Rolls Royce, who at this point were building three cars, the Phantom VI, the Silver Shadow, and the Silver Shadow Two-Door Saloon (later to be known as the Corniche), were looking for a new design that would drastically alter its image from that of the Shadow. Originally, the intention was to use their new brainchild to replace the Two-Door Saloon, but due to financial difficulty within the Rolls Royce company, later followed by bankruptcy after the RB211 Jet Engine project, the company chose instead to save costs and rebrand it as the Corniche instead.

 

For their new car, Rolls Royce chose not to have it designed in-house like previous models, but went for the first time to Pininfarina of Italy. Throughout the remainder of 1969 the company toyed with many sketches, until in 1970 a final design was chosen and given the go by the Rolls Royce management, with the intention for a launch in either late 1972 or early 1973. Within the company, the project was dubbed "Delta", but was later changed to DY20, with ‘D’ signifying Delta, ‘Y’ signifying it was based on the SY (Silver Shadow) platform, and '20' shortened from 120 which was the car’s wheelbase of 120 inches.

 

But as mentioned, following the amount of money poured into the new Rolls Royce RB211 Jet Engine Project for the Lockheed Tristar, the company was bankrupt as of the 4th February 1971. The result was that the Motor Car Division, whose future now rested in the hands of the Official Receiver, had to look closely at all aspects of the business. This led to the splitting of the Rolls Royce company, with Rolls Royce Motors Ltd. being founded and placed under the ownership of Vickers, whilst the bankrupt Rolls Royce Ltd. was nationalised.

 

During this turbulent period, the DY20 project was closely scrutinised and the Receiver gave the go-ahead to commence the project, but following a critical review of the engineering specification for the car, a decision was taken to delay the launch date until 1975.

 

With development continuing, HJ Mulliner Park Ward, who already built the bodies for the Corniche, were chosen to manufacture the bodies of the DY20 project. In the summer of 1972, the first prototype D1 was released and tested heavily to maintain the standard of reliable excellence that Rolls Royce had been known for. At first the car's initial reception was warm, with people noting that it looked far more futuristic than the Shadow on which it was heavily based. Aside from sharing the same running gear, platform, Rolls Royce V8 engine and a majority of the internal features as the Shadow, the car was endearing in that it was fitted with a new and highly sophisticated bi-level automatic air conditioning system that at that time was the very first car in the world to have such a unit fitted. It was declared that this feature alone was more expensive than a British Leyland Mini! Another change was an instrument board, which many commented wouldn't have looked out of place on the flight deck of a Boeing 747!

 

Throughout 1972 and 73 more prototypes continued to be released and tested, with Rolls Royce giving paramount assistance to HJ Mulliner Park Ward's staff as they rigorously put these cars together. On the 18 January 1973 the body of the first production prototype, assigned D3, was attached to the front and rear sub frame assemblies on the normal Silver Shadow production line with maximum security in place and, following the production line assembly, the car was delivered to the experimental department to begin a period of intensive development work.

 

From May 1973 and all through 1974 production increased but still subject to extreme security. The production sequence was shared between MPW and Crewe. Once the body had been produced in the London factory and despatched to Crewe it was ‘finished painted’, attached to the front and rear sub frames and sent in a part built state back to MPW for all trim, general finishing and testing to take place at Hythe Road.

 

In January 1975, the car was officially launched in Catania, Sicily, and christened the name Camargue, an area situated in the delta of the River Rhône in France. Following a very successful press launch, the car was unveiled to the world on 5 March 1975 and the price quoted was £29,250, which made it the most expensive production car in the world ever at that time. Today, this figure translates out to £272,000. To put the price in perspective with other Rolls-Royce models at the time the Corniche saloon car cost £19,013 and the “Flagship of the Fleet” Phantom VI only cost £21,352!

 

The car was launched in the United States a year later after delays in fitting the cars with US Specification running gear meant that production didn't begin until August 1975. The cost of these cars in the US was $147,000, which today is about $588,000.

 

So, after a turbulent development mired in bankruptcy, a complicated building strategy and a delayed launch in America, did Rolls Royce's gamble with an audaciously designed car pay off?

 

Not in the slightest!

 

Purists recoiled at the sight of the angular corners and straight lines, with its big round headlights and chunky panels that made it look less like a Rolls Royce and more like a Lincoln Continental. They argued that for much, much less, owners could buy a Corniche or a Shadow which looked twice as good and performed just as well. This was then added to by the fuel crisis of the late 1970's, upon which that 6.75L Rolls Royce V8 soaking up petrol at a gallon every 15 miles looked deeply undesirable.

 

In all, only 531 of these cars were ever produced during its 11 year lifetime, but with a few variations. In 1985 a specialist hunting car called the Sbarro was reengineered for an Arabian aristocrat, whilst in 1979 two Camargues were used as testbeds for developments that would later find their way into the Silver Spirit/Spur range, including headlights and other features. In 1985 a single Bentley Camargue was also built, identical except for the changed badge and Grille, although many aftermarket conversions are known to exist. The last two cars rolled off the production line on Christmas Eve 1986 bound for Japan, at a price of £83,000.

 

Today, the Rolls Royce Camargue is a very, very rare car, and you would be hard pressed to find them routinely. In the United States a few continue to roam the countryside, with around 200 of the cars being exported there. Reception of these cars sadly continues to be very critical, with the car often topping people's lists for worst car ever made or ugliest car ever made. Although James May is one of a few people who defend this car, dubbing it "like that pug-faced but well-dressed bloke down the pub", for the most part all people can do is laugh at this car, laugh for the fact that it didn't sell, didn't look good and went through so much trouble to design and build that it was just a rushed embarrassment for the Rolls Royce company.

 

The reputation of these cars is so bad that in spite of its rarity, owners can't even give these things away, with most that I've seen going for as little as £20,000. But a word of advice, stop laughing, and buy their car! £20,000 for a two-door luxury saloon, a pedigree Rolls Royce, and one that once held the distinction of being the world's most expensive production car, you not only get this car for the cost of an equivalent Ford or Vauxhall, but you also make a saving on the original price tag of £252,000, that's over a quarter of a million pounds!

 

Me personally, I absolutely adore these cars! Indeed they're not as pretty as other Rollers, but I consider this a car that you not only have to feel sorry for, considering the background troubles that trailed its development from the start, but one that you have to admire as well. I feel that it's a car that's stood the test of time, a bit of automotive history from the 1970's that shows how reckless and ambitious we were with our car construction, like the Aston Martin Lagonda, brash in the extreme, but lovable all the same.

 

In fact if I had £20,000 right now I'd gladly go out and buy one, not only because I'd be saving a fortune, but also because it's a very personable little car, the kind of car you can't take your eyes off of, the car you could really give a name and love forever.

 

I'd name mine Christie! :D

23rd August 2018., Dublin Airport, Ireland

 

+++ 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 Northrop Grumman-IAI F-24 is the latest reincarnation of the USAF "Lightweight Fighter Program" which dates back to the 1950ies and started with the development of Northrop's F-5 "Freedom Fighter".

 

The 1st generation F-5 became very successful in the export market and saw a long line of development, including the much more powerful F-5E "Tiger II" and the F-20 Tigershark (initially called F-5G). Northrop had high hopes for the F-20 in the international market; however, policy changes following Ronald Reagan's election meant the F-20 had to compete for sales against aircraft like the F-16, the USAF's latest fighter design (which was politically favored). The F-20 development program was eventually abandoned in 1986 after three prototypes had been built and a fourth partially completed.

 

But this was not the end for Northrop’s Lightweight Fighter. In the early 1980s, two X-29As experimental aircraft were built by Grumman from two existing Northrop F-5A Freedom Fighter airframes. The Grumman X-29 was a testbed for forward-swept wings, canard control surfaces, and other novel aircraft technologies. The aerodynamic instability of this arrangement increased agility but required the use of computerized fly-by-wire control. Composite materials were used to control the aeroelastic divergent twisting experienced by forward-swept wings, also reducing the weight. The NASA test program continued from 1984 to 1991 and the X-29s flew 242 times, gathering valuable data and breaking ground for new aerodynamic technologies of 4th and 5th generation fighters.

 

Even though no service aircraft directly evolved from the X-29, its innovative FBW system as well as the new material technologies also opened the door for an updated F-20 far beyond the 1990ies. It became clear that ever expensive and complex aircraft could not be the answer to modern, asymmetrical warfare in remote corners of the world, with exploding development costs and just a limited number of aircraft in service that could not generate true economies of scale, esp. when their state-of-the-art design would not permit any export.

Anyway, a global market for simpler fighter aircraft was there, as 1st generation F-16s as well as the worldwide, aging F-5E fleet and types of Soviet/Russian origin like the MiG-29 provided the need for a modern, yet light and economical jet fighter. Contemporary types like the Indian HAL Tejas, the Swedish Saab Gripen, the French Dassault Rafale and the Pakistani/Chinese FC-1/JF-17 ”Thunder” proved this trend among 4th - 4.5th generation fighter aircraft.

 

Northrop Grumman (Northrop bought Grumman in 1994) initiated studies and basic design work on a respective New Lightweight Fighter (NLF) as a private venture in 1995. Work on the NLF started at a slow pace, as the company was busy with re-structuring.

The idea of an updated lightweight fighter was fueled by another source, too: Israel. In 1998 IAI started looking in the USA for a development partner for a new, light fighter that would replace its obsolete Kfir fleet and partly relieve its F-16 and F-15 fleet from interception tasks. The domestic project for that role, the IAI Lavi, had been stillborn, but lots of its avionics and research were still at hand and waited for an airframe for completion.

The new aircraft for the IAF was to be superior to the MiG-29, at least on par with the F-16C/D, but easier to maintain, smaller and overall cheaper. Since the performance profiles appeared to be similar to what Northrop Grumman was developing under the NLF label, the US company eventually teamed up with IAI in 2000 and both started the mutual project "Namer" (=נמר, “Tiger” in Hebrew), which eventually lead to the F-24 I for the IAF which kept its project name for service and to the USAF’s F-24A “Tigershark”.

 

The F-24, as the NLF, was based on the F-20 airframe, but outwardly showed only little family heritage, onle the forward fuselage around the cockpit reminds of the original F-5 design . Many aerodynamic details, e. g. the air intakes and air ducts, were taken over from the X-29, though, as the experimental aircraft and its components had been developed for extreme maneuvers and extra high agility. Nevertheless, the X-29's forward-swept wing was considered to be too exotic and fragile for a true service aircraft, but the F-24 was to feature an Active Aeroelastic Wing (AAW) system.

 

AAW Technology integrates wing aerodynamics, controls, and structure to harness and control wing aeroelastic twist at high speeds and dynamic pressures. By using multiple leading and trailing edge controls like "aerodynamic tabs", subtle amounts of aeroelastic twist can be controlled to provide large amounts of wing control power, while minimizing maneuver air loads at high wing strain conditions or aerodynamic drag at low wing strain conditions. This system was initially tested on the X-29 and later on the X-53 research aircraft, a modified F-18, until 2006.

 

Both USAF and IAF versions feature this state-of-the-art aerodynamic technology, but it is uncertain if other customers will receive it. While details concerning the F-24's system have not been published yet, it is assumed that its AAW is so effective that canard foreplanes could be omitted without sacrificing lift and maneuverability, and that drag is effectively minimized as the wing profile can be adjusted according to the aircraft’s speed, altitude, payload and mission – much like a VG wing, but without its clumsy and heavy swiveling mechanism which has to bear high g forces. As a result, the F-24 is, compared to the F-20, which could carry an external payload of about 3.5 tons, rumored to be able to carry up to 5 tons of ordnance.

 

The delta wing shape proved to be a perfect choice for the required surface and flap actuators inside of the wings, and it would also offer a very good compromise between lift and drag for a wide range of performance. Anyway, there was one price to pay: in order to keep the wing profile thin and simple, the F-24’s landing gear retracts into the lower fuselage, leaving the aircraft with a relatively narrow track.

 

Another major design factor for the outstanding performance of this rather small aircraft was weight reduction and structural integrity – combined with simplicity, ruggedness and a modular construction which would allow later upgrades. Instead of “going big” and expensive, the new F-24 was to create its performance through dedicated loss of weight, which was in some part also a compensation for the AAW system in the wings and its periphery.

 

Weight was saved wherever possible, e .g. a newly developed, lightweight M199A1 gatling gun. This 20mm cannon is a three-barreled, heavily modified version of the already “stripped” M61A2 gun in the USAF’s current F-18E and F-22. One of the novel features is a pneumatic drive instead of the traditional electric mechanism, what not only saves weight but also improves trigger response. The new gun weighs only a mere 65kg (the six-barreled M61A2 weighs 92kg, the original M61A1 112 kg), but still reaches a burst rate of fire of 1.800 RPM (about 800 RPM under cyclic fire, standard practice is to fire the cannon in 30 to 50-round bursts, though) and a muzzle velocity of 1.050 metres per second (3,450 ft/s) with a PGU-28/B round.

 

While the F-16 was and is still made from 80% aluminum alloys and only from 3% composites, the F-24 makes major use of carbon fiber and other lightweight materials, which make up about 40% of the aircraft’s structure, plus an increased share of Titanium and Magnesium alloys. As a consequence and through many other weight-saving measures like keeping stealth capabilities to a minimum (even though RAM was deliberately used and many details designed to have a natural low radar signature, resulting in modest radar cross-section (RCS) reductions), a single, relatively small engine, a fuel-efficient F404-GE-402 turbofan, is enough to make the F-24 a fast and very agile aircraft, coupled with a good range. The F-24’s thrust/weight ratio is considerably higher than 1, and later versions with a vectored thrust nozzle (see below) will take this level of agility even further – with the pilot becoming the limiting factor for the aircraft’s performance.

 

USAF and IAF F-24s are outfitted with Northrop Grumman's AN/APG-80 Active Electronically Scanned Array (AESA) radar, also used in the F-16 Block 60 aircraft. Other customers might only receive the AN/APG-68, making the F-24 comparable to the F-16C/D.

 

The first prototype, the YF-24, flew on 8th of March 2008, followed by two more aircraft plus a static airframe until summer 2010. In early 2011 the USAF placed an initial order of 101 aircraft (probably also to stir export sales – the earlier lightweight fighters from Northrop suffered from the fact that the manufacturer’s country would not use the aircraft in its own forces). These initial aircraft will replace older F-16 in the interceptor role, or free them for fighter bomber tasks. The USN and USMC also showed interest in the aircraft for their aggressor squadrons, for dissimilar air combat training. A two-seater, called the F-24B, is supposed to follow soon, too, and a later version for 2020 onwards, tentatively designated F-24C, is to feature an even stronger F404 engine and a 3D vectoring nozzle.

 

Israel is going to produce its own version domestically from late 2014 on, which will exclusively be used by the IAF. These aircraft will be outfitted with different avionics, built by Elta in Israel, and cater to national requirements which focus more on multi-purpose service, while the USAF focusses with its F-24A on aerial combat and interception tasks.

 

International interest for the F-24A is already there: in late 2013 Grumman stated that initial talks have been made with various countries, and potential export candidates from 2015 on are Taiwan, Singapore, Thailand, Finland, Norway, Australia and Japan.

  

General F-24A characteristics:

Crew: 1 pilot

Length: 47 ft 4 in (14.4 m)

Wingspan: 27 ft 11.9 in / 8.53 m; with wingtip missiles (26 ft 8 in/ 8.13 m; without wingtip missiles)

Height: 13 ft 10 in (4.20 m)

Wing area: 36.55 m² (392 ft²)

Empty weight: 13.150 lb (5.090 kg)

Loaded weight: 15.480 lb (6.830 kg)

Max. take-off weight: 27.530 lb (12.500 kg)

 

Powerplant

1× General Electric F404-GE-402 turbofan with a dry thrust of 11,000 lbf (48.9 kN) and 17,750 lbf (79.2 kN) with afterburner

 

Performance

Maximum speed: Mach 2+

Combat radius: 300 nmi (345 mi, 556 km); for hi-lo-hi mission with 2 × 330 US gal (1,250 L) drop tanks

Ferry range: 1,490 nmi (1715 mi, 2759 km); with 3 × 330 US gal (1,250 L) drop tanks

Service ceiling: 55,000 ft (16,800 m)

Rate of climb: 52,800 ft/min (255 m/s)

Wing loading: 70.0 lb/ft² (342 kg/m²)

Thrust/weight: 1.09 (1.35 with loaded weight & 50% fuel)

 

Armament

1× 20 mm (0.787 in) M199A1 3-barreled Gatling cannon in the lower fuselage with 400 RPG

Eleven external hardpoints (two wingtip tails, six underwing hardpoints, three underfuselage hardpoints) and a total capacity of 11.000 lb (4.994 kg) of missiles (incl. AIM 9 Sidewinder and AIM 120 AMRAAM), bombs, rockets, ECM pods and drop tanks for extended range.

  

The kit and its assembly:

A spontaneous project. This major kitbash was inspired by fellow user nighthunter at whatifmodelers.com, who came up with a profile of a mashed-up US fighter, created “out of boredom”. The original idea was called F-21C, and it was to be a domestic successor to the IAI Kfirs which had been used by the US as aggressor aircraft in USN and USMC service for a few years.

 

As a weird(?) coincidence I had many of the necessary ingredients for this fictional aircraft in store, even though some parts and details were later changed. This model here is an interpretation of the original design. The idea was spun further, and the available parts that finally went into the model also had some influence on design and background.

I thank nighthunter for sharing the early ideas, inviting me to take the design to the hardware stage (sort of…) and adapting my feedback into new design sketches, too, which, in return, inspired the model building process.

 

Well, what went into this thing? To cook up a F-24 à la Dizzyfugu you just need (all in 1:72):

● Fuselage from a Hasegawa X-29, including the cockpit and the landing gear

● Fin and nose cone from an Italeri F-16A

● Inner wings from a (vintage) Hasegawa MiG-21F

● Outer wings from a F-4 (probably a J, Hasegawa or Fujimi)

 

The wing construction deviates from nighthunter’s original idea. The favorite ingredients would have been F-16XL or simple Mirage III wings, but I found the composite wing to be more attractive and “different”. The big F-16XL wings, despite their benefit of a unique shape, might also have created scale/size problems with a F-20 style fuselage? So I built hybrid wings: The MiG-21 landing gear wells were filled with putty and the F-4 outer wings simply glued onto the MiG inner wing sections, which were simply cut down in span. It sounds like an unlikely combo, but these parts fit together almost perfectly! In order to hide the F-4 origins I modified them to carry wingtip launch rails, though, which were also part of nighthunter’s original design.

 

The AAW technology detail mentioned in the background came in handy as it explains the complicated wing shape and the fact that the landing gear retracts into the fuselage, not into the wings, which would have been more plausible… Anyway, there’s still room for a simpler export version, with Mirage III or Kfir C.2/7 wings, and maybe canards?

 

Using the X-29 as basis also made fitting the new wings onto the area-ruled fuselage pretty easy, as I could use the wing root parts from the X-29 to bridge the gap. The original, forward-swept wings were just cut away, and the remains used as consoles for the new hybrid delta wings. Took some SERIOUS putty work, but the result is IMHO fine.

 

The bigger/square X-29 air intakes were taken over, and they change the look of the aircraft, making it look less F-5-ish than a true F-20 fuselage. For the same reason I kept the large fairing at the fin base, combining it with a bigger F-16 tail, though, as a counter-balance to the new, bigger wings. Again, the F-16 fin was/is part of nighthunter’s idea, so the model stays true to the original concept.

 

For the same reason I omitted the original X-29 nose, which is rather pointy, sports vanes and a large sensor boom. The F-16 nose was a plausible choice, as the AN/APG-80 is also carried by late Fighting Falcons, and its shape fits well, too.

 

All around the hull, some small details like radar warning sensors, pitots and air scoops were added. Not really necessary, but such thing add IMHO to the overall impression of such a fictional aircraft beyond the prototype stage.

 

Cockpit and landing gear were taken OOB, I just added a pilot figure and slightly modified the seat.

 

The ordnance was puzzled together from the scrap box, the AIM-9Ls come from the same F-4 kit which donated its outer wings, the AIM-120s come from an Italeri NATO weapons kit. The drop tanks belong to an F-16.

  

Painting and markings:

At first I considered an F-24I in IAF markings, or even a Japanese aircraft, but then reverted to one of nighthunter’s initial, simple ideas: an USAF aircraft in the “Hill II” paint scheme (F-16 style), made up from three shades of gray (FS 36118, 36270 and 36375) with low-viz markings and stencils. Dutch/Turkish NF-5A/Bs in the “Hill II” scheme were used as design benchmarks, too. It’s a simple livery, but on this delta wing aircraft it looks pretty interesting. I used enamels, what I had at hand: Humbrol 127 and 126, and Modelmaster's 1723.

 

A light black ink wash was applied, in order to em,phasize the engraved panel lines, in contrast to that, panels were manually highlighted through dry-brushed, lighter shades of gray (Humbrol 27, 166 and 167).

 

“Hill II” also adds to a generic, realistic touch for this whif. Doing an exotic air force thing is rather easy, but creating a convincing whif for a huge military machinery like the USAF’s takes more subtlety, I think.

 

The cockpit was painted in medium Gray (Dark Gull Grey, FS 36231, Humbrol 140), as well as the radome. The landing gear and the air intakes were painted white. The radome was painted with Revell 47 and dry-brushed with Humbrol 140.

 

Decals were puzzled together from various USAF aircraft, including sheets from an Airfix F-117, an Italeri F-15E and even an Academy OV-10D.

  

Tadah: a hardware tribute to an idea, born from boredom - and the aircraft does not look even bad at all? What I wanted to achieve was to make the F-24 neither look like a F-20, nor a Saab Gripen clone, as the latter comes close in overall shape, size and design.

ATR 72-600 test-bed and demonstrator visiting Guernsey. It performed several circuits in low visibility conditions before returning to Toulouse.

 

Airfield: Guernsey Airport (GCI/EGJB)

This was the 25th 747 built, delivered to Pan Am in March 1970. It was sold to GE in March 1992 and used as an engine testbed until 1/25/2017 when it was finally retired at 19,251 cycles and 90,000 hours.

Visit my Facebook page!

 

- - -

 

The C111 was a series of experimental automobiles produced by Mercedes-Benz in the 1960s and 1970s. The company was experimenting with new engine technologies, including Wankel engines, Diesel engines, and turbochargers, and used the basic C111 platform as a testbed. Other experimental features included gullwing doors and a luxurious interior with leather trim and air conditioning.

 

(Wikipedia)

Engineers at Ball Aerospace test the Wavefront Sensing and Control testbed to ensure that the 18 primary mirror segments and one secondary mirror on JWST work as one. The test is performed on a 1/6 scale model of the JWST mirrors.

 

Credit: NASA/Northrop Grumman/Ball Aerospace

 

To read more about the James Webb Space Telescope go to: www.nasa.gov/topics/technology/features/partnerships.html

 

NASA Goddard Space Flight Center is home to the nation's largest organization of combined scientists, engineers and technologists that build spacecraft, instruments and new technology to study the Earth, the sun, our solar system, and the universe.

F-OLGA Fokker F100 Palair Macedonia 2x RR Tay 650-15 01. Oct 1993

PH-TAB Fokker F100 Fokker Services 2x RR Tay 650-15 05. Jul 1996

PT-MRZ Fokker F100 TAM Linhas Aéreas 2x RR Tay 650-15 07. Dec 1996

EI-DFB Fokker F100 EUjet 2x RR Tay 650-15 22. Apr 2004

F-GPXL Fokker F100 Régional 2x RR Tay 650-15 20. Feb 2006

F-GPXL Fokker F100 Centre D'essais En Vol 2x RR Tay 650-15 Testbed 01. Mar 2013

On 2 September 2005, 37109 tows 960201 (formed from class 310 vehicles) from Ramsgate to Ilford. This unit was used as a testbed for the class 395 traction equipment.

Honeywell Testbed B757-200 N757HW

After years of hiding away the prototype Wright Streetdeck is now out and about in service. Arriva London DW411 started life as a normal VDL DB300 but was fire damaged and then converted & lengthened to be the Streetdeck "testbed" prototype. The bus has a Mercedes engine. Here it is leaving Edmonton Green bus station on the 349 to Enfield bus garage.

The aircraft received a new radome to house the Combat Talon avionics package, which included a Terrain Following/Terrain Avoidance radar, a Doppler radar/GPS tie-in to the aircraft’s inertial navigation system, and a defensive countermeasures suite. Many of these features would be carried over to the MC-130H Combat Talon II.

 

In this image, the XFC-130H (serial number: 74-1683) takes off for flight testing. XFC-130H was the aircraft’vs official designation during development and testing. After the test aircraft failed (see the next image for details), the remaining airframes were stripped of their rocket modifications. Aircraft 74-2065 returned to airlift duties; however, aircraft 74-1686 retained its Operation Credible Sport STOL modifications and was sent to Robins AFB in Georgia. In July 1981, it was designated the YMC-130H and became the testbed for the MC-130H Combat Talon II’s development under the Credible Sport II project. Phase I was conducted between 24 August and 11 November 1981, testing minor modifications to improve aerodynamics, STOL performance, handling characteristics, and avionics.

 

Phase II testing began on 15 June 1982 and continued through October 1982. It was determined that the final configuration resulted in significant improvements in design, avionics, and equipment and that the Combat Talon II design was ready for production. The 1st Special Operations Wing attempted to transfer the testbed to operational duty as an interim Combat Talon II until production models became available, but Tactical Airlift Command disagreed. The cost of returning the YMC-130H to stock airlift configuration was more than its value, and it never flew again. In 1988, the aircraft was placed on display at the Museum of Aviation at Robins AFB in Georgia, and in 2018, it was moved to the Empire State Aerosciences Museum in Glenville, New York.

NASA Dryden's F-15B Research Test bed roared aloft from the Edwards AFB main runway for a Supersonic Boundary Layer Transition - Phase II, or SBLT-II, research flight. The experiment, being conducted in partnership with Aerion Corporation, involved flying a small Aerion-designed test airfoil attached underneath the F-15B to investigate the extent and robustness of natural laminar flow over the test section at supersonic speeds.

  

NASA Dryden Flight Research Center’s F-15B Research Testbed aircraft has been busy this spring, flying an experimental test fixture in partnership with Aerion Corporation of Reno, Nevada.

 

Called the Supersonic Boundary Layer Transition, Phase II, or SBLT-II, the experiment consists of flying a small test airfoil, or wing section, attached underneath the F-15B. This allows NASA and Aerion engineers to continue investigating the extent and robustness of natural laminar flow over the test section at supersonic speeds.

 

Conducting the experiment in actual supersonic flight conditions with the F-15B enables engineers to capture data in a real-world flight environment, allowing for more precise refining of supersonic natural laminar flow airfoil design.

 

“The objective of the flight series is to investigate the extent and robustness of smooth, or laminar, airflow over the specially-designed test airfoil,” said Brett Pauer, NASA Dryden’s deputy High Speed Project manager. “Then, researchers will work to better understand when imperfections in the airfoil’s surface cause the air to transition from laminar to rough, turbulent flow. The greater the extent of laminar airflow over a wing, the less aerodynamic drag there is, which reduces fuel consumption,” Pauer said.

 

It is believed that significant laminar flow has never been achieved on any production supersonic aircraft before, so this research and the data being collected from the SBLT-II test fixture may help provide some of the data that might enable the design of supersonic aircraft in the future that have wings that produce laminar flow at supersonic cruise conditions.

 

One of the goals of NASA’s High Speed Project, which utilizes the F-15B and other high performance jets, is reducing the fuel consumption and increasing efficiency of future supersonic aircraft.

 

Project flights of the SBLT-II experiment began on the F-15B earlier this year. So far, four data-gathering flights have been flown, with six more planned.

Hams Travel Ltd., Flimwell:

 

Dennis Enviro300 SFD113 (12.0m)

N45F - 12/2007

 

Originally built in 2000 as part of the testbed for what would become the TransBus Enviro300, launched in 2003. Registered as a 57-plate once the bus was purchased by the current owners, Hams Travel of Flimwell. This unique E300 will be leaving the fleet in the next couple of weeks, having been sold in part exchange for a new Volvo coach.

  

Benenden Coachworks Yard

 

Sunday 21st May 2017

Zhukovsky, 31 August 1993.

 

An old model Su-15 Flagon that was (still?) used as a testbed.

1960s Lifting Body Testbed, NASA Dreyden

Grumman F-14 Super Tomcat 157986 on display aboard the USS Intrepid CV-11 The Intrepid Sea, Air and Space Museum located in Manhattan New York City New York U.S.A

 

7th prototype used as engine testbed, later used as F-14B-30GR prototype and then modified as F-14A(+) prototype.

 

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This photograph and all those within my photostream are protected by copyright. The photos may not be reproduced, copied, transmitted or manipulated without my written permission.

 

After shooting in Phoenix, Arizona for 2 days it was time to move on to Sin City. My dad and I had hoped to see this aircraft fly but during our time there it didn't move an inch. Waiting for the first flight of the day I suddenly saw this aircraft leaving it's parking position across the runway. Hoping it would take the north runway I got my camera out of the bag and getting ready to shoot it. Sure enough, it departed off the north runway so I got this incredible opportunity to shoot it. I got off around 10 frames which got earned me the attention of an entire gate area full of people, but I didn't care less, I had the shot!

 

As it turns out this was the last ever flight of this very rare Boeing 720. Only 152 were built and this was one of the last 3 to fly, the other 2 operated by Pratt & Whitney. A very expensive corrosion treatment signalled the end for this aircraft and it was scrapped on June 21st and 22nd 2008.

Here's my latest mini-project, a electro-optical rangefinder. This is a proof of concept. Optically, it is similar to the Leica II/III rangefinder. The right angle prism, however, is moved by a servo and a cam. Hoping to implement this into a camera soon.

 

Type: Optical triangulation rangefinder

Magnification: 1.33x Galilean

Baselength: 50mm

Effective Baselength: 66.5mm

 

c/n 17608/122. At Mojave. Used as an engine testbed. Leased from International Air Leases. In PIA colours after lease to them. New to Pan Am as N730PA in 1960. Converted to a freighter in 1970 and to Donaldson International Airways as G-AYXR in 1971. To British Midland Airways in 1975 and leased to a number of airlines. To International Air Leases as N37681 in 1980. To General Electric in 1983 and used as an engine testbed. Reregistered as N707GE in 1990. Scrapped at Mojave in 2003.

Grumman G-1159A Gulfstream III

Calspan

Shannon 11/7/2024

Airborne Testbed

Portland Harbour, Dorset, UK

 

On the left is SD Victoria, an ocean going tug / support vessel operated by SERCO Marine in support of Royal Naval Operations.

 

On the right is RFA Proteus (K60) a ship of the Royal Fleet Auxiliary within His Majesty's Naval Service of the United Kingdom. Its roles being a platform for Remotely Operated Underwater Vehicles (ROUVs and a testbed for new specialist capabilities, required for monitoring waters important to UK interests. Acquired in 2023, the ship entered drydock at Cammell Laird for modification into a Multi-Role Ocean Surveillance Ship (MROSS). She formally entered service in October 2023.

   

N789ZB Boeing 787-9 Dreamliner Boeing Testbed 2x GEnx-1B 23. Apr 2013

 

JA861J Boeing 787-9 Dreamliner Japan Airlines C44W35Y116 2x GEnx-1B 09. Jun 2015 Ferried PAE-NRT 10 - 06/11/2015 on delivery

  

Southern California Logistics Airport, Victorville, CA

Jan. 28, 2016

 

Both GE and Boeing have test facilities located at the Victorville facilities.

 

This GE owned 747 is an engine testbed, and has been testing the new Leap 1B engine for the Boeing 737Max series. This engine would be the No. 2 engine on the left side. The other 3 engines are P&W JT-9Ds. GE also owns a 747-400, but that wasn't visible at the time.

 

This aircraft has apparently been repainted recently, to match their 747-400 livery.

GEAE partner logos on N747GE

Boeing 747-267B

Some background:

The VF-1 was developed by Stonewell/Bellcom/Shinnakasu for the U.N. Spacy by using alien Overtechnology obtained from the SDF-1 Macross alien spaceship. Its production was preceded by an aerodynamic proving version of its airframe, the VF-X. Unlike all later VF vehicles, the VF-X (sometimes referred to as VF-X1) was strictly a conventional/non-transformable jet aircraft, even though it incorporated many structural components and several key technologies that were vital for the transformable VF-1’s successful development that ran in parallel. Therefore, the VF-X was never intended as an air superiority fighter, but rather a flight-capable analogue test bed and proof of concept for the VF-1’s basic layout and major components. In this role, however, the VF-X made vital contributions to systems’ development that were later incorporated into the VF-1’s serial production and sped the program up considerably.

 

VF-X production started in early 2006, with four airframes built. The flight tests began in February 2007. The first prototype (“01”) was piloted and evaluated by ace pilot Roy Fokker, in order to explore the aircraft’s flight envelope, general handling and for external stores carriage tests. The three other VF-Xs successively joined the test program, each with a different focus. “02” was primarily tasked with the flight control and pilot interface program, “03” was allocated to the engine, vectoring thrust and steering systems development, and “04” was primarily involved in structural and fatigue tests.

 

In November 2007, the successful VF-X tests and the flights of the VF-X-1 (the first fully transformable VF-1 prototype, which had been under construction in parallel to the VF-X program) led to formal adoption of the “Valkyrie” variable fighter by the United Nations Government.

The space-capable VF-1's combat debut was on February 7, 2009, during the Battle of South Ataria Island - the first battle of Space War I - and remained the mainstay fighter of the U.N. Spacy for the entire conflict.

 

Introduced in 2008, the VF-1 proved to be an extremely capable craft, successfully combating a variety of Zentraedi mecha, even in most sorties which saw UN Spacy forces significantly outnumbered. The versatility of the Valkyrie design enabled the variable fighter to act as both large-scale infantry and as air/space superiority fighter. The signature skills of U.N. Spacy ace pilot Maximilian Jenius exemplified the effectiveness of the variable systems as he near-constantly transformed the Valkyrie in battle to seize advantages of each mode as combat conditions changed from moment to moment.

 

The basic VF-1 was deployed in four sub-variants (designated A, D, J, and S) and its success was increased by continued development of various enhancements. These included the GBP-1S "Armored Valkyrie” external armor and infantry weapons pack, so-called FAST Packs for "Super Valkyries” for orbital use, and the additional RÖ-X2 heavy cannon pack weapon system for the VF-1S “Strike Valkyrie” with additional firepower.

 

After the end of Space War I, the VF-1 continued to be manufactured both in the Sol system and throughout the UNG space colonies. Although the VF-1 would eventually be replaced as the primary Variable Fighter of the U.N. Spacy by the more capable, but also much bigger, VF-4 Lightning III in 2020, a long service record and continued production after the war proved the lasting worth of the design.

 

The VF-1 was without doubt the most recognizable variable fighter of Space War I and was seen as a vibrant symbol of the U.N. Spacy even into the first year of the New Era 0001 in 2013. At the end of 2015 the final rollout of the VF-1 was celebrated at a special ceremony, commemorating this most famous of variable fighters. The VF-1 Valkryie was built from 2006 to 2013 with a total production of 5,459 VF-1 variable fighters with several variants (VF-1A = 5,093, VF-1D = 85, VF-1J = 49, VF-1S = 30, VF-1G = 12, VE-1 = 122, VT-1 = 68), and several upgrade programs were introduced.

The fighter remained active in many second line units and continued to show its worthiness years later, e. g. through Milia Jenius who would use her old VF-1 fighter in defense of the colonization fleet - 35 years after the type's service introduction.

  

General characteristics:

Accommodation: One pilot in a Marty & Beck Mk-7 zero/zero ejection seat

Length 14.23 meters

Wingspan 14.78 meters (at 20° minimum sweep)

Height 3.84 meters

Empty weight: 13.25 metric tons

Standard T-O mass: 18.5 metric tons

 

Power Plant:

2x Shinnakasu Heavy Industry/P&W/Roice FF-2001 thermonuclear reaction turbine engines, output 650 MW each, rated at 11,500 kg in standard or in overboost (225.63 kN x 2)

4 x Shinnakasu Heavy Industry NBS-1 high-thrust vernier thrusters (1 x counter reverse vernier thruster nozzle mounted on the side of each leg nacelle/air intake, 1 x wing thruster roll control system on each wingtip);

 

Performance:

Top speed: Mach 2.71 at 10,000 m; Mach 3.87 at 30,000+ m

Thrust-to-weight ratio: empty 3.47; standard T-O 2.49; maximum T-O 1.24

 

Armament:

None installed, but the VF-X had 4x underwing hard points for a wide variety of ordnance, plus a ventral hardpoint for a Howard GU-11 55 mm three-barrel Gatling gun pod with 200 RPG, fired at 1,200 rds/min or other stores like test instruments

  

The model and its assembly:

Another submission to the “Prototypes” group build at whatifmodelers.com in July 2020. Being a VF-1 fan (and have built maybe twenty o these simple Arii kits), adding a VF-X was, more or less, a must – even more so because I had a suitable Valkyrie Fighter kit at hand for the conversion. As a side note, I have actually built something quite similar from a VF-1D many years ago: a fictional, non-transformable advanced trainer, without knowing about the VF-X at all.

 

Thanks to the “Macross - Perfect Memory” source book, the differences between the transformable VF-1 and its early testbed were easy to identify:

- Fixed legs with faired ducts from the intakes on (thighs)

- Ankle recesses disappeared

- Less and slightly different panel lines on the back and on the nose

- ventral head unit deleted and a respective fairing installed instead

- Levelled underside (shoulder fairings of the folded arms were cut down)

- Leg attachment points on the nose deleted

- No small, circular vernier thrusters all around the hull

- Some new/different venting grills (created mostly with 0.5mm black decal stripes)

 

Beyond the changes, the VF-1A was basically built OOB. Thankfully, the VF-X already features the later VF-1’s vectored thrust nozzles/feet, so that no changes had to be made in this respect. A pilot figure was added to the cockpit for the beauty pics, and after the flight scenes had been shot, the canopy remained open on a swing arm for static display. For the same reason, the model was built with the landing gear extended.

 

As a test aircraft, the underwing pylons and their AMM-1 ordnance were left away and the attachment points hidden with putty. I also omitted the ventral gun pod and left the aircraft clean. However, for the flight scene pictures, I implanted an adapter for a display holder made from wire.

 

In order to emphasize the test vehicle character of the VF-X, I gave the model a scratched spin recovery parachute installation between the fins, using a real world F-22 testbed as benchmark. It consists of styrene profiles, quite a delicate construction. For the same reason I gave the VF-X a long sensor boom on the nose, which changes the Valkyrie’s look, too. Finally, some small blade antennae were added to the nose and to the spine behind the cockpit.

  

Painting and markings:

To be honest, I have no idea if there was only a single VF-X prototype in the Macross universe, or more. Just one appears in the TV series in episode #33, and lack of suitable information and my personal lack of Japanese language proficiency prevents any deeper research. However, this would not keep me from inventing a personal interpretation of the canonical VF-X, especially because I do not really like the original livery from the TV series: an overall light grey with some simple black trim and “TEST” written on the (fixed) legs. Yamato did an 1:60 scale toy of the VF-X, but it was/is just a VF-1 with a ventral fairing; they added some shading to the basic grey – but this does not make the aircraft more attractive, IMHO.

 

When I looked at the original conceptual drawing of the VF-X in the “Macross - Perfect Memory” source book, however, I was immediately reminded of the F-15 prototypes from the Seventies (and this program used a total of twelve machines!). These featured originally a light grey (FS 36375?) overall base, to which bright dayglo orange markings on wings, fins and fuselage were soon added – in a very similar pattern to the VF-X. I think the VF-X livery was actually inspired by this, the time frame matches well with the production of the Macross TV series, too, and that’s what I adapted for my model.

In order to come close to the F-15 prototype livery, I gave “my” VF-X an overall basic coat of RAL 7047 “Telegrau 4”, one of German Telekom’s corporate colors and a very pale grey that can easily be mistaken for white when you do not have a contrast reference.

 

The cockpit received a medium grey finish, the ejection seat became black with brown cushions; the pilot figure is a 1:100 seated passenger from an architecture supplies, painted like an early VF-1 pilot in a white/blue suit. The jet nozzles/feet were painted with Revell 91 (Iron) and later treated with grinded graphite for a more metallic finish. The landing gear became classic white (I used Revell 301, which is a very pure tone, as contrast to the RAL 7047 on the hull), the air intake ducts and the internal sections of the VG wings were painted with dark grey (Revell 77).

 

For some diversity I took inspiration from the Yamato VF-X toy and added slightly darker (Humbrol 166, RAF Light Aircraft Grey) areas to the hull and the legs. Next, the panel lines were emphasized through a thinned black ink wash, but I did no panel post shading so that the VF-X would not look too dirty or worn.

 

Onto this basis I applied the orange dayglo markings. On the wings and fins, these were painted – they were applied with spray paint from a rattle can, involving lots of masking. The leading edges on wings and fins were created with grey decal sheet material, too. At this stage, some surface details and more fake panel lines were added with a soft pencil.

The orange cheatline under the cockpit is a personal addition; I found that some more orange had to be added to the nose for visual balance, and I eventually went for the simple, trimmed stripe (TL Modellbau material) instead of trying to apply decal sheet material around the jagged air intakes (F-15 prototype style). The black “TEST”, “VFX” and “U.N. Spacy” markings were designed at the computer and printed on clear inkjet decal paper. Even though the “real” VF-X does not feature the UNS “kite” insignia, I decided to add them to the model. These come from the OOB sheet, which also provided most (slightly yellowed) stencils.

Finally, the model was sealed with a coat of matt acrylic varnish (Italeri).

  

A rather different VF-1 project (and it is – to my astonishment – #28 in my 1:100 VF-1 Fighter mode collection!!!), with more changes to the basic model kit than one might expect at first sight. VF-X and VF-1 differ considerably from each other, despite identical outlines! However, I like the outcome, and I think that going a different route from the canonical grey/black livery paid out, the bright orange markings really make this VF-X stand out, and it looks IMHO more like a testbed than the “real” aircraft from the TV series.

Kbely, 1990. Ejectionseat testbed

This was a testbed shot for the E200MMC which was in hot pursuit, however the demonstrator didn't come out so well in Nottingham, but more than happy that this one did!!

 

773 enters Nottingham Victoria Bus Station with a Two having arrived in from Cotmanhay Farm, Ilkeston and Wollaton.

60-0377

 

Served as a testbed for B-2A avionics and laser communication.

 

4950th Test Wing

 

Edwards Air Force Base, CA USA

 

Hams Travel Ltd., Flimwell:

 

Dennis Enviro300 SFD113 (12.0m)

N45F - 12/2007

 

Originally built in 2000 as part of the testbed for what would become the TransBus Enviro300, launched in 2003. Registered as a 57-plate once the bus was purchased by the current owners, Hams Travel of Flimwell. This unique E300 will be leaving the fleet in the next couple of weeks, having been sold in part exchange for a new Volvo coach.

  

Benenden Coachworks Yard

 

Sunday 21st May 2017

Some background:

The VF-1 was developed by Stonewell/Bellcom/Shinnakasu for the U.N. Spacy by using alien Overtechnology obtained from the SDF-1 Macross alien spaceship. Its production was preceded by an aerodynamic proving version of its airframe, the VF-X. Unlike all later VF vehicles, the VF-X (sometimes referred to as VF-X1) was strictly a conventional/non-transformable jet aircraft, even though it incorporated many structural components and several key technologies that were vital for the transformable VF-1’s successful development that ran in parallel. Therefore, the VF-X was never intended as an air superiority fighter, but rather a flight-capable analogue test bed and proof of concept for the VF-1’s basic layout and major components. In this role, however, the VF-X made vital contributions to systems’ development that were later incorporated into the VF-1’s serial production and sped the program up considerably.

 

VF-X production started in early 2006, with four airframes built. The flight tests began in February 2007. The first prototype (“01”) was piloted and evaluated by ace pilot Roy Fokker, in order to explore the aircraft’s flight envelope, general handling and for external stores carriage tests. The three other VF-Xs successively joined the test program, each with a different focus. “02” was primarily tasked with the flight control and pilot interface program, “03” was allocated to the engine, vectoring thrust and steering systems development, and “04” was primarily involved in structural and fatigue tests.

 

In November 2007, the successful VF-X tests and the flights of the VF-X-1 (the first fully transformable VF-1 prototype, which had been under construction in parallel to the VF-X program) led to formal adoption of the “Valkyrie” variable fighter by the United Nations Government.

The space-capable VF-1's combat debut was on February 7, 2009, during the Battle of South Ataria Island - the first battle of Space War I - and remained the mainstay fighter of the U.N. Spacy for the entire conflict.

 

Introduced in 2008, the VF-1 proved to be an extremely capable craft, successfully combating a variety of Zentraedi mecha, even in most sorties which saw UN Spacy forces significantly outnumbered. The versatility of the Valkyrie design enabled the variable fighter to act as both large-scale infantry and as air/space superiority fighter. The signature skills of U.N. Spacy ace pilot Maximilian Jenius exemplified the effectiveness of the variable systems as he near-constantly transformed the Valkyrie in battle to seize advantages of each mode as combat conditions changed from moment to moment.

 

The basic VF-1 was deployed in four sub-variants (designated A, D, J, and S) and its success was increased by continued development of various enhancements. These included the GBP-1S "Armored Valkyrie” external armor and infantry weapons pack, so-called FAST Packs for "Super Valkyries” for orbital use, and the additional RÖ-X2 heavy cannon pack weapon system for the VF-1S “Strike Valkyrie” with additional firepower.

 

After the end of Space War I, the VF-1 continued to be manufactured both in the Sol system and throughout the UNG space colonies. Although the VF-1 would eventually be replaced as the primary Variable Fighter of the U.N. Spacy by the more capable, but also much bigger, VF-4 Lightning III in 2020, a long service record and continued production after the war proved the lasting worth of the design.

 

The VF-1 was without doubt the most recognizable variable fighter of Space War I and was seen as a vibrant symbol of the U.N. Spacy even into the first year of the New Era 0001 in 2013. At the end of 2015 the final rollout of the VF-1 was celebrated at a special ceremony, commemorating this most famous of variable fighters. The VF-1 Valkryie was built from 2006 to 2013 with a total production of 5,459 VF-1 variable fighters with several variants (VF-1A = 5,093, VF-1D = 85, VF-1J = 49, VF-1S = 30, VF-1G = 12, VE-1 = 122, VT-1 = 68), and several upgrade programs were introduced.

The fighter remained active in many second line units and continued to show its worthiness years later, e. g. through Milia Jenius who would use her old VF-1 fighter in defense of the colonization fleet - 35 years after the type's service introduction.

  

General characteristics:

Accommodation: One pilot in a Marty & Beck Mk-7 zero/zero ejection seat

Length 14.23 meters

Wingspan 14.78 meters (at 20° minimum sweep)

Height 3.84 meters

Empty weight: 13.25 metric tons

Standard T-O mass: 18.5 metric tons

 

Power Plant:

2x Shinnakasu Heavy Industry/P&W/Roice FF-2001 thermonuclear reaction turbine engines, output 650 MW each, rated at 11,500 kg in standard or in overboost (225.63 kN x 2)

4 x Shinnakasu Heavy Industry NBS-1 high-thrust vernier thrusters (1 x counter reverse vernier thruster nozzle mounted on the side of each leg nacelle/air intake, 1 x wing thruster roll control system on each wingtip);

 

Performance:

Top speed: Mach 2.71 at 10,000 m; Mach 3.87 at 30,000+ m

Thrust-to-weight ratio: empty 3.47; standard T-O 2.49; maximum T-O 1.24

 

Armament:

None installed, but the VF-X had 4x underwing hard points for a wide variety of ordnance, plus a ventral hardpoint for a Howard GU-11 55 mm three-barrel Gatling gun pod with 200 RPG, fired at 1,200 rds/min or other stores like test instruments

  

The model and its assembly:

Another submission to the “Prototypes” group build at whatifmodelers.com in July 2020. Being a VF-1 fan (and have built maybe twenty o these simple Arii kits), adding a VF-X was, more or less, a must – even more so because I had a suitable Valkyrie Fighter kit at hand for the conversion. As a side note, I have actually built something quite similar from a VF-1D many years ago: a fictional, non-transformable advanced trainer, without knowing about the VF-X at all.

 

Thanks to the “Macross - Perfect Memory” source book, the differences between the transformable VF-1 and its early testbed were easy to identify:

- Fixed legs with faired ducts from the intakes on (thighs)

- Ankle recesses disappeared

- Less and slightly different panel lines on the back and on the nose

- ventral head unit deleted and a respective fairing installed instead

- Levelled underside (shoulder fairings of the folded arms were cut down)

- Leg attachment points on the nose deleted

- No small, circular vernier thrusters all around the hull

- Some new/different venting grills (created mostly with 0.5mm black decal stripes)

 

Beyond the changes, the VF-1A was basically built OOB. Thankfully, the VF-X already features the later VF-1’s vectored thrust nozzles/feet, so that no changes had to be made in this respect. A pilot figure was added to the cockpit for the beauty pics, and after the flight scenes had been shot, the canopy remained open on a swing arm for static display. For the same reason, the model was built with the landing gear extended.

 

As a test aircraft, the underwing pylons and their AMM-1 ordnance were left away and the attachment points hidden with putty. I also omitted the ventral gun pod and left the aircraft clean. However, for the flight scene pictures, I implanted an adapter for a display holder made from wire.

 

In order to emphasize the test vehicle character of the VF-X, I gave the model a scratched spin recovery parachute installation between the fins, using a real world F-22 testbed as benchmark. It consists of styrene profiles, quite a delicate construction. For the same reason I gave the VF-X a long sensor boom on the nose, which changes the Valkyrie’s look, too. Finally, some small blade antennae were added to the nose and to the spine behind the cockpit.

  

Painting and markings:

To be honest, I have no idea if there was only a single VF-X prototype in the Macross universe, or more. Just one appears in the TV series in episode #33, and lack of suitable information and my personal lack of Japanese language proficiency prevents any deeper research. However, this would not keep me from inventing a personal interpretation of the canonical VF-X, especially because I do not really like the original livery from the TV series: an overall light grey with some simple black trim and “TEST” written on the (fixed) legs. Yamato did an 1:60 scale toy of the VF-X, but it was/is just a VF-1 with a ventral fairing; they added some shading to the basic grey – but this does not make the aircraft more attractive, IMHO.

 

When I looked at the original conceptual drawing of the VF-X in the “Macross - Perfect Memory” source book, however, I was immediately reminded of the F-15 prototypes from the Seventies (and this program used a total of twelve machines!). These featured originally a light grey (FS 36375?) overall base, to which bright dayglo orange markings on wings, fins and fuselage were soon added – in a very similar pattern to the VF-X. I think the VF-X livery was actually inspired by this, the time frame matches well with the production of the Macross TV series, too, and that’s what I adapted for my model.

In order to come close to the F-15 prototype livery, I gave “my” VF-X an overall basic coat of RAL 7047 “Telegrau 4”, one of German Telekom’s corporate colors and a very pale grey that can easily be mistaken for white when you do not have a contrast reference.

 

The cockpit received a medium grey finish, the ejection seat became black with brown cushions; the pilot figure is a 1:100 seated passenger from an architecture supplies, painted like an early VF-1 pilot in a white/blue suit. The jet nozzles/feet were painted with Revell 91 (Iron) and later treated with grinded graphite for a more metallic finish. The landing gear became classic white (I used Revell 301, which is a very pure tone, as contrast to the RAL 7047 on the hull), the air intake ducts and the internal sections of the VG wings were painted with dark grey (Revell 77).

 

For some diversity I took inspiration from the Yamato VF-X toy and added slightly darker (Humbrol 166, RAF Light Aircraft Grey) areas to the hull and the legs. Next, the panel lines were emphasized through a thinned black ink wash, but I did no panel post shading so that the VF-X would not look too dirty or worn.

 

Onto this basis I applied the orange dayglo markings. On the wings and fins, these were painted – they were applied with spray paint from a rattle can, involving lots of masking. The leading edges on wings and fins were created with grey decal sheet material, too. At this stage, some surface details and more fake panel lines were added with a soft pencil.

The orange cheatline under the cockpit is a personal addition; I found that some more orange had to be added to the nose for visual balance, and I eventually went for the simple, trimmed stripe (TL Modellbau material) instead of trying to apply decal sheet material around the jagged air intakes (F-15 prototype style). The black “TEST”, “VFX” and “U.N. Spacy” markings were designed at the computer and printed on clear inkjet decal paper. Even though the “real” VF-X does not feature the UNS “kite” insignia, I decided to add them to the model. These come from the OOB sheet, which also provided most (slightly yellowed) stencils.

Finally, the model was sealed with a coat of matt acrylic varnish (Italeri).

  

A rather different VF-1 project (and it is – to my astonishment – #28 in my 1:100 VF-1 Fighter mode collection!!!), with more changes to the basic model kit than one might expect at first sight. VF-X and VF-1 differ considerably from each other, despite identical outlines! However, I like the outcome, and I think that going a different route from the canonical grey/black livery paid out, the bright orange markings really make this VF-X stand out, and it looks IMHO more like a testbed than the “real” aircraft from the TV series.

See this locomotive in the video here: www.youtube.com/watch?v=N3oxDV2lg1s

 

Having just worked the "Cumbrian Mountaineer" over Shap, preserved London, Midland & Scottish Railway Princess Royal 6201 'Princess Elizabeth' readies itself for departure with empty stock bound for the adjacent sidings on what was her last railtour before overhaul.

 

The Princess Royal class were a set of 13 4-6-2 Pacific locomotives designed by William Stanier and built at Crewe Works between 1933 and 1935 to be the prime motive power on the West Coast Mainline between London Euston, Birmingham, Manchester, Liverpool and Glasgow, including the famous Royal Scot premier express service. At first, two prototypical locomotives were built in 1933, followed by 11 production locomotives in 1935. These were later complimented by a fleet of 38 Coronation Pacific locomotives built between 1937 and 1948, which later went on to be arguably the most power steam locomotives ever built for the British Railway network.

 

One of the original prototypes however was retained for use as a testbed for a new Turbine Locomotive project to help improve the efficiency of the engines, later being unofficially dubbed 'Turbomotive'. The engine was fitted with turbines instead of cylinders, with the forward turbine containing 18 rows of blading, resulting in an output of 2,400hp, corresponding to running at 62 mph (100 km/h). The turbine was designed to operate into a maximum back-pressure of 2 psi, allowing a conventional double blast-pipe to provide the boiler draught, and eliminating draught fans, which always seemed to give a disproportionate amount of trouble.

 

The reverse turbine had 4 rows of blades. It was engaged by a dog clutch, activated when the reverser lever being set to "0". This was originally steam-operated by a small piston and cylinder. This locomotive was later rebuilt as a conventional classmate in 1952, using new mainframes and a spare set of cylinders from one of the Coronation Pacifics, and was numbered 46202, later to be named 'Princess Anne'.

 

6201, LMS lot number 99, was built at Crewe for the sum of £11,675 (£685,000 today) and named Princess Elizabeth, after the then Duke of York’s eldest daughter, currently our Queen Elizabeth II, leaving the works on 3rd November 1933.

 

Throughout the years the Princess Royal's continued to ply their trade on the West Coast services, but the years of World War II took their toll on the fleet. The beautiful Crimson Lake was replaced by Wartime Black, and the prestige manner that these locomotives had been accustomed to was stripped away as the railways were rationalised as part of the war effort. Work hours increased, and maintenance turns reduced, meaning these engines were being forced to the very limit of their design to keep Britain moving.

 

With the end of the war in 1945 the workload began to decrease, but the railways had paid the price. The beauty and lavish luxury of the pre-war companies had been stripped and would never return, with all of Britain's main railway companies now almost bankrupt and working a fleet of very tired engines on a poorly maintained railway network. In 1948 the Labour Government nationalised these companies to create British Railways, hoping to modernise the network and rebuild the overworked system.

 

The Princess Royals and their more powerful sisters the Coronation Pacifics continued to work hard as the implementation of diesels gathered pace. Early diesels however were underpowered and suffered heavily from reliability issues, meaning on many occasions the steam locomotives that they intended to replace actually came to their rescue!

 

It was not all plain sailing though for the Princess Royals in the 1950's, as this decade was littered with many fatal accidents. On 21 September 1951, locomotive No.46207 Princess Arthur of Connaught was hauling an express passenger train that was derailed at Weedon, Northamptonshire due to a defective front bogie on the locomotive, resulting in the deaths of 15 people and the injury of 35.

 

This was followed a year later by what would turn out to be the worst rail accident in the whole of British history. On 8 October 1952, an express passenger train hauled by Coronation Class, 46242 'City of Glasgow' overran signals on a train from Perth to London Euston, striking the rear of a stopped Tring to Euston commuter train at Harrow and Wealdstone station in North London. The ensuing wreckage was then struck by a northbound Liverpool express, hauled by Jubilee Class 45637 'Windward Islands', and recently rebuilt ex-Turbomotive Princess Royal 46202 'Princess Anne', which had only entered service two months earlier. In the chaos that followed, a total of 112 people were killed and 340 were injured, with 46202 obliterated in the accident, the first and only member of the class to be lost in an accident.

 

The late 50's however began to see the end of these engines as good, reliable diesels began to be introduced to replace them, followed closely by electric traction on the West Coast Mainline out of Euston. In 1961 the first members of the class were withdrawn from service, including 6201, which was placed in store in March 1961, but returned to service in May of that year due to poor diesel reliability.

 

As more diesels were delivered, in October of the same year 6201 was again placed into storage at Carlisle Kingmoor. However, again in January 1962 6201 was returned to traffic to cover for diesel failures and continued to work until September 1962 where it was once again placed into storage. It was subsequently withdrawn by BR in October 1962 and purchased by Roger Bell. The last of the locomotives to be withdrawn was class premier and original prototype number 62000 'The Princess Royal', which was withdrawn in November 1962 and subsequently scrapped. In all, only two locomotives were preserved, number 6203 'Princess Margaret Rose' and 6201 'Princess Elizabeth'.

 

46201 was bought by the then Princess Elizabeth Locomotive Society straight from BR service when withdrawn in 1962. Initially kept at the Dowty Railway Preservation Society's premises at Ashchurch in Gloucestershire, and then subsequently at the Bulmers Railway Centre in Hereford. When the Bulmers Centre closed in the 1990s, the loco moved to the East Lancashire Railway. Since April 2009 it has been based at the Crewe Heritage Centre. On 3 June 2012, Princess Elizabeth's whistle signalled the start of the Thames Diamond Jubilee Pageant while the locomotive was standing on Battersea Railway Bridge. The Queen was made aware of the locomotive and waved to the crew on the footplate. On 11 July 2012 Princess Elizabeth hauled the Royal Train from Newport to Hereford and again from Worcester to Oxford as part of the Diamond Jubilee Tour. 6201 was withdrawn from service in July 2012 for a piston and valve examination at the Tyseley Locomotive Works and after repairs, she returned to service on 17 November hauling the "Cumbrian Mountaineer" from Carnforth to Carlisle. She was withdrawn for overhaul at the end of December 2012 having completed her longest period of operation in preservation.

Unique Class 47 that was used as a testbed for Class 56 and Class 58 power units. Seen awaiting its next turn of duty at Westbury shed.

Its conversion from 47046 happened during accident repairs in the mid 70s, initially renumbered 47601 in 1975 then as 47901 in 1979. It was scrapped in 1992.

© Dave Bower

"This NC-130B-1-LM, S/N 57-0526, was the second B model Hercules manufactured by Lockheed Corporation of Marietta, Georgia (Lockheed Number 3502). It was delivered to the US Air Force as a JC-130B in February 1959 and assigned to the 6515th Organizational Maintenance Squadron for flight testing at Edwards AFB, California, on November 29, 1960.

 

While with the 6515th the aircraft was used for jet-assisted take-off (JATO) testing, then it was turned over to the 6593rd Test Squadron's Operating Location No. 1 at Edwards.

 

The plane spent the next seven years supporting the top secret Corona Program. The "J" status and prefix were removed from the aircraft in October 1967.

 

On May 31, 1973 the aircraft was transferred to the 6593rd Test Squadron of the 6594th Test Group at Hickam AFB, Hawaii. There it was modified to perform mid-air retrieval of satellites and other objects as they floated back to Earth beneath parachutes, under the "Falling Star" project and others. The aircraft was also used to recover high altitude air samples in various locations around the world.

 

The plane was acquired by the 6514th Test Squadron at Hill AFB on January 19, 1987. While assigned with that unit the plane was used as an electronic testbed and as a cargo transport. On January 27, 1994 the aircraft was finally retired, with over 11,000 flight hours, and made its final move to Hill Aerospace Museum." - www.hill.af.mil/About-Us/Fact-Sheets/Display/Article/3972...

A close up of 37901 passing Magor nr Newport on a train of steel. 37901 was originally 37150 this loco was one of the four chosen for the initial 37/9 series which was to be a testbed for the proposed Class 38. The Class 38 never happened but a larger version of the 37/9 Mirrlees power units were used in the Class 60. The modifications included ballast weighting upto 120 Tons, EE Generator replaced with a Brush Alternator and reprofiling of the roof sections to accomodate the power unit and exhaust differences. It entered Crewe works in February 1986 for a major overhaul which included fitting of Mirrlees power unit. It left Crewe in October 1986 and was named 'Mirrlees Pioneer' at Cardiff Canton on the 3rd December 1986. It was stored unserviceable in November 1998, entering preservation at Llangollen Railway in 2003. Taken on the 09.03.1987

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