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Configuration options for the WMR.

 

From top to bottom, the machine gun (WMR-MG), assault rifle (WMR-AR), and shotgun (WMR-SG) derivatives for the WMR.

 

This is not for the contest, if you must know.

The Supermarine Spitfire is a British single-seat fighter aircraft that was used by the Royal Air Force and many other Allied countries during and after the Second World War. The Spitfire was built in many variants, using several wing configurations, and was produced in greater numbers than any other British aircraft. It was also the only British fighter to be in continuous production throughout the war. The Spitfire continues to be a popular aircraft, with approximately 55 Spitfires being airworthy, while many more are static exhibits in aviation museums all over the world.

 

The Spitfire was designed as a short-range, high-performance interceptor aircraft by R. J. Mitchell, chief designer at Supermarine Aviation Works (which operated as a subsidiary of Vickers-Armstrong from 1928). In accordance with its role as an interceptor, Mitchell designed the Spitfire's distinctive elliptical wing to have the thinnest possible cross-section; this thin wing enabled the Spitfire to have a higher top speed than several contemporary fighters, including the Hawker Hurricane. Mitchell continued to refine the design until his death from cancer in 1937, whereupon his colleague Joseph Smith took over as chief designer, overseeing the development of the Spitfire through its multitude of variants.

 

During the Battle of Britain (July–October 1940), the Spitfire was perceived by the public to be the RAF fighter, though the more numerous Hawker Hurricane shouldered a greater proportion of the burden against the Luftwaffe. However, because of its higher performance, Spitfire units had a lower attrition rate and a higher victory-to-loss ratio than those flying Hurricanes.

 

After the Battle of Britain, the Spitfire superseded the Hurricane to become the backbone of RAF Fighter Command, and saw action in the European, Mediterranean, Pacific and the South-East Asian theatres. Much loved by its pilots, the Spitfire served in several roles, including interceptor, photo-reconnaissance, fighter-bomber and trainer, and it continued to serve in these roles until the 1950s. The Seafire was a carrier-based adaptation of the Spitfire which served in the Fleet Air Arm from 1942 through to the mid-1950s. Although the original airframe was designed to be powered by a Rolls-Royce Merlin engine producing 1,030 hp (768 kW), it was strong enough and adaptable enough to use increasingly powerful Merlin and, in later marks, Rolls-Royce Griffon engines producing up to 2,340 hp (1,745 kW); as a consequence of this the Spitfire's performance and capabilities improved, sometimes dramatically, over the course of its life.

 

Mk V (Types 331, 349 & 352)

 

Spitfire LF.Mk VB, BL479, flown by Group Captain M.W.S Robinson, station commander of RAF Northolt, August 1943. This Spitfire has the wide bladed Rotol propeller, the internal armoured windscreen and "clipped" wings.

Late in 1940, the RAF predicted that the advent of the pressurised Junkers Ju 86P bomber series over Britain would be the start of a new sustained high altitude bombing offensive by the Luftwaffe, in which case development was put in hand for a pressurised version of the Spitfire, with a new version of the Merlin (the Mk VI). It would take some time to develop the new fighter and an emergency stop-gap measure was needed as soon as possible: this was the Mk V.

 

The basic Mk V was a Mk I with the Merlin 45 series engine. This engine delivered 1,440 hp (1,074 kW) at take-off, and incorporated a new single-speed single-stage supercharger design. Improvements to the carburettor also allowed the Spitfire to use zero gravity manoeuvres without any problems with fuel flow. Several Mk I and Mk II airframes were converted to Mk V standard by Supermarine and started equipping fighter units from early 1941. The majority of the Mk Vs were built at Castle Bromwich.

 

The VB became the main production version of the Mark Vs. Along with the new Merlin 45 series the B wing was fitted as standard. As production progressed changes were incorporated, some of which became standard on all later Spitfires. Production started with several Mk IBs which were converted to Mk VBs by Supermarine. Starting in early 1941 the round section exhaust stacks were changed to a "fishtail" type, marginally increasing exhaust thrust. Some late production VBs and VCs were fitted with six shorter exhaust stacks per side, similar to those of Spitfire IXs and Seafire IIIs; this was originally stipulated as applying specifically to VB(trop)s. After some initial problems with the original Mk I size oil coolers, a bigger oil cooler was fitted under the port wing; this could be recognised by a deeper housing with a circular entry. From mid-1941 alloy covered ailerons became a universal fitting.

 

Spitfire VC(trop), fitted with Vokes filters and "disc" wheels, of 417 Squadron RCAF in Tunisia in 1943.

A constant flow of modifications were made as production progressed. A "blown" cockpit hood, manufactured by Malcolm, was introduced in an effort to further increase the pilot's head-room and visibility. Many mid to late production VBs - and all VCs - used the modified, improved windscreen assembly with the integral bullet resistant centre panel and flat side screens introduced with the Mk III. Because the rear frame of this windscreen was taller than that of the earlier model the cockpit hoods were not interchangeable and could be distinguished by the wider rear framing on the hood used with the late-style windscreen.

 

Different propeller types were fitted, according to where the Spitfire V was built: Supermarine and Westland manufactured VBs and VCs used 10 ft 9 in (3.28 m) diameter, 3 bladed de Havilland constant speed units, with narrow metal blades, while Castle Bromwich manufactured VBs and VCs were fitted with a wide bladed Rotol constant speed propeller of either 10 ft 9 in (3.28 m) diameter, with metal blades, or (on late production Spitfires) 10 ft 3 in (3.12 m) diameter, with broader, "Jablo" (compressed wood) blades. The Rotol spinners were longer and more pointed than the de Havilland leading to a 3.5 in (8.9 cm) increase in overall length. The Rotol propellers allowed a modest speed increase over 20,000 ft (6,100 m) and an increase in the service ceiling. A large number of Spitfire VBs were fitted with "gun heater intensifier" systems on the exhaust stacks. These piped additional heated air into the gun bays. There was a short tubular intake on the front of the first stack and a narrow pipe led into the engine cowling from the rear exhaust.

 

The VB series were the first Spitfires able to carry a range of specially designed "slipper" drop tanks which were fitted underneath the wing centre-section. Small hooks were fitted, just forward of the inboard flaps: when the tank was released these hooks caught the trailing edge of the tank, swinging it clear of the fuselage.

 

With the advent of the superb Focke Wulf Fw 190 in August 1941 the Spitfire was for the first time truly outclassed, hastening the development of the "interim" Mk IX. In an effort to counter this threat, especially at lower altitudes, the VB was the first production version of the Spitfire to use "clipped" wingtips as an option, reducing the wingspan to 32 ft 2 in (9.8 m).The clipped wings increased the roll rate and airspeed at lower altitudes. Several different versions of the Merlin 45/50 family were used, including the Merlin 45M which had a smaller "cropped" supercharger impeller and boost increased to +18 lb. This engine produced 1,585 hp (1,182 kW) at 2,750 ft (838 m), increasing the L.F VB's maximum rate of climb to 4720 ft/min (21.6 m/s) at 2,000 ft (610 m).

 

VB Trop of 40 Squadron SAAF fitted with the "streamlined" version of the Aboukir filter, a broad-bladed, 10 ft 3 in (3.12 m) diameter Rotol propeller, and clipped wings.

The Mk VB(trop) (or type 352) could be identified by the large Vokes air filter fitted under the nose; the reduced speed of the air to the supercharger had a detrimental effect on the performance of the aircraft, reducing the top speed by 8 mph (13 km/h) and the climb rate by 600 ft/min (3.04 m/s), but the decreased performance was considered acceptable. This variant was also fitted with a larger oil tank and desert survival gear behind the pilot's seat. A new "desert" camouflage scheme was applied. Many VB(trop)s were modified by 103 MU (Maintenance Unit-RAF depots in which factory fresh aircraft were brought up to service standards before being delivered to squadrons) at Aboukir, Egypt by replacing the Vokes filter with locally manufactured "Aboukir" filters, which were lighter and more streamlined. Two designs of these filters can be identified in photos: one had a bulky, squared off filter housing while the other was more streamlined. These aircraft were usually fitted with the wide blade Rotol propeller and clipped wings.

 

Triumph Spitfire Mk I Roadster

 

The Triumph Spitfire is a small English two-seat sports car, introduced at the London Motor Show in 1962.[3] The vehicle was based on a design produced for Standard-Triumph in 1957 by Italian designer Giovanni Michelotti. The platform for the car was largely based upon the chassis, engine, and running gear of the Triumph Herald saloon, and was manufactured at the Standard-Triumph works at Canley, in Coventry. As was typical for cars of this era, the bodywork was fitted onto a separate structural chassis, but for the Spitfire, which was designed as an open top or convertible sports car from the outset, the ladder chassis was reinforced for additional rigidity by the use of structural components within the bodywork. The Spitfire was provided with a manual hood for weather protection, the design improving to a folding hood for later models. Factory-manufactured hard-tops were also available.

 

The Triumph Spitfire was originally devised by Standard-Triumph to compete in the small sports car market that had opened up with the introduction of the Austin-Healey Sprite. The Sprite had used the basic drive train of the Austin A30/35 in a light body to make up a budget sports car; Triumph's idea was to use the mechanicals from their small saloon, the Herald, to underpin the new project. Triumph had one advantage, however; where the Austin A30 range was of unitary construction, the Herald featured a separate chassis. It was Triumph's intention to cut that chassis down and clothe it in a sports body, saving the costs of developing a completely new chassis / body unit.

 

Italian designer Michelotti—who had already penned the Herald—was commissioned for the new project, and came up with a traditional, swooping body. Wind-up windows were provided (in contrast to the Sprite/Midget, which still featured sidescreens, also called curtains, at that time), as well as a single-piece front end which tilted forwards to offer unrivaled access to the engine. At the dawn of the 1960s, however, Standard-Triumph was in deep financial trouble, and unable to put the new car into production; it was not until the company was taken over by the Leyland organization funds became available and the car was launched. Leyland officials, taking stock of their new acquisition, found Michelotti's prototype hiding under a dust sheet in a corner of the factory and rapidly approved it for production.

 

Spitfire 4 or Mark I (1962-1964)

 

Overview:

Production1962–1964

45,753 made

Powertrain:

Engine1,147 cc (1.1 l) I4

Transmission4-speed manual with optional overdrive on top and third from 1963 onwards

Dimensions:

Curb weight1,568 lb (711 kg) (unladen U.K.-spec)

 

The production car changed little from the prototype, although the full-width rear bumper was dropped in favour of two part-bumpers curving round each corner, with overriders. Mechanicals were basically stock Herald. The engine was an 1,147 cc (1.1 l) 4-cylinder with a pushrod OHV cylinder head and 2 valves per cylinder, mildly tuned for the Spitfire, fed by twin SU carburettors. Also from the Herald came the rack and pinion steering and coil-and-wishbone front suspension up front, and at the rear a single transverse-leaf swing axle arrangement. This ended up being the most controversial part of the car: it was known to "tuck in" and cause violent over steer if pushed too hard, even in the staid Herald. In the sportier Spitfire (and later the 6-cylinder Triumph GT6 and Triumph Vitesse) it led to severe criticism. The body was bolted to a much-modified Herald chassis, the outer rails and the rear outriggers having been removed; little of the original Herald chassis design was left, and the Spitfire used structural outer sills to stiffen its body tub.

 

The Spitfire was an inexpensive small sports car and as such had very basic trim, including rubber mats and a large plastic steering wheel. These early cars were referred to both as "Triumph Spitfire Mark I" and "Spitfire 4", not to be confused with the later Spitfire Mark IV.

 

In UK specification the in-line four produced 63 bhp (47 kW) at 5750 rpm, and 67 lb·ft (91 N·m)of torque at 3500 rpm. This gave a top speed of 92 mph (148 km/h), and would achieve 0 to 60 mph (97 km/h) in 17.3 seconds. Average fuel consumption was 31mpg.

 

For 1964 an overdrive option was added to the 4-speed manual gearbox to give more relaxed cruising. Wire wheels and a hard top were also available.

 

Text regarding the Supermarine Spitfire aeroplane and Triumph Spitfire Roadster has been taken from excerpts of Wikipedia articles on each model.

 

The Supermarine Spitfire Mk VB aircraft and 1962 Triumph Spitfire Mk I road car have been modelled in Lego miniland-scale for Flickr LUGNuts' 79th Build Challenge, - 'LUGNuts goes Wingnuts, ' - featuring automotive vehicles named after, inspired by, or with some relationship to aircraft.

The 6x2 ‘Chinese Six’ configuration was always something of rare bird, although it did enjoy brief periods of popularity, most notably on tractor units in the mid-1960s following changes to the Construction & Use legislation. On rigids, such as this Foden FG, it was believed to provide better weight distribution; although a counter-claim suggests that reversing manoeuvres could be more challenging. Alex Anderson of Bowness in West Lothian is well-known for its traditional livery and superb standard of presentation; and for its excellent selection of fleet preserved vehicles (07-Mar-20).

 

All rights reserved. Not to be re-posted anywhere without prior written permission. Please follow the link below for additional information about my Flickr collection and the techniques used:

www.flickr.com/photos/northernblue109/6046035749/in/set-7..

Excerpt from www.bwst.ca/the-artists/benoy:

 

Nancy Benoy is a self-taught artist working in acrylic, watercolour, and reclaimed materials. This Hamiltonian is recognized for abstract works driven by curiosity of colour and shape to create joy. She is an acclaimed arts educator and advocate with 20 years of experience spreading her enthusiasm.

 

Artist Statement:

 

Curiosity is at the core of my art practice. I am influenced by colour, line and shape and their interaction to create pieces that spark sustained observation and joy. Sustainability has guided me into using offcuts and paints destined for the landfill to elevate the discarded and unwanted.

At work I walked outside briefly today. It'd been raining.

+++ 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 Supermarine Spitfire is a British single-seat fighter aircraft that was used by the Royal Air Force and many other Allied countries during and after the Second World War. The Spitfire was built in many variants, using several wing configurations, and was produced in greater numbers than any other British aircraft.

 

The Spitfire was designed as a short-range, high-performance interceptor aircraft by R. J. Mitchell, chief designer at Supermarine Aviation Works (which operated as a subsidiary of Vickers-Armstrong from 1928). In accordance with its role as an interceptor, Mitchell designed the Spitfire's distinctive elliptical wing to have the thinnest possible cross-section; this thin wing enabled the Spitfire to have a higher top speed than several contemporary fighters, including the Hawker Hurricane.

 

It was the only British fighter to be in continuous production throughout World War II, and remained in service with several air forces around the world for several years. One of its post-war operators was the Lebanese Air Force, or Al Quwwat al-Jawwiya al-Lubnaniyya (لقوات الجوية اللبنانية‎).

The Lebanese Air Force was established in 1949 under the command of then-Lieutenant Colonel Emile Boustany who later became commander of the army. Soon after its establishment, a number of planes were donated by the British, French, and Italian governments, with additional planes donated by Britain and Italy later that same year.

 

Britain donated 4 Percival Prentices, 2 World War II-era Percival Proctors and seven trpocailized Supermarine Spitfires (six Mk. XVIe and one TR.8 two-seater), while Italy donated 4 Savoia-Marchetti SM.79 bombers which were mainly used for transportation.

 

The Mk XVI Spitfire was a WWII design, and the last variant powered by a Merlin engine and based on the original, sleek fuselage. It was basically the same as the Mk IX, except for the engine, a Merlin 266. The Merlin 266 was the Merlin 66 and was built under licence in the USA by the Packard Motor Company. The "2" was added as a prefix in order to avoid confusion with the engines, as they required different tooling.

 

All Mk XVI aircraft produced (a total of 1,054 Mk XVIs left Castle Bromwich) were of the Low-Altitude Fighter (LF) variety. This was not determined by the length of the wings (clipped wings were fitted to most LF Spitfires), but by the engine, which had been optimised for low-altitude operation. All production Mk XVIs had clipped wings for low altitude work and were fitted with the rear fuselage fuel tanks with a combined capacity of 75 gal. Many XVIs featured cut-down rear fuselages with bubble canopies. On these aircraft the rear fuselage tank capacity was limited to 66 gal.

 

Because of a slightly taller intercooler and rearranged accessories on the Packard Merlins a new, bulged upper cowling was introduced, a detail that also appeared on late production IXs. For the service in the Middel East region the Lebanese machines received dust filters which considerably changed the aircraft's silhouette.

 

Armament consisted of two 20 mm Hispano II cannons - each with 120 rpg - and two 0.50 calibre Browning machine guns - each with 250 rpg. 1 × 500 lb (227 kg) bomb could be carried underneath the centre rack, and 1 × 250 lb (114 kg) bomb could be slung under each wing. As a special feature, the wing hardpoints of the Lebanese Spitfires were "wet" so that slipper tanks with 24 gal. each could be carried, compensating for the reduces rear fuselage tank due to the bubble canopy's lowered dorsal spine.

 

The Lebanese Spitfires only saw a short service, since in 1953, jet fighters were introduced when 16 de Havilland Vampire jets were received, and the first Hawker Hunters arrived in 1959, which replaced the obsolete Spitfires. This initial Hunter batch was followed by more Hunters through 1977.

 

In 1968, 12 Mirage IIIELs were delivered from France but were grounded in the late 1970s due to lack of funds. In 2000, the grounded Mirages were sold to Pakistan, and four Hunters were even revived in 2008 and served until 2014.

  

General characteristics:

Crew: one pilot

Length: 29 ft 11 in (9.12 m)

Wingspan: 36 ft 10 in (11.23 m)

Height: 11 ft 5 in (3.86 m)

Wing area: 242.1 ft2 (22.48 m2)

Airfoil: NACA 2209.4(tip)

Empty weight: 5,065 lb (2,297 kg)

Loaded weight: 6,622 lb (3,000 kg)

Max. takeoff weight: 6,700 lb (3,039 kg)

 

Powerplant:

1× Rolls-Royce Merlin 60 supercharged V12 engine,

rated at 1.470 hp (1.096 kW) at 9.250 ft (2.820 m)

 

Performance:

Maximum speed: 370 mph, (322 kn, 595 km/h)

Combat radius: 410 nmi (470 mi, 760 km)

Ferry range: 991 nmi (1,135 mi, 1,827 km)

Service ceiling: 36,500 ft (11,125 m)

Rate of climb: 2,600 ft/min (13.2 m/s)

Wing loading: 27.35 lb/ft2 (133.5 kg/m²)

Power/mass: 0.22 hp/lb (0.36 kW/kg)

 

Armament:

2x 20mm Hispano Mk II cannon (120 RPG)

2x .5 in Browning machine guns (250 RPG)

Three hardpoints (1 ventral, 1 under each outer wing) for up to 1.000 lb (454 kg).

  

The kit and its assembly:

This whif is based on a simple idea: how did Lebanon's Air Force start? Small countries make a good whif playground, and I guess that nobody has the Lebanon on his/her list...?

Another factor was that I had some Austrian roundels left in store that could, with a green dot, easily be turned into Lebanese markings. So the theme was quickly settled, but the details take some preparation time, so the idea lingered for some time.

 

After some legwork I deemed a simple Spitfire with a dust filter worthy as an initial aircraft, and the respective Hobby Boss kit of a Spitfire Mk. VB in the stash came handy.

But somehow this was a bit dull, and at the inception of the Lebanon Air Force there were better option available than an early Mk. V. I still wanted a sleek, Merlin-powered Spitfire variant, though, and eventually settled for the Mk. XVI - with its clipped wings and the bubble canopy it has a very distinctive look.

 

When a "1 Week group Build" at whatifmodelers.com in the Easter Week 2015 was announced, I took this occassion to build the Lebanese Spitfire.

 

By that time I already had a basis kit at hand (Heller's Spitfire XVI) as well as some donation parts and decals.

Work was strightforward, the Heller kit was built almost OOB. It's a rather old model kit, with raised panel lines, but good detail. The material is thin, so the built item lacks some structural stability! On the other side, this makes some minor mods really easy: I lowered the flaps and moved the tail rudders slightly off of neutral position. I also opened the cockpit "door" on the left side for later static display, even though the cockpit itself was left OOB. It's a bit "flat", but for the kit's age it's pretty good, and the injected canopy is crystal clear and fits perfectly.

 

I had some major woes concerning the fit for the forward fuselage, and even more when I tried to mate wings and fuselage: there was a 1mm gap(!) on both sides that had to be bridged with putty, and the thin and flexible material did help much...

 

Other mods concern the propeller (added a styrene tube and a metal axis for free spin), the radiators (these are molded into the lower wings - sounds horrible, but is made very well and thin, I just added some foamed styrene inside as protective mesh because OOB there's just a blank "box" inside) and the kit received a dust filter - a resin piece taken from a Pavla conversion set for Hawker Hurricanes.

  

Painting and markings:

While a donated RAF Spitfire would certainly have carried a desert paint scheme in Dark Earth/Mid Stone/Azure Blue or a late WWII Dark Green/Ocean Grey/Light Sea Grey livery I settled for something more individual and effective for the rugged Levantine terrain.

In this case I went for the rarely used RAF 'Tropical Scheme' in Mid Stone/Dark Green from above and with Mediterrenean Blue undersides.

 

The pattern itself is standard RAF, the upper cammo taken down onto the dust filter's flanks was taken over from RAAF Spitfires during WWII (RAF aircraft would carry a higher waterline, with the filter painted completely in the lower surface's tone). Basic paints are RAF Dark Green from Modelmaster and Humbrol 84 (RAF Mid Stone) - rather authentic. But I used Humbrol 87 (Steel Grey) for the undersides - it's rather intense and has a greenish hue, and by far not as dark as the typical RAF Azure Blue or PRU Blue.

 

Interior surfaces were painted in RAF Cockpit Green (Modelmaster Authentic), while the landing gear and its wells were kept in Aluminum Dope (Humbrol 56).

 

Decals/markings were puzzled together and improvised. The Lebanese roundels are actually Austrian national markings into which a dark green dot has ben added manually... the fin flash and the roman/arabic codes come from an Xtradecal aftermarket sheet.

 

Beyond these basic markings I did not add anything flashy - in 1951 things were rather simple,

The kit received a light shading and some dry painting with light grey, plus a light black ink wash. Soot/exhaust stains were created with grinded graphite and around the engine some leaked oil was added with Tamiya's "Smoke", and everything was sealed under a coat of matt acrylic varnish.

  

I'll admit it's not a spectacular whif, and overall rather simple concerning build and painting. But a proud addition to whatifmodelers.com's "! Week Group Build", even though this was already finished in just three days from sprues to beauty pics...

 

Nikon D800E + 70-200mm F/2.8 Nikkor Lens vs. Sony A7r + 35mm F/2.8 Carl Zeiss Lens! Both in 45surfer bracket configurations, with Sony NEX-6 cameras attached to the upper cameras with a bracket, for shooting stills and video at the same time! Guess which is heavier! :) The new 45surfer rig is a bit lighter, but that will change a bit when Sony comes out with longer zooms for the Sony A7r.

 

Both are great! The Sony NEX-6 bracketed to the D800E has the 50mm F/1.8 lens on it, while the Sony NEX-6 bracketed to the Sony A7R has the 35mm F/2.8 lens on it!

 

Check out some video!

www.youtube.com/watch?v=RiOMrZIEzg8

www.youtube.com/watch?v=Y7gq_gCk0jE

 

The Sony ILCE7R A7r rocks! Was using the B+W 49mm Kaesemann Circular Polarizer MRC Filter on partly cloudy day with some intermittent sun, but mostly cloudy. Check out the low glare off the rocks and water and dramatic, polarizwer-enhanced sky! Super sharp images and crystal-clear pictures!

 

Was testing the Sony HVL-F60M External Flash on the Sony A7r. You can see it going off in some of the photos (check the exif if in doubt)--worked great, but it overheated a bit sooner than my Nikon flash on the D800E. But it's all good!

 

Here's some epic goddess video shot at the same time as stills using my 45surfer method/philosophy:

www.youtube.com/watch?v=bUbE0ay7UeI

www.youtube.com/watch?v=eC-M9fVwk9k

 

Join Johnny Ranger McCoy's youtube channel for goddess video shot @ the same time as the stills with the Sony A7 !

 

www.youtube.com/user/bikiniswimsuitmodels

 

Beautiful swimsuit bikini model goddess on a beautiful December Malibu afternoon! Shot it yesterday. :) Love, love, love the new Sony A7 R!

 

Was a fun test shoot. Many, many more to come!

 

All the best on your Epic Hero's Journey from Johnny Ranger McCoy!

 

Join my facebook!

www.facebook.com/45surfHerosJourneyMythology

Follow me on facebook www.facebook.com/elliot.mcgucken !

Quoting Smithsonian National Air and Space Museum | Dornier Do 335 A-0 Pfeil (Arrow):

 

The Do-335 was one of a small group of aircraft marking the pinnacle of international piston-engined development. It was the fastest production piston-engined fighter ever built, attaining 846 kilometers per hour (474 mph) in level flight at a time when the official world speed record was 755 kph (469 mph). Powered by two 1800-hp engines in a unique low-drag configuration and weighing 9600 kg (21,000 lb) loaded, it was an exceptional heavy fighter. This very innovative design also featured an ejection seat, for pilot safety, and a jettisoning fin.

 

The unconventional layout of the Do-335 -- one engine "pulling" in the nose and another "pushing" in the tail - was patented by Claudius Dornier in 1937. The configuration provided the power of two engines, but with reduced drag and better maneuverability. The German Aviation Ministry (RLM) was interested in the design, but initially wanted Dornier only to produce bombers. By 1942, Dornier was still continuing design work and the war situation was worsening. The Luftwaffe now needed a multi-purpose fighter, and the prototype Do-335V-1 ("V" indicating "versuchs" or "experimental") flew in fighter form in September, 1943 - six years after its conception. Orders were immediately placed for 14 prototypes, 10 A-0 preproduction aircraft, 11 production A-1 single-seaters, and 3 A-10 and A-12 two-seat trainers.

 

The aircraft was quite large for a single-seat fighter, with a cruciform tail and a tricycle landing gear. The two massive liquid-cooled Daimler-Benz DB-603 engines were used in four different versions, each displacing 44.5 liters (2670 cu in) and weighing 910 kg (2006 lb). The engine produced 1750 hp from 12 cylinders in an inverted V layout using fuel injection and an 8.3:1 compression ratio. The rear three-bladed propeller and dorsal fin were jettisoned by explosive bolts in an emergency, to allow the pilot to bail out safely using a pneumatic ejection seat. The seat, inclined 13 degrees to the rear, was ejected with a force of 20 times gravity. The ventral fin could be jettisoned for a belly landing.

 

Unlike a normal twin-engined aircraft, with wing-mounted engines, loss of an engine on the Do-335 did not cause a handling problem. Even with one engine out, speed was a respectable 621 kph (348 mph). Because of its appearance, pilots dubbed it the "Ant eater" ("Ameisenbar"), although they described its performance as exceptional, particularly in acceleration and turning radius. The Do-335 was very docile in flight and had no dangerous spin characteristics. Many Do-335 prototypes were built, as the Reich strained desperately to provide day and night fighters and fast reconnaissance aircraft to the failing war effort. One of the many RLM production plans, issued in December 1943, called for the production of 310 Do-335s by late 1945. Initial production was at the Dornier Manuel plant, but this factory was bombed heavily in March-April, 1944, and the Do-335 tooling was destroyed.

 

Ten Do-335A-0 preproduction aircraft were then produced at Dornier's Oberpfaffenhofen plant in July-October 1944, by which time the Allied bombing campaign was delaying arrivals of engines, propellers, radios, and structural subcomponents. This had a serious effect, because the Do-335 was not a simple aircraft: installation of the electronics alone took 60 hours of assembly, and the electrical parts list was 112 pages long. Production of Daimler-Benz engines, for example, was switched to factories set up in underground salt mines and gypsum mines, but high humidity caused corrosion problems and production dropped 40 percent. Although several preproduction aircraft were issued to combat conversion units some 10 months before the war ended, no Do-335s actually entered combat. Deliveries began to the 1st Experimental Squadron of the Commander-in-Chief of the Luftwaffe ( I/Versuchsverband Ob.d.L.) in late July 1944 for operational trials.

 

The first of the Do-335A-1 production version left the Dornier line at Friedrichshafen early in 1945, one of only four produced in 1945. It was armed with one 30 mm MK-103 cannon (70 rounds were carried) firing through the propeller hub and two 15 mm MG-151/15 cannon (200 rounds per gun) firing from the top of the forward engine. Even with the fighter situation as desperate as it was, these aircraft were still equipped to carry 500 kg (1100 lb) of bombs internally. Further operational testing, including use of air-to-ground guided missiles, began in Spring 1945 with Trials Unit (Erprobungskommando) 335.

 

The Do-335A-6 was to be a two-seat night fighter version with the advanced FFO FuG-217J Neptun radar having triple "trident"-like antennas (hence the name "Neptun") on the fuselage and wings, but only a prototype was completed. A total of 37 prototypes, 10 A-0s, 11 A-1s and 2 A-12 trainers were built, although nearly 85 additional aircraft were in assembly when U.S. troops overran the Friedrichshafen factory in late April, 1945. The Vienna-Swechat plant of the Ernst Heinkel AG was also scheduled to build the Do-335 beginning in February, 1945, but production never started.

 

The NASM aircraft is the second Do-335A-0, designated A-02, with construction number (werke nummer) 240102 and factory registration VG+PH. It was built at Dornier's Rechlin-Oberpfaffenhofen, Germany, plant on April 16, 1945. It was captured by Allied forces at the plant on April 22, 1945. After checkout, it was flown from a grass runway at Oberweisenfeld, near Munich, to Cherbourg, France. During this flight, the Do-335 easily outclimbed and outdistanced two escorting P-51s, beating them to Cherbourg by 45 minutes. Under the U.S. Army Air Force's "Project Sea Horse," two Do-335s were shipped to the United States aboard the Royal Navy ship HMS "Reaper" together with other captured German aircraft, for detailed evaluation. This aircraft was assigned to the U.S. Navy, which tested it at the Test and Evaluation Center, Patuxent River Naval Air Station, Maryland. The other aircraft, with registration FE-1012 (later T2-1012), went to the USAAF at Freeman Field, Indiana, where it was tested in early 1946. Its subsequent fate is unknown, and this is the only Do-335 known to exist.

 

Following Navy flight tests in 1945-48, the aircraft was donated to the Smithsonian's National Air Museum in 1961 but was stored at NAS Norfolk until 1974. It was then returned to Oberpfaffenhofen, Germany, where the Dornier company restored it to original condition in 1975. The return trip to Germany required an exemption under U.S. laws concerning the export of munitions. The Dornier craftsmen doing the restoration - many of whom had worked on the original aircraft -- were astonished to find that the explosive charges fitted to blow off the tail fin and rear propeller in an emergency were still in the aircraft and active, 30 years after their original installation! The Do-335 was put on static display at the May 1-9, 1976, Hannover Airshow, and then loaned to the Deutsches Museum in Munich, where it was on prominent display until returned to Silver Hill, MD, for storage in 1986.

 

Country of Origin:

Germany

 

Physical Description:

Twin engine, pusher / puller, fighter / bomber; grey/green, green; late World War II development.

Illogical no more.

 

Seems when MDU redid the adjacent 3-phase line that served this pole, they decided to make it safer to work around. Pic of its previous configuration in the comments.

Bus Operator: Alps The Bus

Bus number:

Area of Operation: Provincial Operation

Seating Configuration: 2x2

Seating Capacity: 51

 

Bus Manufacturer: Zhengzhou Yutong Bus Company, Ltd.

Model: Yutong ZK6122HD9

Chassis: Yutong ZK6112CRD9

Engine: Yuchai YC6L310-20

Llanfairpwll railway station is a station on the North Wales Coast Line from Crewe to Holyhead, serving the village of Llanfairpwllgwyngyll, Anglesey.

 

Opened in 1848 it was initially the terminus of the line from Holyhead before the opening of the Britannia Bridge to the mainland in 1850. It suffered a catastrophic fire on 13 November 1865 and had to be completely re-constructed. It was closed in 1966 but reopened in 1970 due to the fire on the Britannia Bridge again as the terminus for trains from Holyhead, with a single wooden platform. It was again closed in 1972 and subsequently reopened again 1973 with both wooden platforms (the only one on the island), which was refurbished in 2017 and the signal box remain from the original configuration, but converted into a gate keeper's box, meaning no junctions or signals are controlled from there, except for gate locking. However, a turntable, sidings and goods yard have disappeared, the latter two under a car park.

 

The station is known for its longer name, Llanfairpwllgwyngyllgogerychwyrndrobwllllantysiliogogogoch, but this is a Victorian contrivance for the benefit of tourists with no basis in historical usage. It comprises the full name of the village, plus local topographical details, plus the name of a neighbouring church etc. The actual longest railway station name in Wales (indeed the UK) is Rhoose Cardiff International Airport railway station.

 

The station is unstaffed and has no ticket provision - these must be bought on the train or prior to travel. Waiting shelters are provided on each platform and train running details offered via timetable posters and digital information screens (as can be seen from the accompanying station photograph). The station is not listed as accessible for mobility-impaired and wheelchair users on the National Rail Enquiries website.

 

During April 2017, the upgrade of the footbridge was completed as part of Network Rail's Railway Upgrade Plan. The footbridge, which is over 100 years old, was temporarily removed earlier in the year, to undergo a £395,000 upgrade, including specialist refurbishment and repairs at the Centregreat Rail workshop in Cardiff.

 

Trains used to stop in each direction. These are Transport for Wales Rail services between Holyhead and Chester via Llandudno Junction. These continue to Shrewsbury and then either Birmingham International or Cardiff Central, though a limited number run to/from Crewe instead. On Mondays to Saturdays, 9 services operates to Holyhead and 13 towards Chester. On Sundays, services are reduced to 6 towards Holyhead and 7 towards Chester.

 

The station has very short platforms, only 40 yards (37 m) long. As a result, only one door on Transport for Wales intercity services is unlocked by the conductor/guard for passengers (Except for the BR classes 150/2 and 153 which occasionally visits Holyhead.)

 

Llanfairpwllgwyngyll, or Llanfair Pwllgwyngyll (Welsh: [ɬanˌvair puɬˈɡwɨ̞nɡɨ̞ɬ]), is a large village and local government community on the island of Anglesey, Wales, on the Menai Strait next to the Britannia Bridge and across the strait from Bangor. Both shortened (Llanfairpwll or Llanfair PG) and lengthened (Llanfair-pwllgwyngyll-gogery-chwyrn-drobwll-llan-tysilio-gogo-goch) forms of the placename are used in various contexts.

 

At the 2011 Census, the population was 3,107, of whom 71% could speak Welsh. It is the sixth largest settlement on the island by population.

 

The long form of the name, with 58 characters split into 18 syllables, is purported to be the longest place name in Europe and the second longest one-word place name in the world.

 

There has been human activity and settlement in the area of the village since the Neolithic era (4000–2000 BC), with subsistence agriculture and fishing the most common occupations for much of its early history. The island of Anglesey was at that point reachable only by boat across the Menai Strait. A largely destroyed, collapsed dolmen can be found from this period in the parish, located at Ty Mawr north of the present-day church; early Ordnance Survey maps show a long cairn on the site. The probable remains of a hillfort, with a fragmentary bank and ditch, were recorded on an outcrop known as Craig y Ddinas.

 

The area was briefly invaded and captured by the Romans under Gaius Suetonius Paulinus, temporarily abandoned in order to consolidate forces against Boudicca, then held until the end of Roman Britain.

 

With the withdrawal of the Roman forces, the area fell under the control of the early medieval Kingdom of Gwynedd. There has likely been a small Christian religious site, perhaps a monastic cell, in the area since the 7th century. Surveys of the later medieval period show that the tenants of the township of Pwllgwyngyll, as it was then known, held a total of 9 bovates of land from the Bishop of Bangor under the feudal system. A church was built during the medieval period and dedicated to Mary, probably under Norman influence: the building, later demolished and replaced by a Victorian-era church, was unusual in having a semi-circular apse, a feature more usually associated with cathedrals. Despite religious activity, the rural nature of the settlement meant that the parish had a population of only around 80 in 1563.

 

Much of the land was absorbed into the Earldom of Uxbridge, which later became the Marquisate of Anglesey, and was subject to enclosures. In 1844, for example, 92% of the land in Llanfairpwll was owned by just three individuals. The population of the parish reached 385 by 1801.

 

In 1826, Anglesey was connected to the rest of Wales by the construction of the Menai Suspension Bridge by Thomas Telford, and connected with London in 1850 with the building of the Britannia Bridge and the busy North Wales Coast railway line, which connected the rest of Great Britain to the ferry port of Holyhead. The old village, known as 'Pentre Uchaf' ("upper village") was joined by new development around the railway station, which became known as 'Pentre Isaf', the "lower village".

 

The first meeting of the Women's Institute took place in Llanfairpwll in 1915, and the movement (which began in Canada) then spread through the rest of the British Isles.

 

The original name of the medieval township, within whose boundaries the present-day village lies, was Pwllgwyngyll, meaning "the pool of the white hazels". Pwllgwyngyll was one of two townships making up the parish, the other being Treforion; its name was first recorded as 'Piwllgunyl' in an ecclesiastical valuation conducted in the 1250s for the Bishop of Norwich.[16] The parish name was recorded as Llanfair y Pwllgwyngyll ('Llanfair' meaning "[St.] Mary's church"; y meaning "(of) the") as far back as the mid 16th century, in Leland's Itinerary. The suffixing of the township name to that of the church would have served to distinguish the parish from the many other sites dedicated to Mary in Wales.

 

Longer versions of the name are thought to have first been used in the 19th century in an attempt to develop the village as a commercial and tourist centre. The long form of the name is the longest place name in the United Kingdom and one of the longest in the world at 58 characters (51 "letters" since "ch" and "ll" are digraphs, and are treated as single letters in the Welsh language). The village is still signposted Llanfairpwllgwyngyll, marked on Ordnance Survey maps as Llanfair Pwllgwyngyll and the railway station is officially named Llanfairpwll, a form used by local residents. The name is also shortened to Llanfair PG, sufficient to distinguish it from other places in Wales called Llanfair (meaning "[St.] Mary's church").

 

The long name was supposedly contrived in 1869 as an early publicity stunt to give the station the longest name of any railway station in Britain. According to Sir John Morris-Jones the name was created by a local tailor, whose name he did not confide, letting the secret die with him. This form of the name adds a reference to the whirlpool in the Menai Strait known as the Swellies and to the small chapel of St. Tysilio, located on a nearby island. The final -gogogoch ("red cave") is supposed to have been an addition inspired by the Cardiganshire parish of Llandysiliogogo, rather than by any local features.

 

Literally translated, the long form of the name means: "[The] church of [St.] Mary (Llanfair) [of the] pool (pwll) of the white hazels (gwyn gyll) near to [lit. "over against"] (go ger) the fierce whirlpool (y chwyrn drobwll) [and] the church of [St.] Tysilio (Llantysilio) of the red cave (-ogo[f] goch)". Various elements have occasionally been translated differently, for example "the white pool among the hazel trees" or "the cave of St Tysilio the Red".

 

The true originator and date of the longer version of the name is less certain, however: an ecclesiastical directory published several years before the claimed renaming gives what it calls the "full" parish name in the slightly differing form of Llanfair-pwll-gwyn-gyll-goger-bwll-tysilio-gogo ("St Mary's church of the pool of the white hazels over against the pool of St Tysilio Gogo [Tysilio of the cave]"), while Llan-vair-pwll-gwyn-gyll-goger-bwll-dysilio-gogo appears in a paper on placenames published in 1849, its author noting that "the name was generally abridged" by locals. While the addition regarding the Swellies is supposed only to have been made in the 1860s, early 19th century guidebooks had already suggested a derivation of the element pwllgwyngyll from pwll, gwyn and gwyll ("gloomy raging pool"), in reference to the Swellies.

 

The Isle of Anglesey is a county off the north-west coast of Wales. It is named after the island of Anglesey, which makes up 94% of its area, but also includes Holy Island (Ynys Gybi) and some islets and skerries. The county borders Gwynedd across the Menai Strait to the southeast, and is otherwise surrounded by the Irish Sea. Holyhead is the largest town, and the administrative centre is Llangefni. The county is part of the preserved county of Gwynedd.

 

The Isle of Anglesey is sparsely populated, with an area of 276 square miles (710 km2) and a population of 68,900. After Holyhead (12,103), the largest settlements are Llangefni (5,500) and Amlwch (3,967). The economy of the county is mostly based on agriculture, energy, and tourism, the latter especially on the coast. Holyhead is also a major ferry port for Dublin, Ireland. The county has the second-highest percentage of Welsh speakers in Wales, at 57.2%, and is considered a heartland of the language.

 

The island of Anglesey, at 676 square kilometres (261 sq mi), is the largest in Wales and the Irish Sea, and the seventh largest in Britain. The northern and eastern coasts of the island are rugged, and the southern and western coasts are generally gentler; the interior is gently undulating. In the north of the island is Llyn Alaw, a reservoir with an area of 1.4 square miles (4 km2). Holy Island has a similar landscape, with a rugged north and west coast and beaches to the east and south. The county is surrounded by smaller islands; several, including South Stack and Puffin Island, are home to seabird colonies. Large parts of the county's coastline have been designated an Area of Outstanding Natural Beauty.

 

The county has many prehistoric monuments, such as Bryn Celli Ddu burial chamber. In the Middle Ages the area was part of the Kingdom of Gwynedd and native Principality of Wales, and the ruling House of Aberffraw maintained courts (Welsh: llysoedd) at Aberffraw and Rhosyr. After Edward I's conquest of Gwynedd he built the castle at Beaumaris, which forms part of the Castles and Town Walls of King Edward in Gwynedd World Heritage Site. The Menai Strait to the mainland is spanned by the Menai Suspension Bridge, designed by Thomas Telford in 1826, and the Britannia Bridge, originally designed by Robert Stephenson in 1850.

 

The history of the settlement of the local people of Anglesey starts in the Mesolithic period. Anglesey and the UK were uninhabitable until after the previous ice age. It was not until 12,000 years ago that the island of Great Britain became hospitable. The oldest excavated sites on Anglesey include Trwyn Du (Welsh: Black nose) at Aberffraw. The Mesolithic site located at Aberffraw Bay (Porth Terfyn) was buried underneath a Bronze Age 'kerb cairn' which was constructed c. 2,000 BC. The bowl barrow (kerb cairn) covered a material deposited from the early Mesolithic period; the archeological find dates to 7,000 BC. After millennia of hunter-gather civilisation in the British Isles, the first villages were constructed from 4000 BC. Neolithic settlements were built in the form of long houses, on Anglesey is one of the first villages in Wales, it was built at Llanfaethlu. Also an example permanent settlement on Anglesey is of a Bronze Age built burial mound, Bryn Celli Ddu (English: Dark Grove Hill). The mound started as a henge enclosure around 3000 BC and was adapted several times over a millennium.

 

There are numerous megalithic monuments and menhirs in the county, testifying to the presence of humans in prehistory. Plas Newydd is near one of 28 cromlechs that remain on uplands overlooking the sea. The Welsh Triads claim that the island of Anglesey was once part of the mainland.

 

After the Neolithic age, the Bronze Age began (c. 2200 BC – 800 BC). Some sites were continually used for thousands of years from original henge enclosures, then during the Iron Age, and also some of these sites were later adapted by Celts into hillforts and finally were in use during the Roman period (c. 100 AD) as roundhouses. Castell Bryn Gwyn (English: White hill castle, also called Bryn Beddau, or the "hill of graves") near Llanidan, Anglesey is an example of a Neolithic site that became a hillfort that was used until the Roman period by the Ordovices, the local tribe who were defeated in battle by a Roman legion (c. 78 AD). Bronze Age monuments were also built throughout the British Isles. During this period, the Mynydd Bach cairn in South-west Anglesey was being used. It is a Beaker period prehistoric funerary monument.

 

During the Iron Age the Celts built dwellings huts, also known as roundhouses. These were established near the previous settlements. Some huts with walled enclosures were discovered on the banks of the river (Welsh: afon) Gwna near. An example of a well-preserved hut circle is over the Cymyran Strait on Holy Island. The Holyhead Mountain Hut Circles (Welsh: Tŷ Mawr / Cytiau'r Gwyddelod, Big house / "Irishmen's Huts") were inhabited by ancient Celts and were first occupied before the Iron Age, c. 1000 BC. The Anglesey Iron Age began after 500 BC. Archeological research discovered limpet shells which were found from 200 BC on a wall at Tŷ Mawr and Roman-era pottery from the 3rd to 4th centuries AD. Some of these huts were still being used for agricultural purposes as late as the 6th century. The first excavation of Ty Mawr was conducted by William Owen Stanley of Penrhos, Anglesey (son of Baron Stanley of Alderley).

 

Historically, Anglesey has long been associated with the druids. The Roman conquest of Anglesey began in 60 CE when the Roman general Gaius Suetonius Paulinus, determined to break the power of the druids, attacked the island using his amphibious Batavian contingent as a surprise vanguard assault and then destroyed the shrine and the nemeta (sacred groves). News of Boudica's revolt reached him just after his victory, causing him to withdraw his army before consolidating his conquest. The island was finally brought into the Roman Empire by Gnaeus Julius Agricola, the Roman governor of Britain, in AD 78. During the Roman occupation, the area was notable for the mining of copper. The foundations of Caer Gybi, a fort in Holyhead, are Roman, and the present road from Holyhead to Llanfairpwllgwyngyll was originally a Roman road. The island was grouped by Ptolemy with Ireland ("Hibernia") rather than with Britain ("Albion").

 

After the Roman departure from Britain in the early 5th century, pirates from Ireland (Picts) colonised Anglesey and the nearby Llŷn Peninsula. In response to this, Cunedda ap Edern, a Gododdin warlord from Scotland, came to the area and began to drive the Irish out. This was continued by his son Einion Yrth ap Cunedda and grandson Cadwallon Lawhir ap Einion; the last Irish invaders were finally defeated in battle in 470.

 

During the 9th century, King Rhodri Mawr unified Wales and separated the country into at least 3 provinces between his sons. He gave Gwynedd to his son, Anarawd ap Rhodri, who founded the medieval Welsh dynasty, The House of Aberffraw on Anglesey, also his other son Cadell founded House of Dinefwr in Deheubarth, and another son, Merfyn ruled Powys (where the House of Mathrafal emerged). The island had a good defensive position, and so Aberffraw became the site of the royal court (Welsh: Llys) of the Kingdom of Gwynedd. Apart from devastating Danish raids in 853 and 968 in Aberffraw, it remained the capital until the 13th, after Rhodri Mawr had moved his family seat from Caernarfon and built a royal palace at Aberffraw in 873. This is when improvements to the English navy made the location indefensible. Anglesey was also briefly the most southerly possession of the Norwegian Empire.[citation needed]

 

After the Irish, the island was invaded by Vikings — some raids were noted in famous sagas (see Menai Strait History) such as the Jómsvíkinga— and by Saxons, and Normans, before falling to Edward I of England in the 13th century. The connection with the Vikings can be seen in the name of the island. In ancient times it was called "Maenige" and received the name "Ongulsey" or Angelsoen, from where the current name originates.

 

Anglesey (with Holy Island) is one of the 13 historic counties of Wales. In medieval times, before the conquest of Wales in 1283, Môn often had periods of temporary independence, when frequently bequeathed to the heirs of kings as a sub-kingdom of Gwynedd, an example of this was Llywelyn ap Iorwerth (Llywelyn I, the Great c. 1200s) who was styled the Prince of Aberffraw. After the Norman invasion of Wales was one of the last times this occurred a few years after 1171, after the death of Owain Gwynedd, when the island was inherited by Rhodri ab Owain Gwynedd, and between 1246 and about 1255 when it was granted to Owain Goch as his share of the kingdom. After the conquest of Wales by Edward I, Anglesey became a county under the terms of the Statute of Rhuddlan of 1284. Hitherto it had been divided into the cantrefi of Aberffraw, Rhosyr and Cemaes.

 

During 1294 as a rebellion of the former house of Aberffraw, Prince Madog ap Llywelyn had attacked King Edward I's castles in North Wales. As a direct response, Beaumaris Castle was constructed to control Edward's interests in Anglesey, however, by the 1320s the build was abandoned and never complete. The castle was besieged by Owain Glyndŵr in the early 15th century. It was ruinous by 1609, however, the 6th Viscount Bulkeley had purchased the castle from Crown the in 1807 and it has been open to the public under the guardianship of the Crown ever since 1925.

 

The Shire Hall in Llangefni was completed in 1899. During the First World War, the Presbyterian minister and celebrity preacher John Williams toured the island as part of an effort to recruit young men as volunteers. The island's location made it ideal for monitoring German U-Boats in the Irish Sea, with half a dozen airships based at Mona. German POWs were kept on the island. By the end of the war, some 1,000 of the island's men had died on active service.

 

In 1936 the NSPCC opened its first branch on Anglesey.

 

During the Second World War, Anglesey received Italian POWs. The island was designated a reception zone, and was home to evacuee children from Liverpool and Manchester.

 

In 1971, a 100,000 ton per annum aluminum smelter was opened by Rio Tinto Zinc Corporation and British Insulated Callender's Cables with Kaiser Aluminum and Chemical Corporation as a 30 per cent partner.

 

In 1974, Anglesey became a district of the new county of Gwynedd. The Local Government (Wales) Act 1994 abolished the 1974 county and the five districts on 1 April 1996, and Anglesey became a separate unitary authority. In 2011, the Welsh Government appointed a panel of commissioners to administer the council, which meant the elected members were not in control. The commissioners remained until an election was held in May 2013, restoring an elected Council. Before the period of direct administration, there had been a majority of independent councillors. Though members did not generally divide along party lines, these were organised into five non-partisan groups on the council, containing a mix of party and independent candidates. The position has been similar since the election, although the Labour Party has formed a governing coalition with the independents.

 

Brand new council offices were built at Llangefni in the 1990s for the new Isle of Anglesey County Council.

 

Anglesey is a low-lying island with low hills spaced evenly over the north. The highest six are Holyhead Mountain, 220 metres (720 ft); Mynydd Bodafon, 178 metres (584 ft); Mynydd Llaneilian, 177 metres (581 ft); Mynydd y Garn, 170 metres (560 ft); Bwrdd Arthur, 164 metres (538 ft); and Mynydd Llwydiarth, 158 metres (518 ft). To the south and south-east, the island is divided from the Welsh mainland by the Menai Strait, which at its narrowest point is about 250 metres (270 yd) wide. In all other directions the island is surrounded by the Irish Sea. At 676 km2 (261 sq mi), it is the 52nd largest island of Europe and just five km2 (1.9 sq mi) smaller than the main island of Singapore.

 

There are a few natural lakes, mostly in the west, such as Llyn Llywenan, the largest on the island, Llyn Coron, and Cors Cerrig y Daran, but rivers are few and small. There are two large water supply reservoirs operated by Welsh Water. These are Llyn Alaw to the north of the island and Llyn Cefni in the centre of the island, which is fed by the headwaters of the Afon Cefni.

 

The climate is humid (though less so than neighbouring mountainous Gwynedd) and generally equable thanks to the Gulf Stream. The land is of variable quality and has probably lost some fertility. Anglesey has the northernmost olive grove in Europe and presumably in the world.

 

The coast of the Isle of Anglesey is more populous than the interior. The largest community is Holyhead, which is located on Holy Island and had a population of 12,103 at the 2021 United Kingdom census. It is followed by Amlwch (3,697), Llanfair-Mathafarn-Eithaf (3,085), and Menai Bridge (3,046), all located on the coast of the island of Anglesey. The largest community in the interior of Anglesey is Llangefni (5,500), the county town; the next-largest is Llanfihangel Ysgeifiog (1,711).

 

Beaumaris (Welsh: Biwmares) in the east features Beaumaris Castle, built by Edward I during his Bastide campaign in North Wales. Beaumaris is a yachting centre, with boats moored in the bay or off Gallows Point. The village of Newborough (Welsh: Niwbwrch), in the south, created when townsfolk of Llanfaes were relocated for the building of Beaumaris Castle, includes the site of Llys Rhosyr, another court of medieval Welsh princes featuring one of the United Kingdom's oldest courtrooms. The centrally localted Llangefni is the island's administrative centre. The town of Menai Bridge (Welsh: Porthaethwy) in the south-east, expanded to accommodate workers and construction when the first bridge to the mainland was being built. Hitherto Porthaethwy had been one of the main ferry ports for the mainland. A short distance from the town lies Bryn Celli Ddu, a Stone Age burial mound.

 

Nearby is the village with the longest name in Europe, Llanfairpwllgwyngyllgogerychwyrndrobwllllantysiliogogogoch, and Plas Newydd, ancestral home of the Marquesses of Anglesey. The town of Amlwch lies in the north-east of the island and was once largely industrialised, having grown in the 18th century to support a major copper-mining industry at Parys Mountain.

 

Other settlements include Cemaes, Pentraeth, Gaerwen, Dwyran, Bodedern, Malltraeth and Rhosneigr. The Anglesey Sea Zoo is a local attraction offering looks at local marine wildlife from common lobsters to congers. All fish and crustaceans on display are caught round the island and placed in habitat reconstructions. The zoo also breeds lobsters commercially for food and oysters for pearls, both from local stocks. Sea salt (Halen Môn, from local sea water) is produced in a facility nearby, having formerly been made at the Sea Zoo site.

 

Landmarks

Anglesey Motor Racing Circuit

Anglesey Sea Zoo near Dwyran

Bays and beaches – Benllech, Cemlyn, Red Wharf, and Rhosneigr

Beaumaris Castle and Gaol

Cribinau – tidal island with 13th-century church

Elin's Tower (Twr Elin) – RSPB reserve and the lighthouse at South Stack (Ynys Lawd) near Holyhead

King Arthur's seat – near Beaumaris

Llanfairpwllgwyngyll, one of the longest place names in the world

Malltraeth – centre for bird life and home of wildlife artist Charles Tunnicliffe

Moelfre – fishing village

Parys Mountain – copper mine dating to the early Bronze Age

Penmon – priory and dovecote

Skerries Lighthouse – at the end of a low piece of submerged land, north-east of Holyhead

Stone Science Museum – privately run fossil museum near Pentraeth

Swtan longhouse and museum – owned by the National Trust and managed by the local community

Working windmill – Llanddeusant

Ynys Llanddwyn (Llanddwyn Island) – tidal island

St Cybi's Church Historic church in Holyhead

 

Born in Anglesey

Tony Adams – actor (Anglesey, 1940)

Stu Allan – radio and club DJ

John C. Clarke – U.S. state politician (Anglesey, 1831)

Grace Coddington – creative director for US Vogue (Anglesey, 1941)

Charles Allen Duval – artist and writer (Beaumaris, 1810)

Dawn French – actress, writer, comedian (Holyhead, 1957)

Huw Garmon – actor (Anglesey, 1966)

Hugh Griffith – Oscar-winning actor (Marianglas, 1912)

Elen Gwdman – poet (fl. 1609)

Meinir Gwilym – singer and songwriter (Llangristiolus, 1983)

Owain Gwynedd – royal prince (Anglesey, c. 1100)

Hywel Gwynfryn – radio and TV personality (Llangefni, 1942)

Aled Jones – singer and television presenter (Llandegfan, 1970)

John Jones – amateur astronomer (Bryngwyn Bach, Dwyran 1818 – Bangor 1898); a.k.a. Ioan Bryngwyn Bach and Y Seryddwr

William Jones – mathematician (Llanfihangel Tre'r Beirdd, 1675)

Julian Lewis Jones – actor, known for his portrayal of Karl Morris on the Sky 1 comedy Stella (Anglesey, 1968)

John Morris-Jones – grammarian and poet (Llandrygarn, 1864)

Edward Owen – 18th-century artist, notable for letters documenting life in London's art scene

Goronwy Owen – 18th-century poet (Llanfair-Mathafarn-Eithaf, 1723)

Osian Roberts – association football player and manager (Bodffordd)

Tecwyn Roberts – NASA aerospace engineer and Director of Networks at Goddard Space Flight Center (Llanddaniel Fab, 1925)

Hugh Owen Thomas – pioneering orthopaedic surgeon (Anglesey, 1836)

Ifor Owen Thomas – operatic tenor, photographer and artist (Red Wharf Bay, 1892)

Sefnyn – medieval court poet

Owen Tudor – grandfather of Henry Tudor, married the widow of Henry V, which gave the Tudor family a claim on the English throne (Anglesey, c. 1400).

Kyffin Williams – landscape painter (Llangefni, 1918)

William Williams – recipient of the Victoria Cross (Amlwch, 1890)

Andy Whitfield – actor (Amlwch, 1971)

Gareth Williams – employee of Britain's GCHQ signals intelligence agency (Anglesey, 1978)

The aircraft flight configuration for an airdrop mission is displayed on board a C-130J Hercules at Little Rock Air Force Base, Ark. on Nov. 16, 2016. Stationed at Little Rock AFB, the 19th Aerospace Medicine Squadron’s High Altitude Airdrop Mission Support team provides in-flight physiological support to aircrews, special operations forces, high altitude parachutists, and other DoD agencies that perform unpressurized airdrop operations at 20,000 feet mean sea level and above. (U.S. Air Force photo/Tech Sgt. Brandon Shapiro)

This model was specifically built for the Arawasi Wild Eagles blog's "Hayabusa Model Contest" in April/May 2017 (arawasi-wildeagles.blogspot.de/2017/03/japanese-aircraft-...) - and it is the guesstimate, based on a conversion set and a vague frontal picture of a real aircraft.

 

Inspiration struck when I came across a Rising Decals conversion (from the Czech Republic)set for an experimental Ki43 with wooden, retractable skis - tested in Manchuria in 1944. The set comes with finely crafted and moulded resin skis, plus a decal sheet for the rather bleak aircraft in natural metal finish. Anyway, I found the idea worth to become an entry, and took action.

 

The kit and its assembly:

The basis is the venarable 1:72 Hasegawa kit of the Ki43-II, a simple kit with good detail and fit, even though you get raised (though very fine) panel lines. The kit was basically built OOB, with only some detail additions in the cockpit, and I modified the wings and lower fuselage in so far that the "butterfly flaps" were added in extended position.

 

Concerning the ski landing gear, I did some legwork, and eventually found a Ki43-II with the same landing gear arrangement as the conversion set, but it also featured a four-bladed propeller!

The wheeled landing gear was simply replaced by the resin struts from the conversion set, the skis are separate pieces that fit neatly into each other and into the kit.

The propeller was scratched from the three OOB blades, plus a trimmed donor blade. The spinner is the front end of a German 250 kg bomb. Inside of the engine, a styrene tube was added as propeller mount, which received a long metal axis.

A venturi tube was added under the fuselage, too, and the canopy separated into two pieces for better display.

The frontal benchmark picture of "my" Ki43-II shows the aircraft in clean configuration, but I decided to use/add the underwing tanks in order to avoid filling the respective holes in the wings - and it makes the aircraft look more interesting, IMHO.

  

Painting and markings:

Concerning the aircraft's livery, I basically stuck to the machine depicted in the conversion set and on the few pictures of such machines - even though the info sheet states that "markings are uncertain".

Anyway, I went the suggested overall NMF route with grey-green fabric (individually mixed from Humbrol 90 and 155) on all rudder surfaces. As a personal note, and as an interpretation of the benchmark photograph of the Ki43-II I tried to build, the model received a worn and flaking cowling in IJA Green and Grey. The latter was also used for the drop tanks, with red primer showing through the tanks' front end. A black anti glare panel was added in front of and behind the canopy.

 

The cockpit interior was painted, based on Hasegawa's recommendations, in a greenish brown tone (a mix of Revell 45 and 16). The landing gear wells and the interior of the flaps was painted with Aodake Iro - and instead of mixing a metallic blue tone as a single tone I rather laid down an Aluminum base and added a clear, greenish blue lacquer on top - just like the real thing. The deep yellow ID markings on the wings' leading edges were painted with RAL 1028 (Lufthansa Gelb, Revell 310).

 

The skis appear to be massive wood pieces, and they were painted accordingly with a wet-in-wet mix of red brown and cream, for a streaky look, mimicking the wooden structure.

 

After basic painting (a basic coat with acrylic Aluminum, Revell 99), everything done with brushes and minimal masking, the kit received a light black ink wash, in order to emphasize engravings. For some "depth" effect, panels were post-shaded with Polished Aluminum Metallizer (Humbrol 27002) on top of the acrylic Aluminum base. During the polishing process with a piece of soft cloth, some grinded graphite was rubbed over all surfaces, too, creating a slightly worn and uneven look. This little trick also enhances the metallic shine of the surface, making it look less "painted". Graphite was also used in order to simulate light exhaust stains on the Hayabusa's flanks.

 

Once the (very thin and delicate) decals were in place, they received a light treatment with Aluminium and sand paper, in order to simulate some wear on the aircraft's surface. Finally, everything was sealed with a coat of semi-matt acrylic varnish, just the rudders and the anti-glare panels received a completely matt coat.

  

A quick build, done in less than three days from sprues to photo shots. Anyway, the model should rather be regarded as fictional, since my information basis has been rather corny and relied on very limited references. But I am, nevertheless, happy with the result, and I hope the model conveys the original idea of the converted Ki43 with skis?

+++ DISCLAIMER +++

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

  

The Supermarine Spitfire was a British single-seat fighter aircraft used by the Royal Air Force and other Allied countries before, during and after World War II. Many variants of the Spitfire were built, using several wing configurations, and it was produced in greater numbers than any other British aircraft. It was also the only British fighter produced continuously throughout the war.

 

The Spitfire was designed as a short-range, high-performance interceptor aircraft by R. J. Mitchell, chief designer at Supermarine Aviation Works, which operated as a subsidiary of Vickers-Armstrong from 1928. Mitchell pushed the Spitfire's distinctive elliptical wing designed by Beverley Shenstone to have the thinnest possible cross-section, helping give the aircraft a higher top speed than several contemporary fighters, including the Hawker Hurricane. Mitchell continued to refine the design until his death in 1937, whereupon his colleague Joseph Smith took over as chief designer, overseeing the Spitfire's development through its multitude of variants and many sub-variants. These covered the Spitfire in development from the Merlin to Griffon water-cooled inline engines, the high-speed photo-reconnaissance variants and the different wing configurations.

 

One exception was the Spitfire Mk. X: it was the only variant powered by a radial engine, and it looked quite different from its sleek Merlin-powered brethren. Early in its development, the Merlin engine's lack of fuel injection meant that Spitfires and Hurricanes, unlike the Bf 109E, were unable to simply nose down into a steep dive. This meant a Luftwaffe fighter could simply "bunt" into a high-power dive to escape an attack, leaving the Spitfire behind, as its fuel was forced out of the carburetor by negative "g". An alternative engine was to solve this issue. Another factor that suggested an air-cooled engine were theatres of operations in the Far East, primarily India: the hot and humid climate was expected to be a severe operational problem for the liquid-cooled Merlin. As a further side effect a radial engine was expected to be easier to maintain under these conditions than the Merlin.

 

The project of a radial-powered Spitfire variant was eventually launched in late 1940. The choice for the power unit fell on a Bristol Taurus II 14-Cylinder engine, which had an appreciable small diameter, was available in ample numbers and had about the same power output as the early Merlin variants used in the Spitfire Mk. I and II (1.030 hp/740kW). In order to save time and keep the radial engine variant as close as possible to the Spitfire V design, the production type of that era. The new type’s structure and fuselage were only adapted to a minimum to allow the bulkier power unit and its periphery to be taken. The fuselage was widened in front of the cockpit section, a new engine mount was integrated and the Merlin’s radiator bath and respective piping were removed. The oil cooler under the port wing was retained, though, and the Taurus engine was from the start outfitted with dust filters, so that all resulting Spitfire Mk. Xs left the factory tropicalized. Like the Spitfire Mk. V, different wing armaments were available, e.g. an “A” wing with eight .303 in machine guns and a “B” wing with two 20 mm cannon and four machine guns.

 

The first Spitfire Mk. Xs, finally outfitted with a more powerful Taurus VI engine, were delivered to homeland RAF units for evaluation from May 1941 onwards. From the start, the radial-powered Spitfire proved to be inferior to the Merlin-powered variants - even to the early Mk. Is – and they were no match to the modern German fighters, especially at high altitude. As a consequence many Mk. Xs received clipped wing tips for better roll characteristics at low altitude (receiving an additional “L.F.” designation), but this did not significantly improve the type’s overall mediocre performance. Only a few Mk. Xs were actually employed by front line units, most were quickly relegated to training units. Later production aircraft were immediately shipped to the Far East or to units in Northern Africa, where they could be used more effectively.

A few machines were also delivered to Egypt (30), the Netherlands (12 for the East Indies NL-KNIL, which eventually ended up in RAAF service) and Turkey (24). In 1942, many machines still based in Great Britain were handed over to the USAAF, being either used for USAAF pilot and conversion training, or they were allocated to the Northern Africa invasion force during Operation Torch.

 

Since the Taurus-powered Spitfire turned out to be quite ineffective (it was no good either in the fighter or in an alternative ground attack role and 20 mph slower than the comparable Mk. V), production was already stopped in late 1942 after 353 aircraft. At the same time, the Spitfire Mk. IX with a much more powerful Merlin engine entered service, and all resources were immediately allocated to this more potent fighter variant and the idea of the Spitfire with a radial engine was ultimately dropped. Since the Taurus-powered type was quickly phased out of frontline service, the designation was later re-used for a pressurized high-altitude photo reconnaissance variant of the Spitfire, the PR.X, of which only 16 machines were built.

  

General characteristics:

Crew: one pilot

Length: 29 ft 6 in (9.00 m)

Wingspan: 32 ft 2 in (9.80 m)

Height: 11 ft 5 in (3.86 m)

Wing area: 242.1 ft2 (22.48 m²)

Airfoil: NACA 2213 (root)

NACA 2209.4 (tip)

Empty weight: 5,065 lb (2,297 kg)

Loaded weight: 6,622 lb (3,000 kg)

Max. takeoff weight: 6,700 lb (3,039 kg)

 

Powerplant:

1× Bristol Taurus VI 14-Cylinder sleeve valve radial engine, 1.130 hp (830 kW)

 

Performance:

Maximum speed: 350 mph (312 kn, 565 km/h)

Combat radius: 410 nmi (470 mi/756 km)

Ferry range: 991 nmi (1,135 mi/1,827 km)

Service ceiling: 36,500 ft (11,125 m)

Rate of climb: 2,535 ft/min (12.9 m/s)

Wing loading: 27.35 lb/ft2 (133.5 kg/m²)

Power/mass: 0.22 hp/lb (0.36 kW/kg)

 

Armament:

2× 20 mm Hispano Mk II with 60 RPG

4× .303 in Browning Mk II machine guns with 350 RPG

  

The kit and its assembly:

My third contribution to the “RAF Centenary” Group Build at whatifmodelers.com, and the next one in chronological order. This one was spawned by the simple thought of “What would a Spitfire with a radial engine look like…?”. I have seen this stunt done in the form of a Fw190/Spitfire kitbash – nice result, but it did IMHO just not look like a “real” Spitfire with a radial engine, rather like an Fw 190 with elliptical wings. And the fact that I had already successfully transplanted a Centaurus engine onto a P-51 airframe made me feel positive that the stunt could be done!

 

Consequently, the conversion was pretty straightforward. The basis is a Revell 1:72 Spitfire VB (1996 mold), which was – except for the nose section – taken OOB. A simple, nice kit, even though it comes with some flaws, like a depression at the rear of the wing/fuselage intersection and the general need for PSR – not much, but I expected a better fit for such a relatively young mold?

 

For the engine, I used a personal replacement favorite, the cowling and the engine block from a Mitsubishi A6M2 “Zero” (Hasegawa). The Nakajima Sakae radial engine has a relatively small diameter, so that it serves well as a dummy for the compact Bristol Taurus engine – a replacement I have already used for a radial-powered Westland Whirlwind. The other benefit of the small diameter is that it is relatively easy to blend the round front end into the oval and very slender fuselage of the early Spitfire airframe. This was realized through massive body sculpting from scratch with 2C putty, widening the area in front of the cockpit and expanding its width to match the cowling – I guess that real life engineers would have followed a similar, simple path.

 

Since the radial engine would not need a radiator, I simple omitted this piece (cut out from the single piece lower wing half) and faired the respective underwing area over with a piece of styrene sheet and PSR. The asymmetrical oil cooler was retained, though. The propeller is a replacement from the scrap box, with a smaller diameter spinner and more slender blades which better suit the open cowling.

 

Since the Taurus had its best performance at low altitudes, I used the Revell kit’s OOB option of clipped wing tips – a move that makes the aircraft look much faster, esp. with the new, deeper nose section.

  

Painting and markings:

I did not want classic RAF markings, but still keep the model well within the Centenary GB confines. The original plan had been a classic Dark Green/Ocean Grey livery, which all Spitfire’s in USAAF service and based in the UK received. But I rather wanted to create a frontline aircraft, operated during Operation Torch in late 1942/early 1943 with American roundels – and the grey/green look would not look plausible on a machine taking part in the North African campaign. In fact, any Spitfire with American roundels I found that was used in North Africa carried the RAF Tropical Scheme in Dark Earth/Middle Stone. And, AFAIK, during Operation 'Torch' all British aircraft received American markings in the hope that the Vichy French, who were anti-British due to them bombing their ships in 1940, would switch to the allied cause. They were supposed to think that the Americans would be invading, not British troops as well. So I eventually switched to the classic Tropical Scheme (using Humbrol 29 and Modelmaster 2052 as basic tones), and it does not look bad at all - even though the yellow trim around the roundels does not stand out as much as on a Grey/Green aircraft.

 

Typically, the RAF codes were retained, as well as – at least during the early phases of Operation Torch – the RAF fin flash. A little personal twist is the pale blue (Humbrol 23, Duck Egg Blue) underside of the aircraft, instead of the typical Azure Blue. The rationale behind is that the Tropical Scheme was originally designed with Sky undersides, and the blue shades were later modifications after initial field experience.

The red spinner is a typical Northern Africa marking, and found on many 5th FS aircraft.

 

The interior (cockpit, landing gear wells) was painted with RAF Cockpit Green (Modelmaster), while wheels and struts became light grey.

 

As a standard procedure, the kit received a light black ink wash and a post shading treatment.

 

The decals were puzzled together from various sheets and sources, the design benchmark was a real USAAF Spitfire Vb from Operation Torch, though. The code letters were taken from an Xtradecal sheet, the roundels come from a Carpena Spitfire sheet, even though I placed American markings in all six positions – the roundels without yellow trim under the wings were taken from a Hobby Boss F6F sheet.

The serial number comes from the Revell kit’s OOB sheet, because it fits perfectly into the kit’s intended time frame. The nose art comes from a P-38 sheet (PrintScale) – not a typical feature for an RAF Spitfire, but a frequent personal decoration among USAAF machines during Operation Torch (e.g. on P-40s).

The Allied yellow ID markings on the wings’ leading edges, which were typically carried by Operation Torch Spitfires, too, were created with generic yellow decal sheet (TL Modellbau), while the maroon machine gun nozzle covers are part of Revell’s OOB sheet.

 

Finally, the kit received some soot stains around gun and exhaust nozzles, and was finally sealed with matt acrylic varnish.

  

A bold experiment, and it turned out well. The Zero’s cowling has the perfect diameter for this transplant, and the scratch-sculpted new front fuselage section blends well with the new engine – the whole thing really looks intentional! I am just not certain if the resulting aircraft still deserves the “Spitfire” designation? Even though only the engine was changed, the aircraft looks really different and has a Ki-43ish aura? I guess that a dark green livery and some hinomaru would also look great and pretty plausible?

 

A quick snap for some discussions on my '2nd backup' kit and configs. The main setup is the top left of EOSM, 11-22mm ultra wide, E2 GPS unit and Finder/Scope attached to the back. The other shots are using the EF adapter with some of my Canon 5D3 lenses on. The Rokinon 8mm is interesting as it gives a very useful full frame 12mm lens with moderate distortion

Based on the headlight configuration, the radiator grill design and cab window design, I am guessing that this is a Pickup truck from around 1940. Observed in the mountains of Colorado

Image - Copyright 2020 Alan Vernon

 

Languishing at the back of the Depot is Ballina Based Leyland Leopard E8(CZA668).

Converted into a Ambulance Configuration These vehicles were used to bring disabled pilgrims from the railway station at Claremorris to the shrine at Knock. After some years out of use E8 was brought to Dromod for preservation in September 1994.

Canon EOS 5D mark II

Nikon APO-Nikkor 360mm F9 (for Large Format Process Lens)

  

System configuration--------------------------------------------------------

Canon EOS 5D mark II

U.N. Screw Metal Hood No.4 + No.5 : Depth 110mm

U.N. Metal Step Up Ring Φ72mm to Φ88mm

Step Up Ring Φ62mm to Φ72mm

Step Up Ring Φ60mm to Φ62mm

Rain Photo Tech Co, Ltd. Macro Extension Tube #.3 : 25mm for EOS (Φ60mm)

Rain Photo Tech Co, Ltd. Macro Extension Tube #.2 : 14mm for EOS (Φ60mm)

Rain Photo Tech Co, Ltd. Macro Extension Tube #.3 : 25mm for EOS (Φ60mm)

Total Hood Depth : 20cm

Step Up Ring Φ52mm to Φ60mm

Step Down Ring Φ67mm to Φ52mm

Kenko Protect Filter Φ67mm

Nikon APO-Nikkor 360mm F9 (for Large Format Process Lens) M72 Screw Mount

M72 - Nikon F Mount Change Adaptor

Nikon PN-11 Automatic Extension Ring : 52.5mm

Kathay Technology Industrial Co., Ltd. Lens Macro Fold Bellows (KLMB-1)

for Nikon F is used

Nikon PK-13 Automatic Extension Ring : 27.5mm

Nikon PN-1 Automatic Extension Ring : 52.5mm (for Revolving function used.)

Nikon PK-13 Automatic Extension Ring : 27.5mm

Nikon F - EOS Mount Change Adaptor Ring

BORG [5555] Hip Support HP-1 is used.

  

Photo by : SONY SO906i (Cellular Phone Camera)

 

ベローズは中華製で US $35.00 でした。レンズ本体は大きさのわりに軽いのですが、望遠レンズではなくて、超長焦点レンズな為、金属製の筒が沢山必要になりまして、案外とかさばります。撮影結果は大変良い物でしたが、利便性を追求する人だと駄目なシステムです。私はコンポーネント癖があるので楽しみながら

組み立てて撮影しています。

The Supermarine Spitfire is a British single-seat fighter aircraft that was used by the Royal Air Force and many other Allied countries during and after the Second World War. The Spitfire was built in many variants, using several wing configurations, and was produced in greater numbers than any other British aircraft. It was also the only British fighter to be in continuous production throughout the war. The Spitfire continues to be a popular aircraft, with approximately 55 Spitfires being airworthy, while many more are static exhibits in aviation museums all over the world.

 

The Spitfire was designed as a short-range, high-performance interceptor aircraft by R. J. Mitchell, chief designer at Supermarine Aviation Works (which operated as a subsidiary of Vickers-Armstrong from 1928). In accordance with its role as an interceptor, Mitchell designed the Spitfire's distinctive elliptical wing to have the thinnest possible cross-section; this thin wing enabled the Spitfire to have a higher top speed than several contemporary fighters, including the Hawker Hurricane. Mitchell continued to refine the design until his death from cancer in 1937, whereupon his colleague Joseph Smith took over as chief designer, overseeing the development of the Spitfire through its multitude of variants.

 

During the Battle of Britain (July–October 1940), the Spitfire was perceived by the public to be the RAF fighter, though the more numerous Hawker Hurricane shouldered a greater proportion of the burden against the Luftwaffe. However, because of its higher performance, Spitfire units had a lower attrition rate and a higher victory-to-loss ratio than those flying Hurricanes.

 

After the Battle of Britain, the Spitfire superseded the Hurricane to become the backbone of RAF Fighter Command, and saw action in the European, Mediterranean, Pacific and the South-East Asian theatres. Much loved by its pilots, the Spitfire served in several roles, including interceptor, photo-reconnaissance, fighter-bomber and trainer, and it continued to serve in these roles until the 1950s. The Seafire was a carrier-based adaptation of the Spitfire which served in the Fleet Air Arm from 1942 through to the mid-1950s. Although the original airframe was designed to be powered by a Rolls-Royce Merlin engine producing 1,030 hp (768 kW), it was strong enough and adaptable enough to use increasingly powerful Merlin and, in later marks, Rolls-Royce Griffon engines producing up to 2,340 hp (1,745 kW); as a consequence of this the Spitfire's performance and capabilities improved, sometimes dramatically, over the course of its life.

 

Mk V (Types 331, 349 & 352)

 

Spitfire LF.Mk VB, BL479, flown by Group Captain M.W.S Robinson, station commander of RAF Northolt, August 1943. This Spitfire has the wide bladed Rotol propeller, the internal armoured windscreen and "clipped" wings.

Late in 1940, the RAF predicted that the advent of the pressurised Junkers Ju 86P bomber series over Britain would be the start of a new sustained high altitude bombing offensive by the Luftwaffe, in which case development was put in hand for a pressurised version of the Spitfire, with a new version of the Merlin (the Mk VI). It would take some time to develop the new fighter and an emergency stop-gap measure was needed as soon as possible: this was the Mk V.

 

The basic Mk V was a Mk I with the Merlin 45 series engine. This engine delivered 1,440 hp (1,074 kW) at take-off, and incorporated a new single-speed single-stage supercharger design. Improvements to the carburettor also allowed the Spitfire to use zero gravity manoeuvres without any problems with fuel flow. Several Mk I and Mk II airframes were converted to Mk V standard by Supermarine and started equipping fighter units from early 1941. The majority of the Mk Vs were built at Castle Bromwich.

 

The VB became the main production version of the Mark Vs. Along with the new Merlin 45 series the B wing was fitted as standard. As production progressed changes were incorporated, some of which became standard on all later Spitfires. Production started with several Mk IBs which were converted to Mk VBs by Supermarine. Starting in early 1941 the round section exhaust stacks were changed to a "fishtail" type, marginally increasing exhaust thrust. Some late production VBs and VCs were fitted with six shorter exhaust stacks per side, similar to those of Spitfire IXs and Seafire IIIs; this was originally stipulated as applying specifically to VB(trop)s. After some initial problems with the original Mk I size oil coolers, a bigger oil cooler was fitted under the port wing; this could be recognised by a deeper housing with a circular entry. From mid-1941 alloy covered ailerons became a universal fitting.

 

Spitfire VC(trop), fitted with Vokes filters and "disc" wheels, of 417 Squadron RCAF in Tunisia in 1943.

A constant flow of modifications were made as production progressed. A "blown" cockpit hood, manufactured by Malcolm, was introduced in an effort to further increase the pilot's head-room and visibility. Many mid to late production VBs - and all VCs - used the modified, improved windscreen assembly with the integral bullet resistant centre panel and flat side screens introduced with the Mk III. Because the rear frame of this windscreen was taller than that of the earlier model the cockpit hoods were not interchangeable and could be distinguished by the wider rear framing on the hood used with the late-style windscreen.

 

Different propeller types were fitted, according to where the Spitfire V was built: Supermarine and Westland manufactured VBs and VCs used 10 ft 9 in (3.28 m) diameter, 3 bladed de Havilland constant speed units, with narrow metal blades, while Castle Bromwich manufactured VBs and VCs were fitted with a wide bladed Rotol constant speed propeller of either 10 ft 9 in (3.28 m) diameter, with metal blades, or (on late production Spitfires) 10 ft 3 in (3.12 m) diameter, with broader, "Jablo" (compressed wood) blades. The Rotol spinners were longer and more pointed than the de Havilland leading to a 3.5 in (8.9 cm) increase in overall length. The Rotol propellers allowed a modest speed increase over 20,000 ft (6,100 m) and an increase in the service ceiling. A large number of Spitfire VBs were fitted with "gun heater intensifier" systems on the exhaust stacks. These piped additional heated air into the gun bays. There was a short tubular intake on the front of the first stack and a narrow pipe led into the engine cowling from the rear exhaust.

 

The VB series were the first Spitfires able to carry a range of specially designed "slipper" drop tanks which were fitted underneath the wing centre-section. Small hooks were fitted, just forward of the inboard flaps: when the tank was released these hooks caught the trailing edge of the tank, swinging it clear of the fuselage.

 

With the advent of the superb Focke Wulf Fw 190 in August 1941 the Spitfire was for the first time truly outclassed, hastening the development of the "interim" Mk IX. In an effort to counter this threat, especially at lower altitudes, the VB was the first production version of the Spitfire to use "clipped" wingtips as an option, reducing the wingspan to 32 ft 2 in (9.8 m).The clipped wings increased the roll rate and airspeed at lower altitudes. Several different versions of the Merlin 45/50 family were used, including the Merlin 45M which had a smaller "cropped" supercharger impeller and boost increased to +18 lb. This engine produced 1,585 hp (1,182 kW) at 2,750 ft (838 m), increasing the L.F VB's maximum rate of climb to 4720 ft/min (21.6 m/s) at 2,000 ft (610 m).

 

VB Trop of 40 Squadron SAAF fitted with the "streamlined" version of the Aboukir filter, a broad-bladed, 10 ft 3 in (3.12 m) diameter Rotol propeller, and clipped wings.

The Mk VB(trop) (or type 352) could be identified by the large Vokes air filter fitted under the nose; the reduced speed of the air to the supercharger had a detrimental effect on the performance of the aircraft, reducing the top speed by 8 mph (13 km/h) and the climb rate by 600 ft/min (3.04 m/s), but the decreased performance was considered acceptable. This variant was also fitted with a larger oil tank and desert survival gear behind the pilot's seat. A new "desert" camouflage scheme was applied. Many VB(trop)s were modified by 103 MU (Maintenance Unit-RAF depots in which factory fresh aircraft were brought up to service standards before being delivered to squadrons) at Aboukir, Egypt by replacing the Vokes filter with locally manufactured "Aboukir" filters, which were lighter and more streamlined. Two designs of these filters can be identified in photos: one had a bulky, squared off filter housing while the other was more streamlined. These aircraft were usually fitted with the wide blade Rotol propeller and clipped wings.

 

Triumph Spitfire Mk I Roadster

 

The Triumph Spitfire is a small English two-seat sports car, introduced at the London Motor Show in 1962.[3] The vehicle was based on a design produced for Standard-Triumph in 1957 by Italian designer Giovanni Michelotti. The platform for the car was largely based upon the chassis, engine, and running gear of the Triumph Herald saloon, and was manufactured at the Standard-Triumph works at Canley, in Coventry. As was typical for cars of this era, the bodywork was fitted onto a separate structural chassis, but for the Spitfire, which was designed as an open top or convertible sports car from the outset, the ladder chassis was reinforced for additional rigidity by the use of structural components within the bodywork. The Spitfire was provided with a manual hood for weather protection, the design improving to a folding hood for later models. Factory-manufactured hard-tops were also available.

 

The Triumph Spitfire was originally devised by Standard-Triumph to compete in the small sports car market that had opened up with the introduction of the Austin-Healey Sprite. The Sprite had used the basic drive train of the Austin A30/35 in a light body to make up a budget sports car; Triumph's idea was to use the mechanicals from their small saloon, the Herald, to underpin the new project. Triumph had one advantage, however; where the Austin A30 range was of unitary construction, the Herald featured a separate chassis. It was Triumph's intention to cut that chassis down and clothe it in a sports body, saving the costs of developing a completely new chassis / body unit.

 

Italian designer Michelotti—who had already penned the Herald—was commissioned for the new project, and came up with a traditional, swooping body. Wind-up windows were provided (in contrast to the Sprite/Midget, which still featured sidescreens, also called curtains, at that time), as well as a single-piece front end which tilted forwards to offer unrivaled access to the engine. At the dawn of the 1960s, however, Standard-Triumph was in deep financial trouble, and unable to put the new car into production; it was not until the company was taken over by the Leyland organization funds became available and the car was launched. Leyland officials, taking stock of their new acquisition, found Michelotti's prototype hiding under a dust sheet in a corner of the factory and rapidly approved it for production.

 

Spitfire 4 or Mark I (1962-1964)

 

Overview:

Production1962–1964

45,753 made

Powertrain:

Engine1,147 cc (1.1 l) I4

Transmission4-speed manual with optional overdrive on top and third from 1963 onwards

Dimensions:

Curb weight1,568 lb (711 kg) (unladen U.K.-spec)

 

The production car changed little from the prototype, although the full-width rear bumper was dropped in favour of two part-bumpers curving round each corner, with overriders. Mechanicals were basically stock Herald. The engine was an 1,147 cc (1.1 l) 4-cylinder with a pushrod OHV cylinder head and 2 valves per cylinder, mildly tuned for the Spitfire, fed by twin SU carburettors. Also from the Herald came the rack and pinion steering and coil-and-wishbone front suspension up front, and at the rear a single transverse-leaf swing axle arrangement. This ended up being the most controversial part of the car: it was known to "tuck in" and cause violent over steer if pushed too hard, even in the staid Herald. In the sportier Spitfire (and later the 6-cylinder Triumph GT6 and Triumph Vitesse) it led to severe criticism. The body was bolted to a much-modified Herald chassis, the outer rails and the rear outriggers having been removed; little of the original Herald chassis design was left, and the Spitfire used structural outer sills to stiffen its body tub.

 

The Spitfire was an inexpensive small sports car and as such had very basic trim, including rubber mats and a large plastic steering wheel. These early cars were referred to both as "Triumph Spitfire Mark I" and "Spitfire 4", not to be confused with the later Spitfire Mark IV.

 

In UK specification the in-line four produced 63 bhp (47 kW) at 5750 rpm, and 67 lb·ft (91 N·m)of torque at 3500 rpm. This gave a top speed of 92 mph (148 km/h), and would achieve 0 to 60 mph (97 km/h) in 17.3 seconds. Average fuel consumption was 31mpg.

 

For 1964 an overdrive option was added to the 4-speed manual gearbox to give more relaxed cruising. Wire wheels and a hard top were also available.

 

Text regarding the Supermarine Spitfire aeroplane and Triumph Spitfire Roadster has been taken from excerpts of Wikipedia articles on each model.

 

The Supermarine Spitfire Mk VB aircraft and 1962 Triumph Spitfire Mk I road car have been modelled in Lego miniland-scale for Flickr LUGNuts' 79th Build Challenge, - 'LUGNuts goes Wingnuts, ' - featuring automotive vehicles named after, inspired by, or with some relationship to aircraft.

Valentine sunset with Kercam21, Trevor Tutt and Mic Steel

The church dedicated to the Saviour's Configuration ("Metamorfosi tou Sotira") is built in the middle of "Palio Chorio" ("Old Village"). It was constructed in the 16th century (1520) and it has the same architectural style as the other two small churches of the village, that of "Panagia Theotokos" and that of Saint George "Perachoritis". Up until 1994, liturgies were conducted daily since it was considered as the village's main church.

It is a rectangular church of the Basilica style and with elements of the Byzantine style. It can accommodate up to 100-150 faithful. Externally it is made of stone and whitewashed.

The inhabitants built extensions to the church in 1880 and 1960 because the village was continuously growing. When they dug the floor they discovered many pieces of frescoes, which surely came from this church. Indeed, they were able to read the name of the hagiographer who was named Symeon Afxentis. He is known for his frescoes of the "Panagia Theotokos" and "Archangel" churches in the village of Galata.

The icon screen is woodcut, as also are the two Psalters that can be found in the church.

There are various remarkable representations dating back to the 16th and 17th century. The icon screen is of various different chronologies.

www.kakopetriavillage.com/churches.html

 

The settlement of Kakopetria, although mentioned by the mediaeval annalists, existed -at least- since the Frank domination era. The village's region was inhabited around the 6th - 7th century and the various excavations that have been conducted in 1938 around the old village of Kakopetria (in the Ailades venue) prove this. During the excavations a dispenser of an ancient shrine -most probably belonging to the goddess Athena- came to light. A large number of movable findings were found, mainly terra-cotta, many of which depict the goddess Athena, as well as small, limestone, statues and parts of statues and bronze and iron shafts from spearheads and arrows. The findings most probably date back to the Archaic and Classic eras of Cyprus. Other statuettes represent Hercules and are an indication that he was also worshiped in the area along with the goddess Athena. These findings are found in the Archaeological Museum of Nicosia.

en.wikipedia.org/wiki/Kakopetria

 

The Supermarine Spitfire is a British single-seat fighter aircraft that was used by the Royal Air Force and many other Allied countries during and after the Second World War. The Spitfire was built in many variants, using several wing configurations, and was produced in greater numbers than any other British aircraft. It was also the only British fighter to be in continuous production throughout the war. The Spitfire continues to be a popular aircraft, with approximately 55 Spitfires being airworthy, while many more are static exhibits in aviation museums all over the world.

 

The Spitfire was designed as a short-range, high-performance interceptor aircraft by R. J. Mitchell, chief designer at Supermarine Aviation Works (which operated as a subsidiary of Vickers-Armstrong from 1928). In accordance with its role as an interceptor, Mitchell designed the Spitfire's distinctive elliptical wing to have the thinnest possible cross-section; this thin wing enabled the Spitfire to have a higher top speed than several contemporary fighters, including the Hawker Hurricane. Mitchell continued to refine the design until his death from cancer in 1937, whereupon his colleague Joseph Smith took over as chief designer, overseeing the development of the Spitfire through its multitude of variants.

 

During the Battle of Britain (July–October 1940), the Spitfire was perceived by the public to be the RAF fighter, though the more numerous Hawker Hurricane shouldered a greater proportion of the burden against the Luftwaffe. However, because of its higher performance, Spitfire units had a lower attrition rate and a higher victory-to-loss ratio than those flying Hurricanes.

 

After the Battle of Britain, the Spitfire superseded the Hurricane to become the backbone of RAF Fighter Command, and saw action in the European, Mediterranean, Pacific and the South-East Asian theatres. Much loved by its pilots, the Spitfire served in several roles, including interceptor, photo-reconnaissance, fighter-bomber and trainer, and it continued to serve in these roles until the 1950s. The Seafire was a carrier-based adaptation of the Spitfire which served in the Fleet Air Arm from 1942 through to the mid-1950s. Although the original airframe was designed to be powered by a Rolls-Royce Merlin engine producing 1,030 hp (768 kW), it was strong enough and adaptable enough to use increasingly powerful Merlin and, in later marks, Rolls-Royce Griffon engines producing up to 2,340 hp (1,745 kW); as a consequence of this the Spitfire's performance and capabilities improved, sometimes dramatically, over the course of its life.

 

Mk V (Types 331, 349 & 352)

 

Spitfire LF.Mk VB, BL479, flown by Group Captain M.W.S Robinson, station commander of RAF Northolt, August 1943. This Spitfire has the wide bladed Rotol propeller, the internal armoured windscreen and "clipped" wings.

Late in 1940, the RAF predicted that the advent of the pressurised Junkers Ju 86P bomber series over Britain would be the start of a new sustained high altitude bombing offensive by the Luftwaffe, in which case development was put in hand for a pressurised version of the Spitfire, with a new version of the Merlin (the Mk VI). It would take some time to develop the new fighter and an emergency stop-gap measure was needed as soon as possible: this was the Mk V.

 

The basic Mk V was a Mk I with the Merlin 45 series engine. This engine delivered 1,440 hp (1,074 kW) at take-off, and incorporated a new single-speed single-stage supercharger design. Improvements to the carburettor also allowed the Spitfire to use zero gravity manoeuvres without any problems with fuel flow. Several Mk I and Mk II airframes were converted to Mk V standard by Supermarine and started equipping fighter units from early 1941. The majority of the Mk Vs were built at Castle Bromwich.

 

The VB became the main production version of the Mark Vs. Along with the new Merlin 45 series the B wing was fitted as standard. As production progressed changes were incorporated, some of which became standard on all later Spitfires. Production started with several Mk IBs which were converted to Mk VBs by Supermarine. Starting in early 1941 the round section exhaust stacks were changed to a "fishtail" type, marginally increasing exhaust thrust. Some late production VBs and VCs were fitted with six shorter exhaust stacks per side, similar to those of Spitfire IXs and Seafire IIIs; this was originally stipulated as applying specifically to VB(trop)s. After some initial problems with the original Mk I size oil coolers, a bigger oil cooler was fitted under the port wing; this could be recognised by a deeper housing with a circular entry. From mid-1941 alloy covered ailerons became a universal fitting.

 

Spitfire VC(trop), fitted with Vokes filters and "disc" wheels, of 417 Squadron RCAF in Tunisia in 1943.

A constant flow of modifications were made as production progressed. A "blown" cockpit hood, manufactured by Malcolm, was introduced in an effort to further increase the pilot's head-room and visibility. Many mid to late production VBs - and all VCs - used the modified, improved windscreen assembly with the integral bullet resistant centre panel and flat side screens introduced with the Mk III. Because the rear frame of this windscreen was taller than that of the earlier model the cockpit hoods were not interchangeable and could be distinguished by the wider rear framing on the hood used with the late-style windscreen.

 

Different propeller types were fitted, according to where the Spitfire V was built: Supermarine and Westland manufactured VBs and VCs used 10 ft 9 in (3.28 m) diameter, 3 bladed de Havilland constant speed units, with narrow metal blades, while Castle Bromwich manufactured VBs and VCs were fitted with a wide bladed Rotol constant speed propeller of either 10 ft 9 in (3.28 m) diameter, with metal blades, or (on late production Spitfires) 10 ft 3 in (3.12 m) diameter, with broader, "Jablo" (compressed wood) blades. The Rotol spinners were longer and more pointed than the de Havilland leading to a 3.5 in (8.9 cm) increase in overall length. The Rotol propellers allowed a modest speed increase over 20,000 ft (6,100 m) and an increase in the service ceiling. A large number of Spitfire VBs were fitted with "gun heater intensifier" systems on the exhaust stacks. These piped additional heated air into the gun bays. There was a short tubular intake on the front of the first stack and a narrow pipe led into the engine cowling from the rear exhaust.

 

The VB series were the first Spitfires able to carry a range of specially designed "slipper" drop tanks which were fitted underneath the wing centre-section. Small hooks were fitted, just forward of the inboard flaps: when the tank was released these hooks caught the trailing edge of the tank, swinging it clear of the fuselage.

 

With the advent of the superb Focke Wulf Fw 190 in August 1941 the Spitfire was for the first time truly outclassed, hastening the development of the "interim" Mk IX. In an effort to counter this threat, especially at lower altitudes, the VB was the first production version of the Spitfire to use "clipped" wingtips as an option, reducing the wingspan to 32 ft 2 in (9.8 m).The clipped wings increased the roll rate and airspeed at lower altitudes. Several different versions of the Merlin 45/50 family were used, including the Merlin 45M which had a smaller "cropped" supercharger impeller and boost increased to +18 lb. This engine produced 1,585 hp (1,182 kW) at 2,750 ft (838 m), increasing the L.F VB's maximum rate of climb to 4720 ft/min (21.6 m/s) at 2,000 ft (610 m).

 

VB Trop of 40 Squadron SAAF fitted with the "streamlined" version of the Aboukir filter, a broad-bladed, 10 ft 3 in (3.12 m) diameter Rotol propeller, and clipped wings.

The Mk VB(trop) (or type 352) could be identified by the large Vokes air filter fitted under the nose; the reduced speed of the air to the supercharger had a detrimental effect on the performance of the aircraft, reducing the top speed by 8 mph (13 km/h) and the climb rate by 600 ft/min (3.04 m/s), but the decreased performance was considered acceptable. This variant was also fitted with a larger oil tank and desert survival gear behind the pilot's seat. A new "desert" camouflage scheme was applied. Many VB(trop)s were modified by 103 MU (Maintenance Unit-RAF depots in which factory fresh aircraft were brought up to service standards before being delivered to squadrons) at Aboukir, Egypt by replacing the Vokes filter with locally manufactured "Aboukir" filters, which were lighter and more streamlined. Two designs of these filters can be identified in photos: one had a bulky, squared off filter housing while the other was more streamlined. These aircraft were usually fitted with the wide blade Rotol propeller and clipped wings.

 

Triumph Spitfire Mk I Roadster

 

The Triumph Spitfire is a small English two-seat sports car, introduced at the London Motor Show in 1962.[3] The vehicle was based on a design produced for Standard-Triumph in 1957 by Italian designer Giovanni Michelotti. The platform for the car was largely based upon the chassis, engine, and running gear of the Triumph Herald saloon, and was manufactured at the Standard-Triumph works at Canley, in Coventry. As was typical for cars of this era, the bodywork was fitted onto a separate structural chassis, but for the Spitfire, which was designed as an open top or convertible sports car from the outset, the ladder chassis was reinforced for additional rigidity by the use of structural components within the bodywork. The Spitfire was provided with a manual hood for weather protection, the design improving to a folding hood for later models. Factory-manufactured hard-tops were also available.

 

The Triumph Spitfire was originally devised by Standard-Triumph to compete in the small sports car market that had opened up with the introduction of the Austin-Healey Sprite. The Sprite had used the basic drive train of the Austin A30/35 in a light body to make up a budget sports car; Triumph's idea was to use the mechanicals from their small saloon, the Herald, to underpin the new project. Triumph had one advantage, however; where the Austin A30 range was of unitary construction, the Herald featured a separate chassis. It was Triumph's intention to cut that chassis down and clothe it in a sports body, saving the costs of developing a completely new chassis / body unit.

 

Italian designer Michelotti—who had already penned the Herald—was commissioned for the new project, and came up with a traditional, swooping body. Wind-up windows were provided (in contrast to the Sprite/Midget, which still featured sidescreens, also called curtains, at that time), as well as a single-piece front end which tilted forwards to offer unrivaled access to the engine. At the dawn of the 1960s, however, Standard-Triumph was in deep financial trouble, and unable to put the new car into production; it was not until the company was taken over by the Leyland organization funds became available and the car was launched. Leyland officials, taking stock of their new acquisition, found Michelotti's prototype hiding under a dust sheet in a corner of the factory and rapidly approved it for production.

 

Spitfire 4 or Mark I (1962-1964)

 

Overview:

Production1962–1964

45,753 made

Powertrain:

Engine1,147 cc (1.1 l) I4

Transmission4-speed manual with optional overdrive on top and third from 1963 onwards

Dimensions:

Curb weight1,568 lb (711 kg) (unladen U.K.-spec)

 

The production car changed little from the prototype, although the full-width rear bumper was dropped in favour of two part-bumpers curving round each corner, with overriders. Mechanicals were basically stock Herald. The engine was an 1,147 cc (1.1 l) 4-cylinder with a pushrod OHV cylinder head and 2 valves per cylinder, mildly tuned for the Spitfire, fed by twin SU carburettors. Also from the Herald came the rack and pinion steering and coil-and-wishbone front suspension up front, and at the rear a single transverse-leaf swing axle arrangement. This ended up being the most controversial part of the car: it was known to "tuck in" and cause violent over steer if pushed too hard, even in the staid Herald. In the sportier Spitfire (and later the 6-cylinder Triumph GT6 and Triumph Vitesse) it led to severe criticism. The body was bolted to a much-modified Herald chassis, the outer rails and the rear outriggers having been removed; little of the original Herald chassis design was left, and the Spitfire used structural outer sills to stiffen its body tub.

 

The Spitfire was an inexpensive small sports car and as such had very basic trim, including rubber mats and a large plastic steering wheel. These early cars were referred to both as "Triumph Spitfire Mark I" and "Spitfire 4", not to be confused with the later Spitfire Mark IV.

 

In UK specification the in-line four produced 63 bhp (47 kW) at 5750 rpm, and 67 lb·ft (91 N·m)of torque at 3500 rpm. This gave a top speed of 92 mph (148 km/h), and would achieve 0 to 60 mph (97 km/h) in 17.3 seconds. Average fuel consumption was 31mpg.

 

For 1964 an overdrive option was added to the 4-speed manual gearbox to give more relaxed cruising. Wire wheels and a hard top were also available.

 

Text regarding the Supermarine Spitfire aeroplane and Triumph Spitfire Roadster has been taken from excerpts of Wikipedia articles on each model.

 

The Supermarine Spitfire Mk VB aircraft and 1962 Triumph Spitfire Mk I road car have been modelled in Lego miniland-scale for Flickr LUGNuts' 79th Build Challenge, - 'LUGNuts goes Wingnuts, ' - featuring automotive vehicles named after, inspired by, or with some relationship to aircraft.

Manufacturer: Boeing

Operator: Qatar Emiri AIr Force/ Boeing

Type: F-15QA Ababil (QA536) multirole fighter aircraft

Evnet/ Location: 2024 RIAT/ RAF Fairford

Comment: The demonstration of the Qatari Boeing two F-15QA consisted of two different configurations: one with a 'clean' fit, the second with a simulated full weapons load to demonstrate how little the aircraft's aerodynamic performance is affected by the additional weight/drag. The aircraft themselves were en route to Qatar on their delivery flights from the US, with the demos at RIAT provided by Boeing test-pilots.

The Citroën DS (French pronunciation: ​[si.tʁɔ.ˈɛn de ɛs]) is a front-engine, front-wheel-drive executive car manufactured and marketed by the French company Citroën from 1955 to 1975 in sedan, wagon/estate and convertible body configurations. Italian sculptor and industrial designer Flaminio Bertoni and the French aeronautical engineer André Lefèbvre styled and engineered the car. Paul Magès developed the hydropneumatic self-levelling suspension.

 

Noted for its aerodynamic, futuristic body design and innovative technology, the DS set new standards in ride quality, handling, and braking—and was the first production car equipped with disc brakes.

 

Citroën sold 1,455,746 examples, including 1,330,755 built at the manufacturer's Paris Quai André-Citroën production plant.

 

The DS came third in the 1999 Car of the Century poll recognizing the world's most influential auto designs and was named the most beautiful car of all time by Classic & Sports Car magazine

 

MODEL HISTORY

After 18 years of secret development as the successor to the Traction Avant, the DS 19 was introduced on 5 October 1955 at the Paris Motor Show. In the first 15 minutes of the show, 743 orders were taken, and orders for the first day totalled 12,000. During the 10 days of the show, the DS took in 80,000 deposits; a record that has stood for over 60 years.

 

Contemporary journalists said the DS pushed the envelope in the ride vs. handling compromise possible in a motor vehicle.

 

To a France still deep in reconstruction after the devastation of World War II, and also building its identity in the post-colonial world, the DS was a symbol of French ingenuity. The DS was distributed to many territories throughout the world.

 

It also posited the nation's relevance in the Space Age, during the global race for technology of the Cold War. Structuralist philosopher Roland Barthes, in an essay about the car, said that it looked as if it had "fallen from the sky". An American advertisement summarised this selling point: "It takes a special person to drive a special car".

 

Because they were owned by the technologically aggressive tire manufacturer Michelin, Citroën had designed their cars around the technically superior radial tire since 1948, and the DS was no exception.

 

The car featured a novel hydropneumatic suspension including an automatic leveling system and variable ground clearance, developed in-house by Paul Magès. This suspension allowed the DS to travel quickly on the poor road surfaces common in France.

 

In addition, the vehicle had power steering and a semi-automatic transmission (the transmission required no clutch pedal, but gears still had to be shifted by hand), though the shift lever controlled a powered hydraulic shift mechanism in place of a mechanical linkage, and a fibreglass roof which lowered the centre of gravity and so reduced weight transfer. Inboard front brakes (as well as independent suspension) reduced unsprung weight. Different front and rear track widths and tyre sizes reduced the unequal tyre loading, which is well known to promote understeer, typical of front-engined and front-wheel drive cars.

 

As with all French cars, the DS design was affected by the tax horsepower system, which effectively mandated very small engines. Unlike the Traction Avant predecessor, there was no top-of-range model with a powerful six-cylinder engine. Citroën had planned an air-cooled flat-6 engine for the car, but did not have the funds to put the prototype engine into production.

 

The DS placed third in the 1999 Car of the Century competition, and fifth on Automobile Magazine's "100 Coolest Cars" listing in 2005. It was also named the most beautiful car of all time by Classic & Sports Car magazine after a poll of 20 world-renowned car designers, including Giorgetto Giugiaro, Ian Callum, Roy Axe, Paul Bracq, and Leonardo Fioravanti.

 

NAME

Both the DS and its simpler sibling, the ID, used a punning name. "DS" is pronounced in French as "Déesse" (goddess); "ID" is pronounced as "Idée" (idea). An intermediate model was called the DW.

 

MOTORSPORT

The DS was successful in motorsports like rallying, where sustained speeds on poor surfaces are paramount, and won the Monte Carlo Rally in 1959. In the 1000 Lakes Rally, Pauli Toivonen drove a DS19 to victory in 1962.

 

In 1966, the DS won the Monte Carlo Rally again, with some controversy as the competitive BMC Mini-Cooper team was disqualified due to rule infractions. Ironically, Mini was involved with DS competition again two years later, when a drunk driver in a Mini in Sydney Australia crashed into the DS that was leading the 1968 London–Sydney Marathon, 98 miles from the finish line. The DS was still competitive in the grueling 1974 London-Sahara-Munich World Cup Rally, where it won over 70 other cars, only 5 of which even completed the entire event.

 

TECHNICAL INNOVATION - HYDRAULIC SYSTEMS

In conventional cars, hydraulics are only used in brakes and power steering. In the DS they were also used for the suspension, clutch and transmission. The cheaper 1957 ID19 did have manual steering and a simplified power-braking system. An engine driven pump pressurizes the closed system to 2,400 pounds per square inch.

 

At a time when few passenger vehicles had independent suspension on all wheels, the application of the hydraulic system to the car's suspension system to provide a self-levelling system was an innovative move. This suspension allowed the car to achieve sharp handling combined with very high ride quality, frequently compared to a "magic carpet".

 

The hydropneumatic suspension used was pioneered the year before, on the rear of another car from Citroën, the top of range Traction Avant 15CV-H.

 

IMPACT ON CITROEN BRAND DEVELOPMENT

The 1955 DS cemented the Citroën brand name as an automotive innovator, building on the success of the Traction Avant, which had been the world's first mass-produced unitary body front-wheel-drive car in 1934. In fact, the DS caused such a huge sensation that Citroën was apprehensive that future models would not be of the same bold standard. No clean sheet new models were introduced from 1955 to 1970.

 

The DS was a large, expensive executive car and a downward brand extension was attempted, but without result. Throughout the late 1950s and 1960s Citroën developed many new vehicles for the very large, profitable market segments between the 2CV and the DS, occupied by vehicles like the Peugeot 403, Renault 16 and Ford Cortina, but none made it into production. Either they had uneconomic build costs, or were ordinary "me too" cars, not up to the company's high standard of innovation. As Citroën was owned by Michelin from 1934 to 1974 as a sort of research laboratory, such broad experimentation was possible. Michelin after all was getting a powerful advertisement for the capabilities of the radial tire Michelin had invented, when such experimentation was successful.

 

New models based on the small, utilitarian 2CV economy car were introduced, notably the 1961 Ami. It was also designed by Flaminio Bertoni and aimed to combine Three-box styling with the chassis of the 2CV. The Ami was very successful in France, but less so on export markets. Many found the styling controversial, and the car noisy and underpowered. The Dyane, was a modernised 2CV with a hatchback, competed with the 2CV inspired Renault 4 Hatchback. All these 2 cylinder models were very small, so there remained a wide market gap to the DS range all through the 1960s.

 

In 1970, Citroën finally introduced a car to target the mid-range - the Citroën GS, which won the "European car of the Year" for 1971 and sold 2.5 million units. It combined a small 55 horsepower flat-4 air-cooled engine with Hydropneumatic suspension. The intended 106 horsepower Wankel rotary-engined version with more power did not reach full production.

 

REPLACING THE DS

The DS remained popular and competitive throughout its production run. Its peak production year was 1970. Certain design elements like the somewhat narrow cabin, column-mounted gearstick, and separate fenders began to seem a little old-fashioned in the 1970s.

 

Citroën invested enormous resources to design and launch an entirely new vehicle in 1970, the SM, which was in effect a thoroughly modernized DS, with similar length, but greater width. The manual gearbox was a modified DS unit. The front disc brakes were the same design. Axles, wheel bearings, steering knuckles, and hydraulic components were either DS parts or modified DS parts.

 

The SM had a different purpose than replacing the 15-year-old DS design however - it was meant to launch Citroën into a completely new luxury grand touring market segment. Only fitted with a costly, exotic Maserati engine, the SM was faster and much more expensive than the DS. The SM was not designed to be a practical 4-door saloon suitable as a large family car, the key market for vehicles of this type in Europe. Typically, manufacturers would introduce low-volume coupés based on parts shared with an existing saloon, not as unique models, a contemporary example being the Mercedes-Benz SLC-Class.

 

The SM's high price and limited utility of the 2+2 seating configuration, meant the SM as actually produced could not seize the mantle from the DS.

 

So, while the design funds invested would allow the DS to be replaced by two cars - a 'modern DS' and the smaller CX, it was left to the CX alone to provide Citroën's large family or executive car in the model range.

 

The last DS came off the production line on 24 April 1975 - the manufacturer had taken the elementary precaution of building up approximately eight-month's of inventory of the "break" (estate/station wagon) version of the DS, to cover the period till Autumn 1975 when the estate/station wagon version of the CX would be introduced.

 

DEVELOPMENT

The DS always maintained its size and shape, with easily removable, unstressed body panels, but certain design changes did occur. During the 20-year production life improvements were made on an ongoing basis.

ID 19 submodel to extend brand downwards (1957–69)

 

The 1955 DS19 was 65% more expensive than the car it replaced, the Citroën Traction Avant. This affected potential sales in a country still recovering economically from World War II, so a cheaper submodel, the Citroën ID, was introduced in 1957.

 

The ID shared the DS's body but was less powerful and luxurious. Although it shared the engine capacity of the DS engine (at this stage 1,911 cc), the ID provided a maximum power output of only 69 hp compared to the 75 hp claimed for the DS19. Power outputs were further differentiated in 1961 when the DS19 acquired a Weber-32 twin bodied carburettor, and the increasing availability of higher octane fuel enabled the manufacturer to increase the compression ratio from 7.5:1 to 8.5:1. A new DS19 now came with a promised 83 hp of power. The ID19 was also more traditional mechanically: it had no power steering and had conventional transmission and clutch instead of the DS's hydraulically controlled set-up. Initially the basic ID19 was sold on the French market with a price saving of more than 25% against the DS, although the differential was reduced at the end of 1961 when the manufacturer quietly withdrew the entry level ID19 "Normale" from sale. A station wagon variant, the ID Break, was introduced in 1958.

 

D SPECIAL AND D SUPER (1970–75)

The ID was replaced by the D Spécial and D Super in 1970, but these retained the lower specification position in the range. The D Super was available with the DS21 2175ccm engine and a 5 speed gearbox, and named the D Super 5.

 

SERIE 2 - NOSE REDESIGN IN 1962

In September 1962, the DS was restyled with a more aerodynamically efficient nose, better ventilation and other improvements. It retained the open two headlamp appearance, but was available with an optional set of driving lights mounted on the front fenders. All models in the range changed nose design at the same time, including the ID and station wagon models.

Series 3 - Nose redesign in 1967 with Directional headlights

 

In late 1967, for the 1968 model year, the DS and ID was again restyled, by Robert Opron, who also styled the 1970 SM and 1974 CX. This version had a more streamlined headlamp design, giving the car a notably shark-like appearance. This design had four headlights under a smooth glass canopy, and the inner set swivelled with the steering wheel. This allowed the driver to see "around" turns, especially valuable on twisting roads driven at high speed at night.

 

Behind each glass cover lens, the inboard high-beam headlamp swivels by up to 80° as the driver steers, throwing the beam along the driver's intended path rather than uselessly across the curved road. The outboard low-beam headlamps are self-leveling in response to pitching caused by acceleration and braking.

 

However, this feature was not allowed in the US at the time (see World Forum for Harmonization of Vehicle Regulations), so a version with four exposed headlights that did not swivel was made for the US market.

 

This 'turning headlight' feature was new to the market - it had only been seen before on the very rare three headlight 1935 Tatra 77A. The Tucker, which never was mass-produced, had a central headlight that turned with the steering. 45 years later, it is now a commonly available feature, even in the United States.

 

NEW GREEN HYDRAULIC FLUID

The original hydropneumatic system used a vegetable oil liquide hydraulique végétal (LHV), similar to that used in other cars at the time, but later switched to a synthetic fluid liquide hydraulique synthétique (LHS). Both of these had the disadvantage that they are hygroscopic, as is the case with most brake fluids. Disuse allows water to enter the hydraulic components causing deterioration and expensive maintenance work. The difficulty with hygroscopic hydraulic fluid was exacerbated in the DS/ID due to the extreme rise and fall in the fluid level in the reservoir, which went from nearly full to nearly empty when the suspension extended to maximum height and the six accumulators in the system filled with fluid. With every "inhalation" of fresh moisture- (and dust-) laden air, the fluid absorbed more water.

 

For the 1967 model year, Citroën introduced a new mineral oil-based fluid LHM (Liquide Hydraulique Minéral). This fluid was much less harsh on the system. LHM remained in use within Citroën until the Xantia was discontinued in 2001.

 

LHM required completely different materials for the seals. Using either fluid in the incorrect system would completely destroy the hydraulic seals very quickly. To help avoid this problem, Citroën added a bright green dye to the LHM fluid and also painted all hydraulic elements bright green. The former LHS parts were painted black.

 

All models, including the station wagon and ID, were upgraded at the same time. The hydraulic fluid changed to the technically superior LHM in all markets except the US and Canada, where the change did not take place until January 1969, due to local regulations.

 

INTERNATIONAL SALES AND PRODUCTION

The DS was primarily manufactured at the Quai André-Citroën in the Javel neighborhood of Paris, with other manufacturing facilities in the United Kingdom, South Africa, the former Yugoslavia (mostly Break Ambulances), and Australia.

 

Australia constructed their own D variant in the 1960s at Heidelberg, Victoria, identified as the ID 19 "Parisienne." Australian market cars were fitted with options as standard equipment such as the "DSpecial DeLuxe" that were not available on domestic European models.

 

Until 1965, cars were assembled at the manufacturer's Slough premises, to the west of London, using a combination of French made knock down kits and locally sourced components, some of them machined on site. A French electrical system superseded the British one on the Slough cars in 1962, giving rise to a switch to "continental style" negative earthing. After 1965 cars for the British market were imported fully assembled from the company's French plant. The British-built cars are distinguished by their leather seats, wooden (early ID19 models) one piece plastic (early DS19 models) dashboards, chromed number plate mount let into the front bumper, and (on pre-1962 cars) Lucas-made electrics. These were all right hand drive cars.

 

The DS was built and sold in South Africa from 1959 to 1975.

 

The DS was sold in Japan, but the models were built in France and left hand drive.

 

DS IN NORTH AMERICA

The DS was sold in North America from 1956 to 1972. Despite its popularity in Europe, it didn't sell well in the United States, and little better in Canada. While promoted as a luxury car, it did not have the basic features that American buyers expected to find on such a vehicle, such as an automatic transmission, air conditioning, power windows, or a powerful engine. The DS was designed specifically to address the French market, with punitive tax horsepower taxation of large engines, as well as very poor roads – it's no great mystery that it was a fish out of water when those constraints were removed.

 

Jay Leno described the sporadic supply of spare parts as a problem for 1970s era customers, based on his early experiences working at a Citroën dealer in Boston.

 

The DS was expensive, with a 115 hp (86 kW) vehicle costing $4,170 in 1969, when the price was $4,500 for a 360 hp (268 kW) Buick Electra 225 4 door sedan. For all years, 38,000 units were sold.

 

US regulations at the time also banned one of the car's more advanced features: its composite headlamps with aerodynamic covered lenses. Based on legislation that dated from 1940, all automobiles sold in the U.S. were required to have round, sealed beam headlamps that produced a meager 75,000 candlepower. The powerful quartz iodine swiveling headlamps designed for the 1968 model DS represented so many performance improvements at once that they were far beyond what the regulations could allow.[50] Even the aerodynamic headlight covers were illegal – as seen on the 1968 Jaguar E-Type. It took the lobbying muscle of Ford to point out that the government was requiring two contradictory things – safety, by ensuring that all headlights were best-of-breed circa 1940, and fuel economy through the CAFE standard – by definition, cars with poor aerodynamics are sacrificing fuel economy. Composite bulb lamps and aerodynamic covered headlights were not permitted until 1983.

 

The European lamps were legal in Canada, including the directional headlamps.

 

The hydraulic fluid change in 1967 was another brain teaser for U.S. automotive regulators at the Department of Transportation. NHTSA follows the precautionary principle, also used by the Food and Drug Administration, where new innovations are prohibited until their developers can prove them to the regulators; this stifles the experimentation that automakers need to advance their products. NHTSA had already approved a brake fluid they considered safe – DOT 3 brake fluid, which is red and hygroscopic to promote internal rust. This completely different fluid, used in aircraft applications – the technically superior green LHM (Liquide Hydraulique Mineral) – took NHTSA two years to analyze for automotive use. Approval finally came in January 1969, so half the U.S. cars of the 1969 model year use red fluid and half use green fluid.

 

DESIGN VARIATIONS

PALLAS

In 1965 a luxury upgrade, the DS Pallas (after Greek goddess Pallas), was introduced. This included comfort features such as better noise insulation, a more luxurious (and optional leather) upholstery and external trim embellishments. From 1966 the Pallas model received a driver's seat with height adjustment.

 

STATION WAGON, FAMILIALE AND AMBULANCE

A station wagon version was introduced in 1958. It was known by various names in different markets (Break in France, Safari and Estate in the UK, Wagon in the US, and Citroën Australia used the terms Safari and Station-Wagon). It had a steel roof to support the standard roof rack. 'Familiales' had a rear seat mounted further back in the cabin, with three folding seats between the front and rear squabs. The standard Break had two side-facing seats in the main load area at the back.

 

The Ambulance configuration was similar to that of the Break, but with a 60/30 split in the rear folding seat to accommodate a stretcher. A 'Commerciale' version was also available for a time.

 

The Safari saw use as a camera car, notably by the BBC. The hydropneumatic suspension produces an unusually steady platform for filming while driving.

 

CONVERTIBLE

Rarest and most collectable of all DS variants, a convertible was offered from 1958 until 1973. The Cabriolet d'Usine (factory convertible) were built by French carrossier Henri Chapron, for the Citroën dealer network. It was an expensive car, so only 1,365 were sold. These DS convertibles used a special frame which was reinforced on the sidemembers and rear suspension swingarm bearing box, similar to, but not identical to the Break (Station Wagon) frame.

 

CHAPRON VARIATIONS

In addition, Chapron also produced a few coupés, non-works convertibles and special sedans (including the "Prestige", same wheelbase but with a central divider, and the "Lorraine" notchback).

 

BOSSAERT COUPE

Between 1959 and 1964, Hector Bossaert produced a coupé on a DS chassis shortened by 470 mm. While the front end remained unchanged, the rear end featured notchback styling.

 

THE REACTOR

In 1965, noted American auto customizer Gene Winfield created The Reactor, a Citroën DS chassis, with a turbocharged 180 hp (130 kW) flat-six engine from the Corvair driving the front wheels. Since the DS already had the engine behind the front wheels, the longer engine meant only one row of seats. This was draped in a streamlined, low slung, aluminum body.

 

The Reactor was seen in American Television programs of the era, such as Star Trek: The Original Series episode 2.25 ("Bread and Circuses)," Batman episodes 110 ("Funny Feline Felonies") and 111 (driven by Catwoman Eartha Kitt), and Bewitched, which devoted its episode 3.19 ("Super Car") to The Reactor.

 

MICHELIN PLR

The Michelin PLR is a mobile tire evaluation machine, based on the DS Break, built in 1972, later used for promotion.

Technical details

 

SUSPENSION

In a hydropneumatic suspension system, each wheel is connected, not to a spring, but to a hydraulic suspension unit consisting of a hydraulic accumulator sphere of about 12 cm in diameter containing pressurised nitrogen, a cylinder containing hydraulic fluid screwed to the suspension sphere, a piston inside the cylinder connected by levers to the suspension itself, and a damper valve between the piston and the sphere. A membrane in the sphere prevented the nitrogen from escaping. The motion of the wheels translated to a motion of the piston, which acted on the oil in the nitrogen cushion and provided the spring effect. The damper valve took place of the shock absorber in conventional suspensions. The hydraulic cylinder was fed with hydraulic fluid from the main pressure reservoir via a height corrector, a valve controlled by the mid-position of the anti-roll bar connected to the axle. If the suspension was too low, the height corrector introduced high-pressure fluid; if it was too high, it released fluid back to the fluid reservoir. In this manner, a constant ride height was maintained. A control in the cabin allowed the driver to select one of five heights: normal riding height, two slightly higher riding heights for poor terrain, and two extreme positions for changing wheels. (The correct term, oleopneumatic (oil-air), has never gained widespread use. Hydropneumatic (water-air) continues to be preferred overwhelmingly.)

 

The DS did not have a jack for lifting the car off the ground. Instead, the hydraulic system enabled wheel changes with the aid of a simple adjustable stand. To change a flat tyre, one would adjust the suspension to its topmost setting, insert the stand into a special peg near the flat tyre, then readjust the suspension to its lowermost setting. The flat tyre would then retract upwards and hover above ground, ready to be changed. This system, used on the SM also, was superseded on the CX by a screw jack that, after the suspension was raised to the high position, lifted the tire clear of the ground. The DS system, while impressive to use, sometimes dropped the car quite suddenly, especially if the stand was not placed precisely or the ground was soft or unlevel.

 

SOURCE AND RESERVE OF PRESSURE

The central part of the hydraulic system was the high pressure pump, which maintained a pressure of between 130 and 150 bar in two accumulators. These accumulators were very similar in construction to the suspension spheres. One was dedicated to the front brakes, and the other ran the other hydraulic systems. (On the simpler ID models, the front brakes operated from the main accumulator.) Thus in case of a hydraulic failure, the first indication would be that the steering became heavy, followed by the gearbox not working; only later would the brakes fail.

 

Two different hydraulic pumps were used. The DS used a seven-cylinder axial piston pump driven off two belts and delivering 175 bar (2,540 psi) of pressure. The ID19, with its simpler hydraulic system, had a single-cylinder pump driven by an eccentric on the camshaft.

 

GEARBOX AND CLUTCH

HYDRAULIQUE OR CITROMATIC

The DS was initially offered only with the "hydraulique" four-speed semi-automatic (bvh—"boîte de vitesses hydraulique") gearbox.

 

This was a four-speed gearbox and clutch, operated by a hydraulic controller. To change gears, the driver flicked a lever behind the steering wheel to the next position and eased-up on the accelerator pedal. The hydraulic controller disengaged the clutch, engaged the nominated gear, and re-engaged the clutch. The speed of engagement of the clutch was controlled by a centrifugal regulator sensing engine rpm and driven off the camshaft by a belt, the position of the butterfly valve in the carburettor (i.e., the position of the accelerator), and the brake circuit. When the brake was pressed, the engine idle speed dropped to an rpm below the clutch engagement speed, thus preventing friction while stopped in gear at traffic lights. When the brake was released, the idle speed increased to the clutch dragging speed. The car would then creep forward much like automatic transmission cars. This drop in idle throttle position also caused the car to have more engine drag when the brakes were applied even before the car slowed to the idle speed in gear, preventing the engine from pulling against the brakes. In the event of loss of hydraulic pressure (following loss of system fluid), the clutch would disengage, to prevent driving, while brake pressure reserves would allow safe braking to standstill.

 

MANUAL - FOUR SPEED AND FIVE-SPEED

The later and simpler ID19 had the same gearbox and clutch, manually operated. This configuration was offered as a cheaper option for the DS in 1963. The mechanical aspects of the gearbox and clutch were completely conventional and the same elements were used in the ID 19. In September 1970, Citroën introduced a five-speed manual gearbox, in addition to the original four-speed unit.

 

FULLY AUTOMATIC

In September 1971 Citroën introduced a 3-speed fully automatic Borg-Warner 35 transmission gearbox, on the DS 21 and later DS 23 models. It is ironic that the fully automatic transmission DS was never sold in the US market, where this type of transmission had gained market share so quickly that it became the majority of the market by this time. Many automatic DSs, fuel-injected DS 23 sedans with air conditioning, were sold in Australia.

 

ENGINES

The DS was originally designed around an air-cooled flat-six based on the design of the 2-cylinder engine of the 2CV, similar to the motor in the Porsche 911. Technical and monetary problems forced this idea to be scrapped.

 

Thus, for such a modern car, the engine of the original DS 19 was also old-fashioned. It was derived from the engine of the 11CV Traction Avant (models 11B and 11C). It was an OHV four-cylinder engine with three main bearings and wet liners, and a bore of 78 mm and a stroke of 100 mm, giving a volumetric displacement of 1911 cc. The cylinder head had been reworked; the 11C had a reverse-flow cast iron cylinder head and generated 60 hp (45 kW) at 3800 rpm; by contrast, the DS 19 had an aluminium cross-flow head with hemispherical combustion chambers and generated 75 hp (56 kW) at 4500 rpm.

 

Like the Traction Avant, the DS had the gearbox mounted in front of the engine, with the differential in between. Thus some consider the DS to be a mid engine front-wheel drive car.

 

The DS and ID powerplants evolved throughout its 20-year production life. The car was underpowered and faced constant mechanical changes to boost the performance of the four-cylinder engine. The initial 1911 cc three main bearing engine (carried forward from the Traction Avant) of the DS 19 was replaced in 1965 with the 1985 cc five-bearing wet-cylinder motor, becoming the DS 19a (called DS 20 from September 1969).

 

The DS 21 was also introduced for model year 1965. This was a 2175 cc, five main bearing engine; power was 109 hp This engine received a substantial increase in power with the introduction of Bosch electronic fuel injection for 1970, making the DS one of the first mass-market cars to use electronic fuel injection. Power of the carbureted version also increased slightly at the same time, owing to the employment of larger inlet valves.

 

Lastly, 1973 saw the introduction of the 2347 cc engine of the DS 23 in both carbureted and fuel-injected forms. The DS 23 with electronic fuel injection was the most powerful production model, producing 141 hp (105 kW).

 

IDs and their variants went through a similar evolution, generally lagging the DS by about one year. ID saloon models never received the DS 23 engine or fuel injection, although the Break/Familiale versions received the carburetted version of the DS 23 engine when it was introduced, supplemented the DS20 Break/Familiale.

 

The top of the range ID model, The DSuper5 (DP) gained the DS21 engine (the only model that this engine was retained in) for the 1973 model year and it was mated to a five-speed gearbox. This should not be confused with the 1985 cc DSuper fitted with an optional "low ratio" five-speed gearbox, or with the previous DS21M (DJ) five-speed.

 

IN POPULAR CULTURE

President Charles de Gaulle survived an assassination attempt at Le Petit-Clamart near Paris on August 22, 1962, planned by Algerian War veteran Jean-Marie Bastien-Thiry. The plan was to ambush the motorcade with machine guns, disable the vehicles, and then close in for the kill. De Gaulle praised the unusual abilities of his unarmoured DS with saving his life – the car was peppered with bullets, and the shots had punctured the tyres, but the car could still escape at full speed. This event was accurately recreated in the 1973 film The Day of the Jackal.

 

Beyond de Gaulle and the French aristocracy, the roomy DS also appealed to French taxi drivers.

 

Outside France, the car drew an eclectic customer mix, such as Cosmonaut Yuri Gagarin, Pope John XXIII, painter Marc Chagall, and actors Ken Berry, Jeff Bridges, and Rosamund Pike.

 

The DS appeared in several episodes of contemporary television series Mission: Impossible, including substantial appearances in 'The Slave' (ep. 2.06) and 'Robot' (ep. 4.09).

 

An ode to Jane Child's DS21 appears on her 1989 self-titled album.

 

In 1989, the film Back to the Future Part II featured a modified Citroen DS as a flying taxicab, when the main characters travel 30 years into the future (2015). Scarface (1983 film) with Al Pacino and the 2009 television series The Mentalist both feature the DS in key roles. According to Internet Movie Cars Database, the DS/ID has made over 2,000 film and television appearances so far.

 

Two films focus on the DS, including The Goddess of 1967 about a Japanese man purchasing a DS (goddess or déesse in French) in Australia, and 1995's Icelandic-Japanese road movie Cold Fever.

 

LEGACY

Citroën DS values have been rising – a 1973 DS 23 Injection Electronique "Decapotable" (Chapron Convertible) sold for EUR €176,250 (USD $209,738) at Christie's Rétromobile in February 2006. and a similar car sold by Bonhams in February 2009 brought EUR €343,497 (USD $440,436). On 18 September 2009 a 1966 DS21 Decapotable Usine was sold by Bonhams for a hammer price of UK£131,300. Bonhams sold another DS21 Decapotable (1973) on 23 January 2010 for EUR €189,000.

 

The DS's beloved place in French society was demonstrated in Paris on 9 October 2005 with a celebration of the 50th anniversary of its launch. 1,600 DS cars drove in procession past the Arc de Triomphe.

 

From 2005 to 2008, a young Frenchman named Manuel Boileau travelled around the world in a 1971 DS ambulance. It was an 80,000 kilometer journey across 38 countries called Lunaya World Tour. While traveling through Laos, he located the forlorn 1974 DS Prestige belonging to Sisavang Vatthana, the last King of the Kingdom of Laos, which is now preserved and restored by specialists in Bangkok.

 

In 2009, Groupe PSA created a new brand - DS Automobiles, intended as high quality, high specification variations on existing models, with differing mechanics and bodywork. This brand ranges across four models, the DS3, DS4, DS5, and the China-only SUV DS 6. The DS3, launched in March 2010, is based on Citroen's new C3, but is more customisable and unique, bearing some resemblance to the original DS, with its "Shark Fin" side pillar. These have created their own niches, with the DS4 being a mix of a crossover and a coupe and the DS5 mixing a coupe and an estate. Many feature hybrid-diesel engines to maximise efficiency.

 

WIKIPEDIA

Manufacturer: Boeing

Operator: Qatar Emiri AIr Force/ Boeing

Type: F-15QA Ababil (QA536) multirole fighter aircraft

Evnet/ Location: 2024 RIAT/ RAF Fairford

Comment: The demonstration of the Qatari Boeing two F-15QA consisted of two different configurations: one with a 'clean' fit, the second with a simulated full weapons load to demonstrate how little the aircraft's aerodynamic performance is affected by the additional weight/drag. The aircraft themselves were en route to Qatar on their delivery flights from the US, with the demos at RIAT provided by Boeing test-pilots.

The Supermarine Spitfire is a British single-seat fighter aircraft that was used by the Royal Air Force and many other Allied countries during and after the Second World War. The Spitfire was built in many variants, using several wing configurations, and was produced in greater numbers than any other British aircraft. It was also the only British fighter to be in continuous production throughout the war. The Spitfire continues to be a popular aircraft, with approximately 55 Spitfires being airworthy, while many more are static exhibits in aviation museums all over the world.

 

The Spitfire was designed as a short-range, high-performance interceptor aircraft by R. J. Mitchell, chief designer at Supermarine Aviation Works (which operated as a subsidiary of Vickers-Armstrong from 1928). In accordance with its role as an interceptor, Mitchell designed the Spitfire's distinctive elliptical wing to have the thinnest possible cross-section; this thin wing enabled the Spitfire to have a higher top speed than several contemporary fighters, including the Hawker Hurricane. Mitchell continued to refine the design until his death from cancer in 1937, whereupon his colleague Joseph Smith took over as chief designer, overseeing the development of the Spitfire through its multitude of variants.

 

During the Battle of Britain (July–October 1940), the Spitfire was perceived by the public to be the RAF fighter, though the more numerous Hawker Hurricane shouldered a greater proportion of the burden against the Luftwaffe. However, because of its higher performance, Spitfire units had a lower attrition rate and a higher victory-to-loss ratio than those flying Hurricanes.

 

After the Battle of Britain, the Spitfire superseded the Hurricane to become the backbone of RAF Fighter Command, and saw action in the European, Mediterranean, Pacific and the South-East Asian theatres. Much loved by its pilots, the Spitfire served in several roles, including interceptor, photo-reconnaissance, fighter-bomber and trainer, and it continued to serve in these roles until the 1950s. The Seafire was a carrier-based adaptation of the Spitfire which served in the Fleet Air Arm from 1942 through to the mid-1950s. Although the original airframe was designed to be powered by a Rolls-Royce Merlin engine producing 1,030 hp (768 kW), it was strong enough and adaptable enough to use increasingly powerful Merlin and, in later marks, Rolls-Royce Griffon engines producing up to 2,340 hp (1,745 kW); as a consequence of this the Spitfire's performance and capabilities improved, sometimes dramatically, over the course of its life.

 

Mk V (Types 331, 349 & 352)

 

Spitfire LF.Mk VB, BL479, flown by Group Captain M.W.S Robinson, station commander of RAF Northolt, August 1943. This Spitfire has the wide bladed Rotol propeller, the internal armoured windscreen and "clipped" wings.

Late in 1940, the RAF predicted that the advent of the pressurised Junkers Ju 86P bomber series over Britain would be the start of a new sustained high altitude bombing offensive by the Luftwaffe, in which case development was put in hand for a pressurised version of the Spitfire, with a new version of the Merlin (the Mk VI). It would take some time to develop the new fighter and an emergency stop-gap measure was needed as soon as possible: this was the Mk V.

 

The basic Mk V was a Mk I with the Merlin 45 series engine. This engine delivered 1,440 hp (1,074 kW) at take-off, and incorporated a new single-speed single-stage supercharger design. Improvements to the carburettor also allowed the Spitfire to use zero gravity manoeuvres without any problems with fuel flow. Several Mk I and Mk II airframes were converted to Mk V standard by Supermarine and started equipping fighter units from early 1941. The majority of the Mk Vs were built at Castle Bromwich.

 

The VB became the main production version of the Mark Vs. Along with the new Merlin 45 series the B wing was fitted as standard. As production progressed changes were incorporated, some of which became standard on all later Spitfires. Production started with several Mk IBs which were converted to Mk VBs by Supermarine. Starting in early 1941 the round section exhaust stacks were changed to a "fishtail" type, marginally increasing exhaust thrust. Some late production VBs and VCs were fitted with six shorter exhaust stacks per side, similar to those of Spitfire IXs and Seafire IIIs; this was originally stipulated as applying specifically to VB(trop)s. After some initial problems with the original Mk I size oil coolers, a bigger oil cooler was fitted under the port wing; this could be recognised by a deeper housing with a circular entry. From mid-1941 alloy covered ailerons became a universal fitting.

 

Spitfire VC(trop), fitted with Vokes filters and "disc" wheels, of 417 Squadron RCAF in Tunisia in 1943.

A constant flow of modifications were made as production progressed. A "blown" cockpit hood, manufactured by Malcolm, was introduced in an effort to further increase the pilot's head-room and visibility. Many mid to late production VBs - and all VCs - used the modified, improved windscreen assembly with the integral bullet resistant centre panel and flat side screens introduced with the Mk III. Because the rear frame of this windscreen was taller than that of the earlier model the cockpit hoods were not interchangeable and could be distinguished by the wider rear framing on the hood used with the late-style windscreen.

 

Different propeller types were fitted, according to where the Spitfire V was built: Supermarine and Westland manufactured VBs and VCs used 10 ft 9 in (3.28 m) diameter, 3 bladed de Havilland constant speed units, with narrow metal blades, while Castle Bromwich manufactured VBs and VCs were fitted with a wide bladed Rotol constant speed propeller of either 10 ft 9 in (3.28 m) diameter, with metal blades, or (on late production Spitfires) 10 ft 3 in (3.12 m) diameter, with broader, "Jablo" (compressed wood) blades. The Rotol spinners were longer and more pointed than the de Havilland leading to a 3.5 in (8.9 cm) increase in overall length. The Rotol propellers allowed a modest speed increase over 20,000 ft (6,100 m) and an increase in the service ceiling. A large number of Spitfire VBs were fitted with "gun heater intensifier" systems on the exhaust stacks. These piped additional heated air into the gun bays. There was a short tubular intake on the front of the first stack and a narrow pipe led into the engine cowling from the rear exhaust.

 

The VB series were the first Spitfires able to carry a range of specially designed "slipper" drop tanks which were fitted underneath the wing centre-section. Small hooks were fitted, just forward of the inboard flaps: when the tank was released these hooks caught the trailing edge of the tank, swinging it clear of the fuselage.

 

With the advent of the superb Focke Wulf Fw 190 in August 1941 the Spitfire was for the first time truly outclassed, hastening the development of the "interim" Mk IX. In an effort to counter this threat, especially at lower altitudes, the VB was the first production version of the Spitfire to use "clipped" wingtips as an option, reducing the wingspan to 32 ft 2 in (9.8 m).The clipped wings increased the roll rate and airspeed at lower altitudes. Several different versions of the Merlin 45/50 family were used, including the Merlin 45M which had a smaller "cropped" supercharger impeller and boost increased to +18 lb. This engine produced 1,585 hp (1,182 kW) at 2,750 ft (838 m), increasing the L.F VB's maximum rate of climb to 4720 ft/min (21.6 m/s) at 2,000 ft (610 m).

 

VB Trop of 40 Squadron SAAF fitted with the "streamlined" version of the Aboukir filter, a broad-bladed, 10 ft 3 in (3.12 m) diameter Rotol propeller, and clipped wings.

The Mk VB(trop) (or type 352) could be identified by the large Vokes air filter fitted under the nose; the reduced speed of the air to the supercharger had a detrimental effect on the performance of the aircraft, reducing the top speed by 8 mph (13 km/h) and the climb rate by 600 ft/min (3.04 m/s), but the decreased performance was considered acceptable. This variant was also fitted with a larger oil tank and desert survival gear behind the pilot's seat. A new "desert" camouflage scheme was applied. Many VB(trop)s were modified by 103 MU (Maintenance Unit-RAF depots in which factory fresh aircraft were brought up to service standards before being delivered to squadrons) at Aboukir, Egypt by replacing the Vokes filter with locally manufactured "Aboukir" filters, which were lighter and more streamlined. Two designs of these filters can be identified in photos: one had a bulky, squared off filter housing while the other was more streamlined. These aircraft were usually fitted with the wide blade Rotol propeller and clipped wings.

 

Triumph Spitfire Mk I Roadster

 

The Triumph Spitfire is a small English two-seat sports car, introduced at the London Motor Show in 1962.[3] The vehicle was based on a design produced for Standard-Triumph in 1957 by Italian designer Giovanni Michelotti. The platform for the car was largely based upon the chassis, engine, and running gear of the Triumph Herald saloon, and was manufactured at the Standard-Triumph works at Canley, in Coventry. As was typical for cars of this era, the bodywork was fitted onto a separate structural chassis, but for the Spitfire, which was designed as an open top or convertible sports car from the outset, the ladder chassis was reinforced for additional rigidity by the use of structural components within the bodywork. The Spitfire was provided with a manual hood for weather protection, the design improving to a folding hood for later models. Factory-manufactured hard-tops were also available.

 

The Triumph Spitfire was originally devised by Standard-Triumph to compete in the small sports car market that had opened up with the introduction of the Austin-Healey Sprite. The Sprite had used the basic drive train of the Austin A30/35 in a light body to make up a budget sports car; Triumph's idea was to use the mechanicals from their small saloon, the Herald, to underpin the new project. Triumph had one advantage, however; where the Austin A30 range was of unitary construction, the Herald featured a separate chassis. It was Triumph's intention to cut that chassis down and clothe it in a sports body, saving the costs of developing a completely new chassis / body unit.

 

Italian designer Michelotti—who had already penned the Herald—was commissioned for the new project, and came up with a traditional, swooping body. Wind-up windows were provided (in contrast to the Sprite/Midget, which still featured sidescreens, also called curtains, at that time), as well as a single-piece front end which tilted forwards to offer unrivaled access to the engine. At the dawn of the 1960s, however, Standard-Triumph was in deep financial trouble, and unable to put the new car into production; it was not until the company was taken over by the Leyland organization funds became available and the car was launched. Leyland officials, taking stock of their new acquisition, found Michelotti's prototype hiding under a dust sheet in a corner of the factory and rapidly approved it for production.

 

Spitfire 4 or Mark I (1962-1964)

 

Overview:

Production1962–1964

45,753 made

Powertrain:

Engine1,147 cc (1.1 l) I4

Transmission4-speed manual with optional overdrive on top and third from 1963 onwards

Dimensions:

Curb weight1,568 lb (711 kg) (unladen U.K.-spec)

 

The production car changed little from the prototype, although the full-width rear bumper was dropped in favour of two part-bumpers curving round each corner, with overriders. Mechanicals were basically stock Herald. The engine was an 1,147 cc (1.1 l) 4-cylinder with a pushrod OHV cylinder head and 2 valves per cylinder, mildly tuned for the Spitfire, fed by twin SU carburettors. Also from the Herald came the rack and pinion steering and coil-and-wishbone front suspension up front, and at the rear a single transverse-leaf swing axle arrangement. This ended up being the most controversial part of the car: it was known to "tuck in" and cause violent over steer if pushed too hard, even in the staid Herald. In the sportier Spitfire (and later the 6-cylinder Triumph GT6 and Triumph Vitesse) it led to severe criticism. The body was bolted to a much-modified Herald chassis, the outer rails and the rear outriggers having been removed; little of the original Herald chassis design was left, and the Spitfire used structural outer sills to stiffen its body tub.

 

The Spitfire was an inexpensive small sports car and as such had very basic trim, including rubber mats and a large plastic steering wheel. These early cars were referred to both as "Triumph Spitfire Mark I" and "Spitfire 4", not to be confused with the later Spitfire Mark IV.

 

In UK specification the in-line four produced 63 bhp (47 kW) at 5750 rpm, and 67 lb·ft (91 N·m)of torque at 3500 rpm. This gave a top speed of 92 mph (148 km/h), and would achieve 0 to 60 mph (97 km/h) in 17.3 seconds. Average fuel consumption was 31mpg.

 

For 1964 an overdrive option was added to the 4-speed manual gearbox to give more relaxed cruising. Wire wheels and a hard top were also available.

 

Text regarding the Supermarine Spitfire aeroplane and Triumph Spitfire Roadster has been taken from excerpts of Wikipedia articles on each model.

 

The Supermarine Spitfire Mk VB aircraft and 1962 Triumph Spitfire Mk I road car have been modelled in Lego miniland-scale for Flickr LUGNuts' 79th Build Challenge, - 'LUGNuts goes Wingnuts, ' - featuring automotive vehicles named after, inspired by, or with some relationship to aircraft.

Temporary repair of the pilothouse aft bulkhead is complete. The outside steering station has been removed, and the pilothouse returned to its original configuration. The work was done by shipwright Chris Chase, assisted by Paul Lyter.

 

Canvasmake Suzi Clinefelter of Mystery Bay Sails and Canvas made the canvas cover over the aft cockpit. It will stretch tight when it first gets wet. www.mysterybaysailscanvas.com/

 

RIPTIDE was built in 1927 by the Schertzer Brothers Boat and Machine Company, then located on the north end of Lake Union near the foot of Stone Way in Seattle. She is 47 feet 1-inch long with a beam of 11 feet 10-inches and a draft of four feet. She is planked in port orford cedar riveted to white oak frames over an apitong backbone with western red cedar houses. She displaces about 10 tons, relatively light for a boat this size.

 

She was originally named NEREIAD, then, shortly thereafter, NOKARE. Her trunk cabin (the raised cabin aft of the pilothouse) was reportedly added (or extended) in 1933. By 1936, when owned by Russell G. Gibson, a Director of the Seattle Yacht club, she had been named RIPTIDE.

 

Mr Gibson owned her through at least 1960. After a few years, she was bought in 1965 by Richard Billings, who used her as a cruiser and live-aboard in Alaska. In 1968 Richard sold her to his brother Roger, who owned her through 2014. RIPTIDE is fortunate to have been owned by knowledgeable and caring owners throughout her long life.

 

RIPTIDE is a Coast Guard documented vessel. She carries documentation number 226242 carved into the interior face of both port and starboard bilge stringers. She is documented at 17 net tons and 21 gross tons.

 

Her original engine may have been a Hall-Scott gasoline engine, but is as yet unknown. By 1959 she had an eight cylinder Chrysler Crown gas engine, a common engine of the time, most likely added in the late 1940's. That engine was removed in 1967 when RIPTIDE was re-powered by a 1967 Volvo MD-70A diesel engine. The Volvo engine was removed in early June 2015 and was replaced by Cummins 5.9 liter diesel of 210hp. While her top speed is over 14 knots at 2400 rpm, her cruising speed is a much more sedate 9 knots at 1500 rpm. She carries 300 gallons of diesel fuel.

 

She was overhauled by the Port Townsend Shipwright's Co-Op in Port Townsend WA between April 8th and September 16th, 2015. The Co-Op replaced 35 frames, then replanked much of her hull above the waterline. They installed a new transom and decks, replaced her engine and exhaust system, and installed a modern electrical system. Finally, a new anchor windlass and chain was installed.

 

Diane Salguero of Salguero Marine Services varnished the transom and pilothouse windows and painted the vessel.

 

RIPTIDE's hailing port is Port Ludlow WA. She is usually moored in Port Madison, on Bainbridge Island, WA.

 

Port Townsend Shipwright's Co-Op:

 

www.ptshipwrights.com/wp/

www.facebook.com/PortTownsendShipwrightsCoOp?fref=ts

 

Salguero Marine:

 

a href="http://salgueromarine.com/" rel="nofollow">salgueromarine.com/

www.facebook.com/marinefinishes

 

Mystery Bay Sails and Canvas:

 

www.mysterybaysailscanvas.com/

=== = = = = = = = = == == ==

 

Best viewed @ large size

 

Verbenaceae - Taiwan

Taiwan Beautyberry

Shown: The strikingly unusual, rectangular configuration of the flower buds in their earliest stage of development

 

Additional views:

farm4.static.flickr.com/3353/3670026919_b500214565_b.jpg

farm4.static.flickr.com/3618/3670036043_33528f9c49_b.jpg

farm4.static.flickr.com/3119/3670861638_76bfdf8664_b.jpg

farm3.static.flickr.com/2433/3670076613_f87215ddd0_b.jpg

 

Photographed in U.C. Botanical Garden at Berkeley - Berkeley, California

+++ 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 P-74 "Charger" was a fighter aircraft built by Lockheed for the United States Army Air Forces (USAAF). Its configuration was unusual as it was designed as a twin boom pusher configuration, where the propeller is mounted in the rear of the fuselage, pushing the aircraft forward.

 

The P-74 entered service with the USAAF in late 1944, its conception dated back to 1939 when the U.S. Army Air Corps requested with the Circular Proposal R40C domestic manufacturers to develop high performance fighter types, allowing (even demanding) unusual configurations. Lockheed did not respond immediately and missed the chance to sign a development contract in mid-1940 until early 1941. Twenty-three proposals were submitted to R40C, and after a fist selection of ideas three companies, Vultee with the large XP-54 Swoose Goose, Curtiss with its XP-55 Ascender and Northrop's XP-56 Black Bullet were able to secure prototype contracts.

 

Vultee eventually won the competition, but all these innovative new aircraft suffered from various flaws or development delays, missing various performance goals, so that none ever entered service.

 

In the meantime, Lockheed had been working on the 1939 request in the background on a private venture basis, as it was clear that by 1944 a successor to the company's own P-38 Lightning had to be offered to the USAAC.

The new North American P-51 Mustang was also a sharp competitor, esp. for the Pacific conflict theatre where long range was needed. This role was filled out very well by the P-38, but it was a relatively large and complicated aircraft, so an alternative with a single engine was strived for. Even though jet engines already showed their potential, it was clear that the requested range for the new type could only be achieved through a piston engine.

 

This aircraft became the XP-74, originally christened “Laelaps”, following Lockheed’s tradition, after a female Greek mythological dog who never failed to catch what she was hunting. It was presented as a mock-up to USAAC officials on August 8th 1942 and immediately found sponsorship: with the disappointing results from the XP-54,55 and 56 was immediately ushered into the prototype stage. Its name, though, was rejected, and the more common name “Charger” was adopted.

 

Just like Lockheed’s successful P-38 the XP-74 Charger was designed as a twin-boom aircraft, but it was driven by only a single Packard (License-built Rolls Royce Merlin) V-1650 pusher engine in the aft part of the fuselage. The tail was mounted rearward between two mid-wing booms, with a four-bladed 12-ft propeller between them. The design also included a "ducted wing section" developed by the NACA that enabled installation of cooling radiators and intercoolers in the wing root section.

 

The advantages of a pusher design are that the view forward is unobstructed and armament can be concentrated in the nose, while a major drawback is difficulty in escaping from the aircraft in an emergency, as the pilot could get drawn into the propeller blades. Lockheed deliberated between systems that would eject the pilot, or jettison the propeller or the engine, via a system of explosive bolts. Lockheed eventually installed an early ejector seat which was driven by pressurized air, combined with a mechanism that would blow the canopy off. The system was successfully tested in summer 1943, even though skepticism remained among pilots.

 

Initial armament comprised one 20mm Hispano cannon and four 12.7mm Browning machine guns, the same as in the P-38, but two machine guns were relocated from the nose into the front ends of the tail booms because of the new aircraft’s smaller overall dimensions.

 

The first prototype was ready in October 1943, with a different engine and heavier armor fitted. The second prototype was built to this specification from the start, which would become the serial production standard, the P-74A.

The P-74A used the new V-1650-9 engine, a version of the Merlin that included Simmons automatic supercharger boost control with water injection, allowing War Emergency Power as high as 2,218 hp (1,500 kW). Another change concerned the armament: a longer weapon range was deemed necessary, so the gun armament was changed into four 20mm Hispano cannons, two of the placed in the fuselage nose and one in each tail boom front end. Each gun was supplied with 250 RPG.

 

Alternatively, a nose installment with a single 37mm cannon and two 12.7mm Browning MGs was tested on the first prototype, but this arrangement was found to be less effective than the four 20mm cannons. Another factor that turned this option down was the more complicated logistics demands for three different calibers in one aircraft.

 

The P-74A was ready for service in summer 1944, but its deployment into the Pacific region took until December – the 5th Air Force first units replaced most of its P-38 and also early P-47Ds with the P-74A.These new aircraft had their first clashes with Japanese forces in January 1945.

 

The P-74 was used in a variety of roles. It was designed as an intreceptor against bombers, but its good range and handling at all altitudes made it suitable for tasks like fighter sweeps against enemy airfields, support for U.S. ground forces and protection of sea convoys and transport routes.

While the P-74 could not out-turn the A6M Zero and most other Japanese fighters when flying below 200 mph (320 km/h), its superior speed coupled with a good rate of climb meant that it could utilize energy tactics, making multiple high-speed passes at its target. Also, its focused firepower was deadly to lightly armored Japanese warplanes.

 

Because of its late service introduction, only 305 P-74s were ever produced until the end of hostilities, and they were exclusively used in the Pacific theatre. The P-74's service record shows mixed results, but usually because of misinformation. P-74s have been described as being harder to fly than traditional, single-engined aircraft, but this was because of inadequate training in the first few months of service.

Another drawback was the ejection seat system – it worked basically well, but the tank for the pressurized air turned out to be very vulnerable to enemy fire. Several P-74s literally exploded in midair after cannon fire hits, and this poeblem could only be cured when the tank section behind the cockpit received a more rigid structure and additional armor. Anyway, the P-74 was quickly retired after WWII, as the USAAF focussed on P-47 and P-51.

  

General characteristics

Crew: 1

Length: 10.45 m (34 ft 3 in)

Wingspan: 11.6 m (38 ft 0 in)

Height: 3.97 (13 ft 0 in)

Wing area: 22.2 m² (238.87 ft²)

Empty weight: 3,250 kg (7,165 lb)

Loaded weight: 4,150 kg (9,149 lb)

Max. take-off weight: 4,413 kg (9,730 lb)

 

Powerplant:

1× Packard (License-built Rolls Royce Merlin) V-1650-9 ,

rated at 1,380 hp (1,030 kW) and 2,218 hp (1,500 kW) w. water injection

 

Performance

Maximum speed: 640 km/h (343 knots, 398 mph)

Cruise speed: 495 km/h (265 knots, 308 mph)

Range: 1,105 mi (1,778 km)

Ferry range: 1,330 nmi (1,530 mi, 2,460 km)

Service ceiling: 11,000 m (36,090 ft)

Rate of climb: 15 m/s (2,950 ft/min)

 

Armament

4× 20 mm (0.79 in) Hispano-Suiza HS.404 cannons with 250 RPG

2× hardpoints for up to 2,000 lb (907 kg) of bombs, 6 or 10× T64 5.0 in (127 mm) H.V.A.R rockets

  

The kit and its assembly:

This whif was inspired by a CG rendition of a Saab J21 in a natural metal finish and with (spurious) USAAF markings, probably a skin for a flight simulator. Anyway, I was more or less enchanted by the NMF on the Saab – I had to build one, and it would become the P-74, the only USAF fighter code that had never been used.

 

The kit is the venerable Heller Saab J21A, an “old style” design with raised panel lines. But it is still around and affordable. No big mods were made to the kit during its transition into a USAAF fighter, even though I changed some minor things:

● Main landing gear was completely exchanged through struts from an Airfix A-1 Skyraider and the wheels from a Hasegawa P-51D; thin wire was added as hydraulic tubes

● New propeller blades: instead of the three-bladed original I added four much broader blades with square tips (from a Heller P-51D) to the original spinner

● Different exhaust stubs, which actually belong to a Spitfire Merlin (Special Hobby kit)

● Underfuselage flap was slightly opened

● A pilot figure was added to the nice cockpit

● The gun barrels were replaced with hollow styrene tubes

  

Painting and markings:

NMF was certain, but the rest…? I wanted to have a colorful aircraft, and eventually settled for a machine in the Pacific theatre of operations. When I browsed for options I eventually decided to apply broad black stripes on wings and fuselage, typical 5th Air Force markings that were used e. g. on P-47Ds and P-51Ds.

 

Overall design benchmark for my aircraft is a P-47D-28 of 310th FS/58th FG. The tail would be all white, and the rudder sported red and white stripes, early war insignia. The red nose trim and the deep yellow spinner were taken over from this aircraft, too. The blue individual code number is a personal addition, as well as the nose art, which was puzzled together from a Czech 'Perdubice' Meeting MiG-21 and leftover bits from a Pacific use P-51.

 

The aircraft was basically painted with Aluminum Metallizer (Humbrol 27002) and Polished Steel Metallizer (Modelmaster), and some panels were contrasted with Aluminum (Humbrol 56).

The anti-glare panel in front of the cockpit was painted in Olive Drab (Humbrol 66), the red nose trim with Humbrol 19. The tail was painted with a mix of Humbrol 34 & 196, for a very light grey, and later dry-painted with pure white.

 

The black ID stripes as well as the red and blue rudder trim were not painted, but rather created through decal sheet material (from TL Modellbau), cut to size and shape to fit into their respective places. The tail was a PITA, but for the black stripes this turned out to be very effective and convenient - an experiment that willcertainly see more future use.

 

Cockpit interior was painted in Humbrol 226 (Cockpit Green) and Zinc Chromate Green from Model Master, the landing gear wells received a chrome yellow primer (Humbrol 225) finish.

The landing gear struts were kept in bare Aluminum.

 

For weathering the kit received a rubbing treatment with grinded graphite, which adds a dark, metallic shine and emphasizes the kit’s raised panel lines. Some dry painting with Aluminum was added, too, simulating chipped paint on the leading edges, and on the black ID stripes some dark grey shading was added.

  

A relatively simple whif, but I love how the Saab 21 looks in the unusual, shiny NMF finish - and the USAAF markings with the prominent ID stripes suit it well, even though it looks a bit like a circus attraction now?

EdgeIQ provides a full suite of device management solutions. Our local service running on the local gateway communicates directly with the device and delivers full configuration updates, software updates, and monitors the device health and wellness for correct operation. Visit: www.edgeiq.io/field-service

Company/Owner: Riding Public First Joint Venture, Inc. (Bulacan P2P RPF)

Fleet/Bus Number: 1902

Classification: Air-conditioned Point-to-Point (P2P) Provincial Bus

Coachbuilder: (Suzhou) Higer Bus Company, Ltd.

Body Model: Higer B92 KLQ6129G

Engine Model: Yuchai YC6G270-40 (GA1*A)

Chassis Model: Higer KLQ61***

Transmission: 6-speed Manual Transmission

Suspension: Leaf Spring Suspension

Seating Configuration: 2×2; side-facing seats

Seating Capacity: 50

Franchise route: TBD

Route TriNoma / SM City North, Quezon City [NST, QC]–Primark Plaridel, Plaridel, Bulacan via NLEX-Sta. Rita Exit

Pickup/drop-off points: Waltermart Plaridel

Cities/municipalities passing: Santa Rita (Guiguinto)

Type of Operation: Provincial Operation Public Utility Bus (Premium Point-to-Point Regular Class)

Area of Operation: Central Luzon (Region III)

 

Shot location: NLEX-Turo, Bocaue, Bulacan

Date and time taken: April 6, 2024 (5:25 pm)

 

Notices:

* Please DON'T GRAB A PHOTO WITHOUT A PERMISSION. If you're going to GRAB IT, please give A CREDIT TO THE OWNER. Also, don't PRINT SCREEN my photos. Do not (re)upload this in any social media platforms (especially in YouTube and TikTok).

** If I have mistakes on the specifications, please comment in a good manner so that I can edit it immediately.

*** The specifications and routes (for provincial, inter-provincial, and city operation) mentioned above are subjected for verification and may be changed without prior notice.

**** The vehicle's registration plate(s), conduction sticker(s), and/or persons (if applicable) were pixelated/blurred to prevent any conflict with the photographer, the bus company and/or to the car owner for their security and/or privacy purposes. So, don't use their plate number, conduction sticker, and vehicle tag as an evidence for any incident. And, I have taken this photo for bus fanatics, bus enthusiasts, and bus lovers purposes.

First North Luzon Transit Inc. 2914

 

Bus Number:2914

Route:Cubao-Hagonoy Via Tabang/Malolos/Paombong

Seating Configuration:2x3

Engine:KMJP1C

Chasis:D6AC

Taken At:Sta Elena,Hagonoy,Bulacan

1960 diagram of a Centaur upper stage, with an Atlas first stage, a configuration used often since the development of Centaur.

In the late 1950s and early 1960s, Centaur was proposed as a high energy upper stage for the Saturn I, Saturn IB, and Saturn V rockets under the designation "S-V", in accordance with the numbering of Saturn rocket stages. Centaur development was too slow however, and never flew on any Saturn vehicle. The first test flight in May 1962 was unsuccessful.

 

Pertinent extract from the "Saturn Illustrated Chronology - Part 1: April 1957 through December 1960":

 

"On March 13 ABMA submitted to ARPA the results of the Saturn System Study. This study indicated that either an Atlas or a Titan could be used as the second stage of the proposed vehicle. During May ARPA decided that modified Titan hardware could be used for the second stage and that the third stage could use a slightly modified Centaur vehicle."

 

ICW the diagram (with slight variation), as figure no. 9:

 

history.nasa.gov/MHR-5/Images/fig009.jpg

 

Excellent (as always) additional amplifying info:

 

heroicrelics.org/info/saturn-i-and-ib/saturn-ib-centaur.html

Credit: Mike Jetzer/heroicrelics.org

 

And:

www.hughesscgheritage.com/the-atlas-centaur-story-jack-fi...

Credit: Hughes Aircraft Company blog site

 

The same figure also within this excellent article:

 

www.drewexmachina.com/2015/03/02/the-launch-of-atlas-cent...

Credit: Drew Ex Machina/Andrew LePage

Detail of one window featuring dozens of self-closing apertures.

 

Reminds me of a cross between Hellraiser's Lament Configuration and the opening segment of a James Bond flick...

Neither SPIELBURG, LUCAS, nor DeMILLE can NEVER say that THEY can TOP ... The ORIGINAL...

 

NOW or **EVER!!**

september 2014, some naked guy singing by the canal, some drug dealers near FLEX, some people having a night walk, a city lit and cars going and coming. I got no ispirations and the more I get in depth of neural networks, the more I find hard to choose a system configuration for my project. So..

新北市新店區Xindian District, New Taipei City

Camera Model : Canon EOS 7D Mark II

Shooting Mode : Manual Exposure

Tv( Shutter Speed ) : 1/3200

Av( Aperture Value ) : 5.6

Metering Mode : Evaluative Metering

ISO Speed : 1000

Lens : EF400mm f/5.6L USM

Focal Length : 400.0mm

White Balance Mode : Auto

AF Mode : AI Servo AF

AF Configuration Tool : Case 4

AF area select mode : Manual selection

Picture Style : Standard

Sharpness : 7

Contrast : -2

Saturation : 1

Color tone : 0

影像品質 : RAW(Adobe Photoshop Lightroom)轉JPEG檔

影像後製軟體 : Adobe Photoshop Lightroom 5

版權所有不得轉載 © All rights reserved

 

Please don't use this image on websites, blogs or other media

Variable configuration SAR drone.

Can configure its footprint and dimensions to pass through multitude of confined spaces to search for survivors in tunnels and mineshafts.

 

A late tablescrap build for Droneuary...

Operator: Saint Rose Transit, Incorporated

Bus #: 8829

Classification: Ordinary Fare City Operation Bus

MMDA OBR Classification: Bus A

Coachbuilder: Partex Auto Body

Model: Nissan Diesel-Partex body*

Chassis: Nissan Diesel CPB87N*

Engine: Nissan Diesel FE6B*

Engine location: Front

A/C system: N/A

Seating Configuration: 2x3

Seating Capacity: 54 passengers

Route: Pacita Complex - SM Fairview via EDSA

Shot Location: Pacita Complex, San Pedro, Laguna

 

*needs verification

Tribute to ANDREW RIDGELEY and GEORGE MICHAEL who once both happened to be something called WHAM!

Split Rail Fence a common fence construction in the pioneer days, lot of wood arounf, cut and stacked in this configuration made a pretty secure fence. Shot in the Carolina's

Different configurations of the Altum Invidia fusion rifle.

 

[LEFT - Overcharge Barrel]

A particle acceleration system mounted on the barrel in addition to an energy amplifier mounted underneath the stock enables the weapon to fire supercharged bolts of Arc energy that explode on impact. This comes at the cost of a lengthened charge time.

 

[RIGHT - Assault Sights]

The removal of the scope and modifications to the rifle barrel grants shortened charging time at the expense of damage output.

 

The main weapon can be found here:

www.flickr.com/photos/125667481@N02/48164745547/in/datepo...

Bus no.: 767 "Rosenda"

Classification: Airconditioned Provincial Operation Bus

Seating Configuration: 2x2

Seating Capacity: 49 Passengers

Model: SR 620 NV Series

Manufacturer: Santarosa Motor Works Inc. Philippines

Chassis: JA450SSN

Engine: Nissan Diesel PF6-A

Suspension: Leaf Spring Suspension

(Note: Specification are subjected for verification and may be changed without prior notice.)

 

Shot Location: Gen. Romulo Blvd. Cubao, Quezon City

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