(cont.) ...MDOT has altered the configuration of this interchange, for the major benefit of this one specific off-ramp to boot. There are now three lanes here, and the traffic signal controls two. There's still the one lane that turns left (302 west, to Horn Lake), but there's also a dedicated right-turn lane at the stoplight, which takes you to the northern portion of Southcrest Parkway (leading to the hospital, hence the blue “H” tacked atop the sign here. Personally, I believe the “H” ought to have been made a permanent part of the sign itself, or MDOT could even have had the sign read “Hospital” in addition to the relatively lesser-known “Southcrest Pkwy,” but I digress.). Then, you've also got the existing “country,” non-signalized right-turn lane that has also been allowed to remain intact.

Why the two right-turn lanes? Well, to solve the issue of the drivers sweeping across mulitple lanes of traffic, of course! On Goodman Road itself – which we'll see momentarily – the large center median has been removed, in favor of new, parking-lot-bumper-style barricades. These barricades serve to essentially “trap” drivers in the lanes they are in. That sounds like it's a bad thing, but I promise, it's not! (cont.)

(c) 2018 Retail Retell

These places are public so these photos are too, but just as I tell where they came from, I'd appreciate if you'd say who :)

SLS Engine Section Barrel Hot off the Vertical Weld Center at Michoud

The barrel for the engine section of NASA's new rocket, the Space Launch System, is taken off the Vertical Weld Center at NASA's Michoud Assembly Facility in New Orleans. The barrel is flight hardware to be used on the first uncrewed test flight of the 70-metric-ton configuration of the rocket. The engine section, made up of the barrel and a ring -- also welded at Michoud -- will hold four RS-25 engines that will power the core stage of the SLS. The core stage, towering more than 200 feet tall with a diameter of 27.5 feet, will store cryogenic liquid hydrogen and liquid oxygen that will feed the vehicle’s RS-25 engines.

The Vertical Weld Center is part of a family of state-of-the-art tools at Michoud that is being used to build the core stage. Along with the engine section, it will weld barrel panels together to produce whole barrels for the SLS two pressurized tanks, the intertank and the forward skirt. It stands about three stories tall and weighs 150 tons.

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 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 two pistols are definitely wheellock mechanisms. The fact that neither pistol is equipped with a front blade sight leads me to believe that the pair were included in a cased set of dueling pistols. The long arm is not familiar to me. The wooden stock and the firing mechanism are unusual in configuration. I welcome any suggestions as to place of origin and date of manufacture.

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)

Main photo: www.flickr.com/photos/188464565@N06/50186109438/in/datepo...

Things that I've changed/tweaked from the original configuration of my joe appaloosa

Once again...STUNNING!!

'Nuff Said!!!!

+++ 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?

Perhaps this seat lug configuration is the finest work on the frame..well it is in my opinion..and I wish that I had made it.

In this joint the top tube has a decorative reinforcement sleeve brazed on while the back of the seat tube has a very attractive plate onto which are brazed two seat-bolts.

The rear brake cable having run along the inside of the top-tube passes through a tube which itself passes through the seat tube - a very direct cable routing often used on cyclo-cross frames.

I suspect that the seat pillar has been shortened and stops just above the small cable tube.- hence the need for a very strong seat lug and clamping device. Some builders cut a slot along the length of the seat pillar to the point where the cable will pass. This facilty enables the pillar to be adjusted in height.

The other fine point of this cluster is in fact the point at the end of the seat-stay. This has been very skillfully profiled and then brazed into place..finished with excellent filing of the joint.

It's apity that the frame is spoiled to a lesser extent by not having two AK bolts in the seat-pillar clamp.

Well...come on..it's difficult to find any fault with this seat cluster.

+++ DISCLAIMER +++

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

The KAI T-50 Golden Eagle (골든이글) is a family of South Korean supersonic advanced trainers and light combat aircraft, developed by Korea Aerospace Industries (KAI) with Lockheed Martin. The T-50 is South Korea's first indigenous supersonic aircraft and one of the world's few supersonic trainers.

The first four Scottish Golden Hawk TF.1 aircraft were allocated to the newly established RoScAC No. 2 Squadron, based at Leuchars, where the RoScAC took control from the British Army. The latter had just taken over the former air base from the RAF in 2015, losing its “RAF air base” status and was consequentially re-designated “Leuchars Station”, primarily catering to the Royal Scots Dragoon Guards who have, in the meantime, become part of Scotland’s Army Corps. The brand new machines were publically displayed on the shared army and air corps facility in the RoScAC’s new paint scheme on 1st of December 2019 for the first time, and immediately took up service.

General characteristics:

Crew: 2

Length: 13.14 m (43.1 ft)

Wingspan (with wingtip missiles): 9.45 m (31 ft)

Height: 4.94 m (16.2 ft)

Wing area: 23.69 m² (255 ft²)

Empty weight: 6,470 kg (14,285 lb)

Max. takeoff weight: 12,300 kg (27,300 lb)

Powerplant:

1× Volvo RM12 afterburning turbofan, rated at 54 kN (12,100 lbf) dry thrust

and 80.5 kN (18,100 lbf) with afterburner

Performance:

Maximum speed: Mach 1.5 (1,640 km/h, 1,020 mph at 9,144 m or 30,000 ft)

Range: 1,851 km (1,150 mi)

Service ceiling: 14,630 m (48,000 ft)

Rate of climb: 198 m/s (39,000 ft/min)

Thrust/weight: 0.96

Max g limit: -3 g / +8 g

Armament:

1× 27mm Mauser BK-27 revolver cannon with 120 rounds

A total of 7 hardpoints (4 underwing, 2 wingtip and one under fuselage)

for up to 3,740 kg (8,250 lb) of payload

The kit and its assembly:

A rare thing concerning my builds: an alternative reality whif. A fictional air force of an independent Scotland crept into my mind after the hysterical “Brexit” events in 2016 and the former (failed) public vote concerning the independence of Scotland from the UK. What would happen to the military, if the independence would take place, nevertheless, and British forces left the country?

The aforementioned Scottish National Party (SNP) paper from 2013 is real, and I took it as a benchmark. Primary focus would certainly be set on air space defense, and the Gripen appears as a good and not too expensive choice. The Sk 90 is a personal invention, but would fulfill a good complementary role.

Nevertheless, another multi-role aircraft would make sense as an addition, and both M-346 and T-50 caught my eye (Russian options were ruled out due to the tense political relations), and I gave the TA-50 the “Go” because of its engine and its proximity to the Gripen.

The T-50 really looks like the juvenile offspring from a date between an F-16 and an F-18. There’s even a kit available, from Academy – but it’s a Snap-Fit offering without a landing gear but, as an alternative, a clear display that can be attached to the engine nozzle. It also comes with stickers instead of waterslide decals. This sounds crappy and toy-like, but, after taking a close look at kit reviews, I gave it a try.

And I am positively surprised. While the kit consists of only few parts, moulded in the colors of a ROCAF trainer as expected, the surfaces have minute, engraved detail. Fit is very good, too, and there’s even a decent cockpit that’s actually better than the offering of some “normal” model kits. The interior comes with multi-part seats, side consoles and dashboards that feature correctly shaped instrument details (no decals). The air intakes are great, too: seamless, with relatively thin walls, nice!

So far, so good. But not enough. I could have built the kit OOB with the landing gear tucked up, but I went for the more complicated route and trans-/implanted the complete landing gear from an Intech F-16, which is available for less than EUR 5,- (and not much worth, to be honest). AFAIK, there’s white metal landing gear for the T-50 available from Scale Aircraft Conversions, but it’s 1:48 and for this set’s price I could have bought three Intech F-16s…

But back to the conversion. This landing gear transplantation stunt sounds more complicated as it actually turned out to be. For the front wheel well I simply cut a long opening into the fuselage and added inside a styrene sheet as a well roof, attached under the cockpit floor.

For the main landing gear I just opened the flush covers on the T-50 fuselage, cut out the interior from the Intech F-16, tailored it a little and glued it into its new place.

This was made easy by the fact that the T-50 is a bit smaller than the F-16, so that the transplants are by tendency a little too large and offer enough “flesh” for adaptations. Once in place, the F-16 struts were mounted (also slightly tailored to fit well) and covers added. The front wheel cover was created with 0.5 mm styrene sheet, for the main covers I used the parts from the Intech F-16 kit because they were thinner than the leftover T-50 fuselage parts and feature some surface detail on the inside. They had to be adapted in size, though. But the operation worked like a charm, highly recommended!

Around the hull, some small details like missing air scoops, some pitots and antennae were added. In a bout of boredom (while waiting for ordered parts…) I also added static dischargers on the aerodynamic surfaces’ trailing edges – the kit comes with obvious attachment points, and they are a small detail that improves the modern look of the T-50 even more.

Since the Academy kit comes clean with only a ventral drop tank as ordnance, underwing pylons from a SEPECAT Jaguar (resin aftermarket parts from Pavla) and a pair of AGM-65 from the Italeri NATO Weapons set plus launch rails were added, plus a pair of Sidewinders (from a Hasegawa AAM set, painted as blue training rounds) on the wing tip launch rails.

Since the T-50 trainer comes unarmed, a gun nozzle had to be added – its position is very similar to the gun on board of the F-16, on the upper side of the port side LERX. Another addition are conformal chaff/flare dispensers at the fin’s base, adding some beef to the sleek aircraft.

Painting and markings:

I did not want a grey-in-grey livery, yet something “different” and rather typical or familiar for the British isles. My approach is actually a compromise, with classic RAF colors and design features inspired by camouflage experiments of the German Luftwaffe on F-4F Phantoms and Alpha Jets in the early Eighties.

For the upper sides I went for a classic British scheme, in Dark Green and Dark Sea Grey (Humbrol 163 and 164), colors I deem very appropriate for the Scottish landscape and for potential naval operations. These were combined with elements from late RAF interceptors: Barley Grey (Humbrol 167) for the flanks including the pylons, plus Light Aircraft Grey (Humbrol 166) for the undersides, with a relatively high waterline and a grey fin, so that a side or lower view would rather blend with the sky than the ground below.

Another creative field were the national markings: how could fictional Scottish roundels look like, and how to create them so that they are easy to make and replicate (for a full set for this kit, as well as for potential future builds…)? Designing and printing marking decals myself was an option, but I eventually settled for a composite solution which somewhat influenced the roundels’ design, too.

My Scottish roundel interpretationconsists of a blue disk with a white cross – it’s simple, different from any other contemporary national marking, esp. the UK roundel, and easy to create from single decal parts. In fact, the blue roundels were die-punched from blue decal sheet, and the cross consists of two thin white decal strips, cut into the correct length with the same stencil, using generic sheet material from TL Modellbau.

Another issue was the potential tactical code, and a small fleet only needs a simple system. Going back to a WWII system with letter codes for squadrons and individual aircraft was one option, but, IMHO, too complicated. I adopted the British single letter aircraft code, though, since this system is very traditional, but since the RoScAC would certainly not operate too many squadrons, I rather adapted a system similar to the Swedish or Spanish format with a single number representing the squadron. The result is a simple 2-digit code, and I adapted the German system of placing the tactical code on the fuselage, separated by the roundel. Keeping British traditions up I repeated the individual aircraft code letter on the fin, where a Scottish flag, a small, self-printed Fife coat-or-arms and a serial number were added, too.

The kit saw only light weathering and shading, and the kit was finally sealed with matt acrylic varnish (Italeri).

Creating this whif, based on an alternative historic timeline with a near future perspective, was fun – and it might spawn more models that circle around the story. A Scottish Sk 90 and a Gripen are certain options (and for both I have kits in the stash…), but there might also be an entry level trainer, some helicopters for the army and SAR duties, as well as a transport aircraft. The foundation has been laid out, now it’s time to fill Scotland’s history to come with detail and proof. ;-)

Besides, despite being a snap-fit kit, Academy’s T-50 is a nice basis, reminding me of some Hobby Boss kits but with less flaws (e .g. most of the interiors), except for the complete lack of a landing gear. But with the F-16 and Jaguar transplants the simple kit developed into something more convincing.

Artist's view of the configuration of Ariane 6 using four boosters (A64).

ESA and European industry are currently developing a new-generation launcher: Ariane 6. This follows the decision taken at the ESA Council meeting at Ministerial level in December 2014, to maintain Europe’s leadership in the fast-changing commercial launch service market while responding to the needs of European institutional missions.

This move is associated with a change in the governance of the European launcher sector, based on a sharing of responsibility, cost and risk by ESA and industry.

The participating states are: Austria, Belgium, France, Germany, Ireland, Italy, Netherlands, Norway, Romania, Spain, Sweden and Switzerland.

Credit: ESA–David Ducros, 2016

The Volkswagen Type 2, officially known as the Transporter or informally as Bus (US) or Camper (UK), was a panel van introduced in 1950 by German automaker Volkswagen as its second car model – following and initially deriving from Volkswagen's first model, the Type 1 (Beetle), it was given the factory designation Type 2.

As one of the forerunners of the modern cargo and passenger vans, the Type 2 gave rise to competitors in the United States and Europe, including the Ford Econoline, the Dodge A100, and the Corvair 95 Corvan, the latter adopting the Type 2's rear-engine configuration. European competition included the Renault Estafette and the Ford Transit. As of January 2010, updated versions of the Type 2 remain in production in international markets— as a passenger van, as a cargo van, and as a pickup truck.

Like the Beetle, the van has received numerous nicknames worldwide, including the "microbus", "minibus", "kombi" and, due to its popularity during the counterculture movement of the 1960s, "hippie van".

The concept for the Type 2 is credited to Dutch Volkswagen importer Ben Pon. (It has similarities in concept to the 1920s Rumpler Tropfenwagen and 1930s Dymaxion car by Buckminster Fuller, neither of which reached production.) Pon visited Wolfsburg in 1946, intending to purchase Type 1s for import to Holland, where he saw an improvised parts-mover and realized something better was possible using the stock Type 1 pan. He first sketched the van in a doodle dated April 23, 1947, proposing a payload of 690 kg (1,500 lb) and placing the driver at the very front. Production would have to wait, however, as the factory was at capacity producing the Type 1.

When capacity freed up a prototype known internally as the Type 29 was produced in a short three months. The stock Type 1 pan proved to be too weak so the prototype used a ladder chassis with unit body construction. Coincidentally the wheelbase was the same as the Type 1's. Engineers reused the reduction gear from the Type 81, enabling the 1.5 ton van to use a 25 hp (19 kW) flat four engine.

Although the aerodynamics of the first prototypes were poor (with an initial drag coefficient of 0.75), engineers used the wind tunnel at the Technical University of Braunschweig to optimize the design. Simple changes such as splitting the windshield and roofline into a "vee" helped the production Type 2 achieve a drag coefficient of 0.44, exceeding the Type 1's 0.48. Volkswagen's new chief executive officer Heinz Nordhoff (appointed 1 January 1948) approved the van for production on 19 May 1949 and the first production model, now designated Type 2, rolled off the assembly line to debut 12 November. Only two models were offered: the Kombi (with two side windows and middle and rear seats that were easily removable by one person), and the Commercial. The Microbus was added in May 1950, joined by the Deluxe Microbus in June 1951. In all 9,541 Type 2s were produced in their first year of production.

An ambulance model was added in December 1951 which repositioned the fuel tank in front of the transaxle, put the spare tire behind the front seat, and added a "tailgate"-style rear door. These features became standard on the Type 2 from 1955 to 1967. 11,805 Type 2s were built in the 1951 model year. These were joined by a single-cab pickup in August 1952, and it changed the least of the Type 2s until all were heavily modified in 1968.

Unlike other rear engine Volkswagens, which evolved constantly over time but never saw the introduction of all-new models, the Transporter not only evolved, but was completely revised periodically with variations retrospectively referred to as versions "T1" to "T5" (a nomenclature only invented after the introduction of the front-drive T4 which repaced the T25) However only generations T1 to T3 (or T25 as it is still called in Ireland and Great Britain) can be seen as directly related to the Beetle (see below for details).

The Type 2, along with the 1947 Citroën H Van, are among the first 'forward control' vans in which the driver was placed above the front roadwheels. They started a trend in Europe, where the 1952 GM Bedford CA, 1959 Renault Estafette, 1960 BMC Morris J4, and 1960 Commer FC also used the concept. In the United States, the Corvair-based Chevrolet Corvan cargo van and Greenbrier passenger van went so far as to copy the Type 2's rear-engine layout, using the Corvair's horizontally-opposed, air-cooled engine for power. Except for the Greenbrier and various 1950s–70s Fiat minivans, the Type 2 remained unique in being rear-engined. This was a disadvantage for the early "barndoor" Panel Vans, which couldn't easily be loaded from the rear due to the engine cover intruding on interior space, but generally advantageous in traction and interior noise.

The Type 2 was available as a:

Panel van, a delivery van without side windows or rear seats.

Nippen Tucket, available in six colours, with or without doors.

Walk-Through Panel Van, a delivery van without side windows or rear seats and cargo doors on both sides.

High Roof Panel Van (German: Hochdach), a delivery van with raised roof.

Kombi, from German: Kombinationskraftwagen (combination motor vehicle), with side windows and removable rear seats, both a passenger and a cargo vehicle combined.

Bus, also called a Volkswagen Caravelle, a van with more comfortable interior reminiscent of passenger cars since the third generation.

Samba-Bus, a van with skylight windows and cloth sunroof, first generation only, also known as a Deluxe Microbus. They were marketed for touring the Alps,

Flatbed pickup truck, or Single Cab, also available with wider load bed.

Crew cab pick-up, a flatbed truck with extended cab and two rows of seats, also called a Doka, from German: Doppelkabine.

Westfalia camping van, "Westy", with Westfalia roof and interior.

Adventurewagen camping van, with high roof and camping units from Adventurewagen.

Semi-camping van that can also still be used as a passenger car and transporter, sacrificing some camping comforts. "Multivan" or "Weekender", available from the third generation on.

Apart from these factory variants, there were a multitude of third-party conversions available, some of which were offered through Volkswagen dealers. They included, but were not limited to, refrigerated vans, hearses, ambulances, police vans, fire engines and ladder trucks, and camping van conversions by companies other than Westfalia. There were even 30 Klv 20 rail-going draisines built for Deutsche Bundesbahn in 1955.

The first generation of the Volkswagen Type 2 with the split windshield, informally called the Microbus, Splitscreen, or Splittie among modern fans, was produced from 8 March 1950 through the end of the 1967 model year. From 1950–1956, the T1 was built in Wolfsburg; from 1956, it was built at the completely new Transporter factory in Hanover. Like the Beetle, the first Transporters used the 1100 Volkswagen air cooled engine, an 1,131 cc (69.0 cu in), DIN-rated 18 kW (24 PS; 24 bhp), air-cooled flat-four cylinder 'boxer' engine mounted in the rear. This was upgraded to the 1200 – an 1,192 cc (72.7 cu in) 22 kW (30 PS; 30 bhp) in 1953. A higher compression ratio became standard in 1955; while an unusual early version of the 30 kW (41 PS; 40 bhp) engine debuted exclusively on the Type 2 in 1959. This engine proved to be so uncharacteristically troublesome that Volkswagen recalled all 1959 Transporters and replaced the engines with an updated version of the 30 kW engine. Any 1959 models that retain that early engine today are true survivors. Since the engine was totally discontinued at the outset, no parts were ever made available.

The early versions of the T1 until 1955 were often called the "Barndoor" (retrospectively called T1a since the 1990s), owing to the enormous rear engine cover, while the later versions with a slightly modified body (the roofline above the windshield is extended), smaller engine bay, and 15" roadwheels instead of the original 16" ones are nowadays called the T1b (again, only called this since the 1990s, based on VW's restrospective T1,2,3,4 etc. naming system.). From the 1964 model year, when the rear door was made wider (same as on the bay-window or T2), the vehicle could be referred to as the T1c. 1964 also saw the introduction of an optional sliding door for the passenger/cargo area instead of the outwardly hinged doors typical of cargo vans. This change arguably makes the 1964 Volkswagen the first true minivan, although the term wouldn't be coined for another two decades.

In 1962, a heavy-duty Transporter was introduced as a factory option. It featured a cargo capacity of 1,000 kg (2,205 lb) instead of the previous 750 kg (1,653 lb), smaller but wider 14" roadwheels, and a 1.5 Le, 31 kW (42 PS; 42 bhp) DIN engine. This was so successful that only a year later, the 750 kg, 1.2 L Transporter was discontinued. The 1963 model year introduced the 1500 engine – 1,493 cc (91.1 cu in) as standard equipment to the US market at 38 kW (52 PS; 51 bhp) DIN with an 83 mm (3.27 in) bore, 69 mm (2.72 in) stroke, and 7.8:1 compression ratio. When the Beetle received the 1.5 L engine for the 1967 model year, its power was increased to 40 kW (54 PS; 54 bhp) DIN.

1966 Volkswagen Kombi (North America)

German production stopped after the 1967 model year; however, the T1 still was made in Brazil until 1975, when it was modified with a 1968–79 T2-style front end, and big 1972-vintage taillights into the so-called "T1.5" and produced until 1996. The Brazilian T1s were not identical to the last German models (the T1.5 was locally produced in Brazil using the 1950s and 1960s-era stamping dies to cut down on retooling, alongside the Beetle/Fusca, where the pre-1965 body style was retained), though they sported some characteristic features of the T1a, such as the cargo doors and five-stud 205 mm (8.1 in) PCD) rims.

VW Bus Type 2 (T1), hippie colors

Among American enthusiasts, it is common to refer to the different models by the number of their windows. The basic Kombi or Bus is the 11-window (a.k.a. three-window bus because of three side windows) with a split windshield, two front cabin door windows, six rear side windows, and one rear window. The DeLuxe model featured eight rear side windows and two rear corner windows, making it the 15-window (not available in Europe). Meanwhile, the sunroof DeLuxe with its additional eight small skylight windows is, accordingly, the 23-window. From the 1964 model year, with its wider rear door, the rear corner windows were discontinued, making the latter two the 13-window and 21-window respectively. The 23- and later 21-window variants each carry the nickname 'Samba', or in Australia, officially 'Alpine'.

Certain models of the Volkswagen Type 2 played a role in an historic episode during the early 1960s, known as the Chicken War. France and West Germany had placed tariffs on imports of U.S. chicken. Diplomacy failed, and in January 1964, two months after taking office, President Johnson imposed a 25% tax (almost 10 times the average U.S. tariff) on potato starch, dextrin, brandy, and light trucks. Officially, the tax targeted items imported from Europe as approximating the value of lost American chicken sales to Europe.

In retrospect, audio tapes from the Johnson White House, revealed a quid pro quo unrelated to chicken. In January 1964, President Johnson attempted to convince United Auto Workers' president Walter Reuther not to initiate a strike just prior to the 1964 election, and to support the president's civil rights platform. Reuther, in turn, wanted Johnson to respond to Volkswagen's increased shipments to the United States.

The Chicken Tax directly curtailed importation of German-built Type 2s in configurations that qualified them as light trucks – that is, commercial vans (panel vans) and pickups. In 1964, U.S. imports of automobile trucks from West Germany declined to a value of $5.7 million – about one-third the value imported in the previous year. After 1971, Volkswagen cargo vans and pickup trucks, the intended targets, "practically disappeared from the U.S. market". While post-1971 Type 2 commercial vans and single-cab and double-cab pickups can be found in the United States today, they are exceedingly rare. As of 2009, the Chicken tax remains in effect.

(Source Wikipedia)

United Airlines Boeing 787-9 Dreamliner N61101 cn 68647/1267 IAD 100 Years Anniversary stickers Premium high configuration aircraft

"what do you make of that planetoid beyond"

"...is class D... made up of many unremarkable ores... essentially a great rock in space"

“The first flight configuration of the giant Saturn C-1 rocket is seen in the Fabrication and Assembly Engineering Division at the George C. Marshall Space Flight Center, National Aeronautics and Space Administration, Huntsville, Ala. Dwarfed by the 180-foot C-1 are a Juno II rocket (left rear) and a Mercury-Redstone rocket (front foreground). The C-1 will be capable of placing about 10 tons into low earth orbit.”

An iconic photo.

An extract from the Space Launch Report website pertaining to SA-1:

WHICH OF COURSE/UNFORTUNATELY HAS GONE POOF.

“...Trial horizontal assembly of complete vehicle at MSFC in February 1961."

At:

www.spacelaunchreport.com/satstg.html

So...it must indeed be SA-1? They wouldn’t "trial horizontally assemble" a subsequent vehicle, right?

1. September Configuration, 2. Floating, 3. Sunset Colours, 4. Paddling and Jetskiing, 5. Beachgoers, 6. Spaghetti Amatriciana., 7. New Traffic Lights, 8. Violet Sea and Sky, 9. Hibiscus, 10. Crossing Over, 11. Airport Queue, 12. Empty Cocktail Glasses, 13. Alex and the Praying Mantis, 14. Raisins Drying, 15. Reflection, 16. Bar Paraphernalia, 17. Table for Twelve, 18. Taverna Sign, 19. Checking Facebook, 20. India, 21. Bedtime Story, 22. Me and My Girls, 23. Ezra Baptism, 24. Beach Games, 25. Cheryl, 26. Coolest Dude on the Beach, 27. Toddler at the Bar, 28. Hotel Balcony, 29. Brindisi Ferry, 30. Airport Reunion, 31. Taking to the Sea, 32. Dinner at Freddie's

Created with fd's Flickr Toys

Revolutionary design by Marcello Gandini’s (Bertone) sleek styling is the benchmark of sports car design: Cab-forward styling, with shortened front end and longer tail section

Racecar served as ambitious sports car

In 1965 at the Turin Autoshow Lamborghini instigated the trend of high performance, two-seater, mid-engined sports cars.

At launch in 1966 it was the fastest production road car available.

Manufacturing period: 1966 – 1973

Units: 275 (P400: 1966-1969) / 764 (all P400 versions: P400 / S (1968-1971: 338) / SV (1971-1973: 150) / Jota / SV/J / Roadster / SV J Spider)

Top speed: 280 km/h

Empty weight: 1125 kg (S / SV: 1298 kg)

Designer: Marcello Gandini @ Bertone

Cylinders: 12 (60 degree angle / V-configuration)

Displacement: 3929 cc

Rated output: 257 KW / 350 PS @ 7000 rpm (S: 370 PS @ 7700 rpm / SV: 385 PS @ 7700 rpm)

Valvetrain: Two overhead camshafts per cylinder bank, chain driven, bucket tappets

Operation: 4-stroke petrol engine with four Weber IDL40 3C 3bbl downdraught carburetors

Bore x stroke: 82 x 62 mm

Cooling system: Liquid cooled with pump

Engine block: Full alloy

Configuration - 45º V16

Location - Mid, longitudinally mounted

Construction - Aluminium block, light alloy head

Displacement - 6.006 litre / 366.5 cu in

Bore / Stroke - 75.0 mm (3 in) / 85.0 mm (3.3 in)

Compression - 9.2:1

Valvetrain - 2 valves / cylinder, OHV

Fuel feed - 2 Solex Carburettors

Aspiration - Roots-Type Supercharger

Power - 520 bhp / 388 KW @ 5000 rpm

Torque - 850 Nm / 627 ft lbs @ 2500 rpm

BHP/Liter - 87 bhp / litre

Goodwood Festival of Speed 2011

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 brown painted wood is the mast step). The work was done by shipwright Chris Chase, assisted by Paul Lyter. The owner will finish the temporary interior beams and woodwork.

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.

www.ptshipwrights.com/wp/

www.facebook.com/PortTownsendShipwrightsCoOp?fref=ts

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

www.facebook.com/marinefinishes

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

INSTRUCTIONS AVAILABLE FOR P558 SUPERDUTY - MULTIPLE CONFIGURATIONS

On September 24, 2015, Ford unveiled the 2017 Ford Super Duty line at the 2015 State Fair of Texas. he frame is made from 95% high strength steel and the body (like the contemporary F-150) is made from 6000 series aluminum alloy. For the first time since 1999, both the Super Duty and F-150 lines are constructed using the same cab.

For 2017 production, the Super Duty line shares its powertrain lineup with its 2016 predecessor: a 6.2L gasoline V8, 6.8L V10 (F-450 and above), with a 6.7L diesel V8 available in all versions. The 6.2L gasoline V8 engine remains at 385 hp but torque rises from 405 lb-ft to 430 lb-ft. Additionally, the gasoline V8 produces its max torque at over 700 rpm less than the previous 405 lb-ft engine. The 6.7L diesel engine also remains at the same 440 hp (323 kW) but torque increases from 860 lb-ft upwards to 925 lb-ft.

The 2020 Super Duty debuted at the 2019 Chicago Auto Show. It features a revised grille and tailgate design, new wheel options, and higher-quality interior materials for the Limited trim. A new 7.3-liter gasoline engine is available. Nicknamed "Godzilla", it makes 430 horsepower and 475 lb-ft of torque.

Cab configurations continue to be 2-Door Regular Cab, 4-Door Super Cab, and 4-Door Super Crew Cab, with Short Box (6' 9") and Long Box (8') bed lengths. The truck will be available in F-250, F-350, and F-450 pickup truck models, and F-350, F-450, and F-550 chassis cab models. All will be available in both 4X2 and 4X4 configurations. The F-350 will be the only model available in either Single Rear Wheel (SRW) or Dual Rear Wheel (DRW) configurations, the F-450 and F-550 will only be available in a Dual Rear Wheel (DRW) configuration, and the F-250 will only be available in a Single Rear Wheel configuration.

Configuration 2 for keeping the arms at a certain place, using two 1x2 thin liftarms as stoppers. I went with this version here because the buzz saws were way too close together with the first configuration.

Model: Yutong ZK6122HD9/ 1st Gen

Engine: Yuchai YC6L310-20 (L32YA)

Chasis: ZK6122CRD9

Body: Zhengzhou Yutong Bus Co. Ltd.

Susspenssion: Air Susspenssion

Seating Configuration: 2x2

Seat Type: Yutong HD Seats

Seating Capacity: 51

Transmission: 6 Speed M/T

Fare: Airconditioned

Route: Dagupan City Pangasinan - Avenida Manila.

knitted Lemarchand's box / Hellraiser cube / Lament Configuration

Farinas Trans Inc.- 2004

Bus No: 2004

Year released: 2000

Capacity: 45; 2x2 seating configuration

Route: Manila/Sampaloc-Laoag via Dau/SCTEX-Concepcion/Capas/Tarlac/Paniqui/Moncada/Carmen/Villasis/Urdaneta/Sison/Rosario/La Union/Sison/Rosario/La Union

Body: Daewoo Motors Korea

Model: 2000 Daewoo Royal Economy series

Chassis: Daewoo BH115E

Engine: Daewoo DE12

Fare: Airconditioned

Transmission System: M/T

Suspension: Leaf-Spring Suspension

Taken on: July 29, 2014

Location: McArthur Highway, Brgy. San Sebastian, Tarlac City, Tarlac

Bus No: 1547

Model: 2016 Yutong ZK6107HA Series/Surot 3rd Gen

Engine: Yuchai YC6L280-42

Chassis: ZK6107CRA

Body: Zhengzhou Yutong Bus Co. Ltd.

Seating Configuration: 2x2

Seat Design: Fabric (Blue) 2nd Gen ZK6107HA Seats

Seating Capacity: 45

Operator: Jac Liner Inc.

Transmission: M/T

Fare: Airconditioned

Route: Cubao Q.C. Metro Manila - Dagupan City Pangasinan via: E. Rodriguez Sr. Ave. Quezon City Metro Manila/A. Bonifacio Manila/NLEX/Dau Mabalacat Pampanga/SCTEX/Concepcion Exit SCTEX Tarlac, Capas, San Miguel, Tarlac City, Gerona, Paniqui, Moncada, San Manuel Tarlac/Rosales (SM Carmen), Villasis, Urdaneta City, Binalonan, Laoac, Manaoag, San Jacinto, Mangaldan Pangasinan.

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 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.

Company/Owner: Victory Liner, Inc.

Fleet/Bus Number: 131

Classification: Air-conditioned Provincial Bus

Coachbuilder: Hyundai Motor Company

Body Model: Hyundai Super Aero City

Engine Model: Hyundai D6AB (Q300)

Chassis Model: Hyundai Super Aero City (KMJTA18BPBC)

Transmission: Manual (5-speed forward, 1-speed reverse)

Suspension: Leaf Spring Suspension

Seating Configuration: 3×2

Seating Capacity: 56

Route: Monumento, Caloocan City–San Fernando City, Pampanga via NLEX-Balintawak–NLEX-Tabang / MacArthur Highway / NLEX-San Simon–NLEX-San Fernando

Municipalities/cities passing: Tabang (Guiguinto)/Malolos City/Calumpit/Apalit/San Simon

Type of Operation: Provincial Operation Public Utility Bus (Economy Class)

Area of Operation: Central Luzon (Region III)

Shot Location: MacArthur Highway (Manila North Road), Barangay Guinhawa, Malolos City, Bulacan

Date Taken: July 14, 2015

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.

** 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.

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 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.

Model of a mining excavator in front shovel configuration in scale 1:28.5. This 300 tonne machine is a representative of Liebherr's most popular size class and is ideally suited to load a fleet of 100 tonne payload mining trucks.

When LEGO introduced its 42100 Liebherr R 9800, I knew I had to get that set immediately after release. But I also knew from the beginning, that I would not like the official model's Technic design and that I had to build my own version.

Here it is, scaled larger than 42100, but on the other hand representing a much smaller machine than the 9800. About 300 vs. 800 tonnes in real life. This allowed me to use the main components of the official LEGO model to build my R 994 B. I used the clamshell bucket, the Power Functions XL actuators and the tracks and sprockets.

The main difference from 42100 lies in the electric components of my model. The following functions are all powered by two Power Functions rechargeable battery boxes and controlled by three SBricks via bluetooth connection and Brick Controller 2 app:

- Left and right crawler treads each using a Power Functions L motor

- Slewing of the upper structure using two Power Functions M motors

- Boom cylinders: one Power Functions XL motor

- Stick cylinders: one Power Functions L motor

- Bucket cylinders: one Power Functions M motor

- Clamshell bucket: one Brick Engine V1 motor (compatible to Power Functions)

- Access ladder: one Power Functions M motor

- Service flap: one Power Functions M motor

- Lighting: three pairs of Power Functions LEDs

Besides the main drive and digging functions, the model features a retractable access ladder and a lowerable service flap on the underside of the upper structure frame. The service flap is used to refuel and grease the excavator.

While building the Liebherr R 994 B Litronic in 1:28.5 scale, I could refer to a highly detailed diecast model of the very same machine in 1:50 scale.

“This artist’s concept depicts one configuration currently being studied by Textron’s Bell Aerosystems Company in conjunction with its one-man Lunar Flying Vehicle preliminary design work for the National Aeronautics and Space Administration’s Manned Spacecraft Center, Houston, Texas. Powered by twin rocket engines, it would be capable of 10-15 mile minimum flight ranges. It also could perform at least 30 sorties and be able to use the residual propellants from the descent stage of the Lunar Module. Mounted to the back of this design is a payload pallet. Motorcycle-like handle grips would be used for thrust and attitude control.”

To my knowledge, the Descent Propulsion System fuel of the Lunar Module was hypergolic. Wouldn’t that’ve been a risky proposition to use?

Note the deployed EASEP/ALSEP components.

Beautiful & iconic (in my world) ca. 1968/69 artwork by Bell Aerosystems’ immensely talented artist, John J. Carr.

See also...always informative & entertaining:

www.aerospaceprojectsreview.com/blog/?s=Bell+Aerosystems&...

Specifically:

www.aerospaceprojectsreview.com/blog/wp-content/uploads/2...

Both above credit: Aerospace Projects Review website/blog

Additional interesting designs:

www.astronautix.com/l/lunarflyers.html

Credit: Astronautix website

New to Transdev - London Sovereign(SP84), with dual-door configuration, in 10/2009, this smart OmniCity later operated for RATP Group - London Sovereign as their SP40084. It then transferred to Go North West, in preparation for Bee Network, where it received fleetnumber 3620. After transfer to Stagecoach Manchester under Tranche 2 of Bee Network, which began on 24/03/2024, it is seen here at Shudehill Interchange, Manchester, on 09/10/2024. It is awaiting departure on Bee Network Service 97 14:25 Manchester, Shudehill Interchange - Lower Broughton, Great Cheetham Street West - Prestwich Hospital, Stanhope Avenue - Unsworth Medical Centre - Bury Interchange. This Scania has since been withdrawn. This service changed operator under Tranche 2 of Bee Network. It was previously operated by Go North West out of the Manchester Queens Road depot which is now operated by Stagecoach Manchester under Bee Network.

In Tranche 1 of Bee Network, which started on 24/09/2023, Stagecoach Manchester(Greater Manchester West) lost the Wigan depot to Go North West and under Tranche 2 of Bee Network, which started on 24/03/2024, Stagecoach Manchester(Greater Manchester South) gained Manchester Queens Road depot from Go North West and the Oldham Mumps depot from First Manchester. In Tranche 3, which started on 05/01/2025, Stagecoach Manchester(Greater Manchester South) lost Ashton-under-Lyne, Manchester Hyde Road, and Manchester Sharston to Comfort DelGro Metroline Manchester who also gained Arriva Manchester's Wythenshawe depot. Stagecoach Manchester(Greater Manchester South) kept their Stockport depots. © Peter Steel 2024.

[i]A pair of Scandinavia-based JAS1A Valkyries from SVF-15 in mid air, one in clean configuration and the other one with a typical air-to-ground weapon load: a GU-11 gun pod, two jet-powered Rbs20 anti-ship missiles with IR targeting system plus two 200mm rocket launchers againts hardened targets.[/i]

Another historic classic, another "child" of the late 70ies: an anime interpretation of the famous 'Fields & Meadows' camouflage, characteristic for the Swedish Saab 37 'Viggen' jet plane family (and also used on other Swedish military vehicles, but the Viggen is/was the most prominent one).

This weirdo idea had been lurking in the back of my mind for a long time, and when a friend of mine uttered the idea of such a color variant for a Valkyrie, too, I decided to start a kind of competion - for comparison purposes, to see how an individual interpretation of this unique paradigm on a Valykrie from both of us would look like?

The kit is, as usual, a simple, vintage 1:100 scale VF-1A Valkyrie Fighter from ARII. Since the livery would be the "star" of the kit, only minor things were changed/enhanced. Usual added cockpit details include a HUD, a pilot figure, seat belts and an ejection seat trigger. Some typical Valkyrie antennae on the outside were added, too, and the rudders re-positioned off of the neutral position.

Additional external features are a IR pod under the nose, small bulges in tne air intake area which are supposed to contain guidance antennae for the air-to-ground missiles (see below), and two outriggers under the vertical fins which contain a (fictional) radar warning system and a chaff dispenser. Viggen would frequently carry such equipment in external pods, so why not be more effective and integrate them into the hull?

Now for the camouflage scheme... that one was tricky. The colors themselves are already a riddle. I guess that anyone who tries to match the original colors through photographs becomes crazy at some point, because light and weathering make them look VERY different from machine to machine, and even from picture to picture!

The Viggen's proportions hardly match a Valkyrie, but I tried my best to apply the 'Fields & Meadows' scheme on the upper surfaces. But transferring a scheme from a fixed double delta wing airplane onto a variable geometry wing fighter just leaves lots of room for interpretation... After extensive research (and experience with two 'Fields & Meadows' Viggens in 1/72 scale in the past) I finally settled for the small Valykrie on:

Light Green "322M" = Testors/Model Master 1734 (Green Zinc Chromate)

Dark Green "326M" = Humbrol 117 (Leaf Green, FS34102)

Black "093M" = Mix of Humbrol's 33 & 91 (Flat Black & Black Green) in 1:1 ratio

Earth "507M" = Testors/Model Master 2008 (Raw Sienna)

Grey undersides "058M" = Testors/Model Master 2086 (RLM76, Lichtblau)

The Zinc Chromate sounds crude and IS very bright, but on the 1/100 scale Valkyrie this extreme green is O.K., esp. with the later black ink wash which tones down everything a bit. At 1/72 scale I would have rather used Humbrol's 80 (Grass Green), which is a bit "milder" and comes IMHO very close to the real life color.

Humbrol 117 for the dark green tone is a compromise, and IMHO still a bit too dark. During pre-tests I found more authentic but even darker greens like Humbrol's 116 (FS 34079), 75 (Bronze Green) or 30 (Dark Green) to be too murky for the small kit. 117 is already considerably "brighter", and this contrast was simply necessary for a good overall impression of the camouflage scheme - the dark green was supposed to stand out against both the light green and the black fields. I should have used RAL6003, but the way it turned out is still acceptable.

Instead of pure black which 'Fields & Meadows' is supposed to contain, I went for a very dark green, which also yields a slightly bleached look. Some pictures of real Viggen also suggest that the "Black" is actually a greenish tone.

Testors' Raw Sienna from their figure color series is a very good match for the Viggen's light earth color patches. Another, more common but also very plausible alternative is Humbrol's 118 (US Tan, FS30219). Again, pictures of real Viggen suggest a wide variety of light brown shades due to fading and light influences! The Sienna is more yellowish, though, so I went for that tone.

Finally, RLM76 for the undersides was a surprise find! Originally, FS36375 (Humbrol 127) was my choice. But when I checked other paints in store I found Testors' RLM76 to be a tad lighter and with a stronger bluish hue - exactly the look I had been searching for for this kit, without need for mixing.

The radar nose became semi-gloss black and the wings' leading edges were painted in flatr aluminium Markings were consciously left simple, trying to emulate the stern original Viggen look as much as possible, with no flashy distractions. Consequently, there are just standard Macross roundels instead of Swedish insignia (which look, in red/white instead of blue/yellow, a bit disturbing?), a yellow squadron number at the cockpit (for SVF-15) and the red individual airplane number on the vertical fins' outsides. Only a falcon squadron empblem in red and yellow found its way onto the fins (it comes from an Israeli IAI Kfir from a Hasegawa kit), because the colors matched well with the overall look of the kit.

After basic painting, the kit received a light wash with black ink and some fine liner treatment. Then, decals and finally a coat of matte varnish was appllied. The end result looks cool, though, whatever one might quibble about authenticity!

Some extra effort went into the ordnance under this VF-1A's wings, though: the outer pylons hold a 4-missile launcher each (leftover from a fictional but neat ESCI Kamow Ka-34 'Hokum' kit), the inner pylons carry larger cruise missiles which were inspired by the characteristic Rb04E and more modern Rbs-15 anti-ship/surface missiles the AJ37 used to carry in its heydays.

These are actually modified Norwegian AGM-119C 'Penguin' missiles in 1/72 which I found in a Hasegawa F-16 weapon kit and never has a use for. I shortened the fuselage, changed the main fins into wing end plate types and added details like an underbelly air intake for a jet engine (like the more modern RBS-15 missile now carried by the Gripen) and an exhaust nozzle. Finally, these missiles were painted to look like a Rb04E in white, black and aluminium - they help a lot in order to create a "vintage AJ37 feel" to this Valkyrie.

Even when the finish is not perfect, it is amazing to see how well even such an exotic livery works on a Macross Valkyrie - it suits her well, as an hommage to one of the most famous (and attractive?) camouflage schemes ever applied to military verhicles.

This picture is taken with stacked extenders.

The configuration of the camera and lens is as follows:

EF70-200mm f/2.8L IS II USM @ 200mm

Canon Extender EF 2x III

Kenko Teleplus HD 2x DGX

Kenko 20mm extension tube

Canon Extender EF 1.4x III

60D

The 20mm extension tube is added so that I can mount the Canon 1.4x extender. Although adding extension tubes should lose the ability to focus at infinity, it would seem that I am still able to focus on the moon.

What is the focal length for this photo?

It would seem that the focal length recorded by the EXIF accounts for the two 2x extenders (200mm x2 x2), but not the 1.4x extender. Similar case for the aperture. I also do not know what is the effect of extension tube on focal length.

Given that this photo is uncropped, is it possible to determine the focal length of the setup based on this photo?

Focusing difficulties

Viewfinder AF does not work. Live View AF sometimes work. Manual focus is difficult because a slight touch on the camera or lens will cause a lot of shake, especially with 10x magnification Live View, making it difficult to judge focus.

Not to mention that the moon will move across the frame in around 30s, so that I have to re-frame again.

Also, Live View will auto switch off, if I don't keep my finger on the shutter button, half pressed.

Processed in Canon Digital Photo Professional 4

When you finally crack the configuration of Lemarchand's diabolical puzzle box.

Embraer 135/145 - MSN 681

Status : Active

Registration : N18120

Airline Trans States Airlines

Country : USA

Date : 1982 -

Codes AX LOF

Callsign : Waterski

Web site : www.transstates.net

Serial number681

Type145XR

First flight dateUnknown

Test registrationPT-SFN

Plane age15.7 years

Seat configuration

Engines2 x AN AE3007A1E

15/01/2003ExpressjetN18120

25/08/2015Trans States AirlinesN18120

My new North American diesel engine in the Canadian Nation Railway scheme is the first Lego loco I have built since my childhood days and was strongly inspired by the EMD-GP 7, 9 and 20 diesel engines and other similar types that came in full high hood configuration, but I went on to building the model rather freely, leaving out things I didn’t want and not sticking to any particular real model.

Being 9+ studs wide, it’s quite a beast and fits very well to the “large city minifigure scale” preferred by ER0L and me. It drives on two 9V train motors from the 90s. The lighting is realized with materials from that time as well, energized by a separate battery box in the shorter section of the hood and thus illuminating the two fronts and cabin of the engine independently from the transformer. That way, the light can be on even when the model stands still.

I went for moving pilots, even though they don’t exist on such models in reality. This was mostly due to the prolonged bionicle trucks I wanted to use here, which would otherwise have made the stairs stand out too far from the trucks in curves and switches.

I have nearly finished building the first of several tank cars for it, so consider these pics an “opener” for more train equipment to come from me.

+++ DISCLAIMER +++

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

Some background:

The Cessna Model 336 and 337 “Skymaster” were American twin-engine civil utility aircraft built in a unique push-pull configuration. Their engines were mounted in the nose and rear of its pod-style fuselage. Twin booms extended aft of the wings to the vertical stabilizers, with the rear engine between them. The horizontal stabilizer was aft of the pusher propeller, mounted between and connecting the two booms.

The type’s versatility, low noise level, high travel speed and good loitering time in the operational area at low speed proved to be vital assets for these public service operators and justified its relatively high maintenance costs. A handful of the modernized Spectrum SA-550 machines were still in active service after the Millennium, primarily in the USA.

General characteristics:

Crew: 1 + 3 passengers (up to 5 passengers possible in special seat configuration)

Length: 32 ft 6½ in (9.94 m)

Wingspan: 38 ft ¾ in (11.62 m)

Height: 9 ft 2 in (2.79 m)

Wing area: 201 sq ft (18.81 m²)

Aspect ratio: 7.18:1

Airfoil: NACA 2412 at root, NACA 2409 at tip

Empty weight: 2,655 lb (1,204 kg)

Max takeoff weight: 4,400 lb (1,996 kg)

Fuel capacity: 92 US gal (77 imp gal; 350 l) normal,

128 US gal (107 imp gal; 480 l) with auxiliary tank

in the cabin instead of two passenger seats

Powerplant:

1× Pratt & Whitney PT6A-27 turboprop engine, delivering 550 shp (410 kW) and

driving a four-blade McCauley fully-feathering, constant-speed propeller, 6 ft 4 in (1.93 m) diameter

Performance:

Maximum speed: 199 mph (320 km/h, 173 kn) at sea level

Cruise speed: 144 mph (232 km/h, 125 kn) at 10,000 ft (3,000 m) (econ cruise)

Stall speed: 69 mph (111 km/h, 60 kn)

Range: 1421 mi (2.288 km, 1.243 nmi) at 10.000 ft (3.050 m) altitude and economy cruise

Service ceiling: 19,500 ft (5,900 m)

Rate of climb: 1,200 ft/min (6.1 m/s)

Takeoff distance to 50 ft (15m): 1,545 ft (471 m)

Landing distance from 50 ft (15m): 1,650 ft (500 m)

The kit and its assembly:

This build is the combination of ingredients that had already been stashed away for a long time, and the “Red Lights” Group Build at whatifmodellers.com in early 2021 was a good motivator and occasion to finally put everything together.

The basis is an ARII 1:72 Cessna T337 model kit – I had purchased it long ago with the expectation to create a military Skymaster from it, but I was confused by a fixed landing gear which would make it a 336? Well, without a further concrete plan the kit preliminarily landed in The Stash™…

However, the ARII model features the optional observation windows in the doors on the starboard side, in the form of a complete(!) fuselage half, so that it lends itself to a police or firefighter aircraft of some sort. This idea was furthermore fueled by a decal sheet that I had been given from a friend, left over from a 1:72 Italeri JetRanger, with three optional police helicopter markings.

The final creative element was the real-world “Pelican” conversion of six O-2As for the US Navy, as mentioned in the background above: the front engine was replaced with a longer nose and the engine configuration changed to a pusher-only aircraft with a single powerful turboprop engine. This looked so odd that I wanted to modify the ARII Cessna in a similar fashion, too, and all these factors came together in this model.

My Arii Cessna 337 kit is a re-boxing from 2009, but its origins date back to Eidai in 1972 and that’s just what you get: a vintage thing with some flash and sinkholes, raised (but fine) surface details and pretty crude seams with bulges and gaps. Some PSR is direly necessary, esp. the fit of the fuselage halves is cringeworthy. The clear parts were no source of joy, either; especially the windscreen turned out to be thick, very streaky (to a degree that I’d almost call it opaque!) and even not fully molded! The side glazing was also not very clear. I tried to improve the situation through polishing, but if the basis is already poor, there’s little you can do about it. Hrmpf.

However, the kit was built mostly OOB, including the extra O-2 glazing in the lower doors, but with some mods. One is a (barely visible) extra tank in the cabin’s rear, plus a pilot and an observer figure placed into the tight front seats. The extended “Pelican” nose was a lucky find – I was afraid that I had had to sculpt a nose from scratch with 2C putty. But I found a radome from a Hasegawa RA-5C, left over from a model I built in the Eighties and that has since long fallen apart. However, this nose fitted almost perfectly in size and shape, I just “blunted” the tip a little. Additionally, both the hull in front of the dashboard and the Vigilante radome were filled with as many lead beads as possible to keep the nose down.

The kit’s OOB spatted, fixed landing gear was retained – even though it is dubious for a Cessna 337, because this type had a fully retractable landing gear, and the model has the landing gear covers actually molded into the lower fuselage. On the other side, the Cessna 336’s fixed landing gear looks quite different, too! However, this is a what-if model, and a fixed landing gear might have been a measure to reduce maintenance costs?

The propeller was replaced with a resin four-blade aftermarket piece (from CMK, probably the best-fitting thing on this build!) on my standard metal axis/styrene tube adapter arrangement. The propeller belongs to a Shorts Tucano, but I think that it works well on the converted Cessna and its powerful pusher engine, even though in the real world, the SA-550 is AFAIK driven by a three-blade prop. For the different engine I also enlarged the dorsal air intake with a 1.5 mm piece of styrene sheet added on top of the molded original air scoop and added a pair of ventral exhaust stubs (scratched from sprue material).

Another addition is a pair of winglets, made from 0.5 mm styrene sheet – an upgrade which I found on several late Cessna 337s in various versions. They just add to the modernized look of the aircraft. For the intended observation role, a hemispherical fairing under the nose hides a 180° camera, and I added some antennae around the hull.

However, a final word concerning the model kit itself: nothing fits, be warned! While the kit is a simple affair and looks quite good in the box, assembling it turned out to be a nightmare, with flash, sinkholes, a brittle styrene and gaps everywhere. This includes the clear parts, which are pretty thick and blurry. The worst thing is the windscreen, which is not only EXTRA thick and EXTRA blurry, it was also not completely molded, with gaps on both sides. I tried to get it clearer through manual polishing, but the streaky blurs are integral – no hope for improvement unless you completely replace the parts! If I ever build a Cessna 337/O-2 again, I will give the Airfix kit a try, it can only be better…

Painting and markings:

The choice between the operator options from the JetRanger sheet was hard, it included Sweden and Italy, but I eventually settled for the LAPD because the livery looks cool and this police department not only operates helicopters, but also some fixed-wing aircraft.

I adapted the LAPD’s classic black-and-white police helicopter livery (Gloss White and Black, Humbrol 22 and 21, respectively) to the Cessna and extended it to the wings. At this point – already upset because of the poor fit of the hardware – disaster struck in the form of Humbrol’s 22 turning into a pinkish ivory upon curing! In the tin, the paint and its pigments looked pretty white and “clean”, and I assume that it’s the thinner that caused this change. What a crap! It’s probably the third tin with 22 that causes trouble, even though in different peculiarities!

The result was total rubbish, though, and I tried to rub the paint off as good as possible on the small model with its many windows, the fixed, delicate landing gear and the wing support struts. Then I overpainted the areas with Revell 301 (Semi-matt White). While this enamel yielded the intended pure white tone, the paint itself is rather gooey and not easy to work with, so that the overall finish turned out worse than desired. At least the black paint worked properly. The demarcations were created with black decal stripes (TL Modellbau), because the tiny model left little room for complex masking measures – and I did not risk any more painting accidents.

Since the aircraft would be kept shiny and clean, I just did a light black ink washing to emphasize surface details and did a light panel post-shading on the black areas, not for weathering but rather to accent surface structures. No further weathering was done (and necessary).

The markings/decals come – as mentioned above – from an Italeri 1:72 JetRanger, but they were augmented with some additional markings, e. g. grey walkways on the wings and “L-A-P-D” in large black letters under the wings, to distract from the poor finish of the white paint around them…

Finally, the kit was sealed overall with Italeri semi-gloss acrylic varnish, just with a matt anti-glare shield in front of the windscreen, which received thin white trim lines (generic decal stripes).

A challenging build due to the Arii kit’s rather poor basis, the massive rhinoplasty and the crisp paint scheme. However, I like the result – what-if models do not always have to be armed military vehicles, there’s potential in other genres, too. And this mono-engine “Pelican” Skymaster plays its role as a “flying eye” in police service credibly and well. However, this was my first and last Eidai kit…

+++ DISCLAIMER +++

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

Some background:

The Cessna Model 336 and 337 “Skymaster” were American twin-engine civil utility aircraft built in a unique push-pull configuration. Their engines were mounted in the nose and rear of its pod-style fuselage. Twin booms extended aft of the wings to the vertical stabilizers, with the rear engine between them. The horizontal stabilizer was aft of the pusher propeller, mounted between and connecting the two booms.

The type’s versatility, low noise level, high travel speed and good loitering time in the operational area at low speed proved to be vital assets for these public service operators and justified its relatively high maintenance costs. A handful of the modernized Spectrum SA-550 machines were still in active service after the Millennium, primarily in the USA.

General characteristics:

Crew: 1 + 3 passengers (up to 5 passengers possible in special seat configuration)

Length: 32 ft 6½ in (9.94 m)

Wingspan: 38 ft ¾ in (11.62 m)

Height: 9 ft 2 in (2.79 m)

Wing area: 201 sq ft (18.81 m²)

Aspect ratio: 7.18:1

Airfoil: NACA 2412 at root, NACA 2409 at tip

Empty weight: 2,655 lb (1,204 kg)

Max takeoff weight: 4,400 lb (1,996 kg)

Fuel capacity: 92 US gal (77 imp gal; 350 l) normal,

128 US gal (107 imp gal; 480 l) with auxiliary tank

in the cabin instead of two passenger seats

Powerplant:

1× Pratt & Whitney PT6A-27 turboprop engine, delivering 550 shp (410 kW) and

driving a four-blade McCauley fully-feathering, constant-speed propeller, 6 ft 4 in (1.93 m) diameter

Performance:

Maximum speed: 199 mph (320 km/h, 173 kn) at sea level

Cruise speed: 144 mph (232 km/h, 125 kn) at 10,000 ft (3,000 m) (econ cruise)

Stall speed: 69 mph (111 km/h, 60 kn)

Range: 1421 mi (2.288 km, 1.243 nmi) at 10.000 ft (3.050 m) altitude and economy cruise

Service ceiling: 19,500 ft (5,900 m)

Rate of climb: 1,200 ft/min (6.1 m/s)

Takeoff distance to 50 ft (15m): 1,545 ft (471 m)

Landing distance from 50 ft (15m): 1,650 ft (500 m)

The kit and its assembly:

This build is the combination of ingredients that had already been stashed away for a long time, and the “Red Lights” Group Build at whatifmodellers.com in early 2021 was a good motivator and occasion to finally put everything together.

The basis is an ARII 1:72 Cessna T337 model kit – I had purchased it long ago with the expectation to create a military Skymaster from it, but I was confused by a fixed landing gear which would make it a 336? Well, without a further concrete plan the kit preliminarily landed in The Stash™…

However, the ARII model features the optional observation windows in the doors on the starboard side, in the form of a complete(!) fuselage half, so that it lends itself to a police or firefighter aircraft of some sort. This idea was furthermore fueled by a decal sheet that I had been given from a friend, left over from a 1:72 Italeri JetRanger, with three optional police helicopter markings.

The final creative element was the real-world “Pelican” conversion of six O-2As for the US Navy, as mentioned in the background above: the front engine was replaced with a longer nose and the engine configuration changed to a pusher-only aircraft with a single powerful turboprop engine. This looked so odd that I wanted to modify the ARII Cessna in a similar fashion, too, and all these factors came together in this model.

My Arii Cessna 337 kit is a re-boxing from 2009, but its origins date back to Eidai in 1972 and that’s just what you get: a vintage thing with some flash and sinkholes, raised (but fine) surface details and pretty crude seams with bulges and gaps. Some PSR is direly necessary, esp. the fit of the fuselage halves is cringeworthy. The clear parts were no source of joy, either; especially the windscreen turned out to be thick, very streaky (to a degree that I’d almost call it opaque!) and even not fully molded! The side glazing was also not very clear. I tried to improve the situation through polishing, but if the basis is already poor, there’s little you can do about it. Hrmpf.

However, the kit was built mostly OOB, including the extra O-2 glazing in the lower doors, but with some mods. One is a (barely visible) extra tank in the cabin’s rear, plus a pilot and an observer figure placed into the tight front seats. The extended “Pelican” nose was a lucky find – I was afraid that I had had to sculpt a nose from scratch with 2C putty. But I found a radome from a Hasegawa RA-5C, left over from a model I built in the Eighties and that has since long fallen apart. However, this nose fitted almost perfectly in size and shape, I just “blunted” the tip a little. Additionally, both the hull in front of the dashboard and the Vigilante radome were filled with as many lead beads as possible to keep the nose down.

The kit’s OOB spatted, fixed landing gear was retained – even though it is dubious for a Cessna 337, because this type had a fully retractable landing gear, and the model has the landing gear covers actually molded into the lower fuselage. On the other side, the Cessna 336’s fixed landing gear looks quite different, too! However, this is a what-if model, and a fixed landing gear might have been a measure to reduce maintenance costs?

The propeller was replaced with a resin four-blade aftermarket piece (from CMK, probably the best-fitting thing on this build!) on my standard metal axis/styrene tube adapter arrangement. The propeller belongs to a Shorts Tucano, but I think that it works well on the converted Cessna and its powerful pusher engine, even though in the real world, the SA-550 is AFAIK driven by a three-blade prop. For the different engine I also enlarged the dorsal air intake with a 1.5 mm piece of styrene sheet added on top of the molded original air scoop and added a pair of ventral exhaust stubs (scratched from sprue material).

Another addition is a pair of winglets, made from 0.5 mm styrene sheet – an upgrade which I found on several late Cessna 337s in various versions. They just add to the modernized look of the aircraft. For the intended observation role, a hemispherical fairing under the nose hides a 180° camera, and I added some antennae around the hull.

However, a final word concerning the model kit itself: nothing fits, be warned! While the kit is a simple affair and looks quite good in the box, assembling it turned out to be a nightmare, with flash, sinkholes, a brittle styrene and gaps everywhere. This includes the clear parts, which are pretty thick and blurry. The worst thing is the windscreen, which is not only EXTRA thick and EXTRA blurry, it was also not completely molded, with gaps on both sides. I tried to get it clearer through manual polishing, but the streaky blurs are integral – no hope for improvement unless you completely replace the parts! If I ever build a Cessna 337/O-2 again, I will give the Airfix kit a try, it can only be better…

Painting and markings:

The choice between the operator options from the JetRanger sheet was hard, it included Sweden and Italy, but I eventually settled for the LAPD because the livery looks cool and this police department not only operates helicopters, but also some fixed-wing aircraft.

I adapted the LAPD’s classic black-and-white police helicopter livery (Gloss White and Black, Humbrol 22 and 21, respectively) to the Cessna and extended it to the wings. At this point – already upset because of the poor fit of the hardware – disaster struck in the form of Humbrol’s 22 turning into a pinkish ivory upon curing! In the tin, the paint and its pigments looked pretty white and “clean”, and I assume that it’s the thinner that caused this change. What a crap! It’s probably the third tin with 22 that causes trouble, even though in different peculiarities!

The result was total rubbish, though, and I tried to rub the paint off as good as possible on the small model with its many windows, the fixed, delicate landing gear and the wing support struts. Then I overpainted the areas with Revell 301 (Semi-matt White). While this enamel yielded the intended pure white tone, the paint itself is rather gooey and not easy to work with, so that the overall finish turned out worse than desired. At least the black paint worked properly. The demarcations were created with black decal stripes (TL Modellbau), because the tiny model left little room for complex masking measures – and I did not risk any more painting accidents.

Since the aircraft would be kept shiny and clean, I just did a light black ink washing to emphasize surface details and did a light panel post-shading on the black areas, not for weathering but rather to accent surface structures. No further weathering was done (and necessary).

The markings/decals come – as mentioned above – from an Italeri 1:72 JetRanger, but they were augmented with some additional markings, e. g. grey walkways on the wings and “L-A-P-D” in large black letters under the wings, to distract from the poor finish of the white paint around them…

Finally, the kit was sealed overall with Italeri semi-gloss acrylic varnish, just with a matt anti-glare shield in front of the windscreen, which received thin white trim lines (generic decal stripes).

A challenging build due to the Arii kit’s rather poor basis, the massive rhinoplasty and the crisp paint scheme. However, I like the result – what-if models do not always have to be armed military vehicles, there’s potential in other genres, too. And this mono-engine “Pelican” Skymaster plays its role as a “flying eye” in police service credibly and well. However, this was my first and last Eidai kit…

Setting configuration: Low Light

Configuration of the Mir space station in 1990, without the Spektr and Priroda modules.

+++ DISCLAIMER +++

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

Some background:

The Cessna Model 336 and 337 “Skymaster” were American twin-engine civil utility aircraft built in a unique push-pull configuration. Their engines were mounted in the nose and rear of its pod-style fuselage. Twin booms extended aft of the wings to the vertical stabilizers, with the rear engine between them. The horizontal stabilizer was aft of the pusher propeller, mounted between and connecting the two booms.

The type’s versatility, low noise level, high travel speed and good loitering time in the operational area at low speed proved to be vital assets for these public service operators and justified its relatively high maintenance costs. A handful of the modernized Spectrum SA-550 machines were still in active service after the Millennium, primarily in the USA.

General characteristics:

Crew: 1 + 3 passengers (up to 5 passengers possible in special seat configuration)

Length: 32 ft 6½ in (9.94 m)

Wingspan: 38 ft ¾ in (11.62 m)

Height: 9 ft 2 in (2.79 m)

Wing area: 201 sq ft (18.81 m²)

Aspect ratio: 7.18:1

Airfoil: NACA 2412 at root, NACA 2409 at tip

Empty weight: 2,655 lb (1,204 kg)

Max takeoff weight: 4,400 lb (1,996 kg)

Fuel capacity: 92 US gal (77 imp gal; 350 l) normal,

128 US gal (107 imp gal; 480 l) with auxiliary tank

in the cabin instead of two passenger seats

Powerplant:

1× Pratt & Whitney PT6A-27 turboprop engine, delivering 550 shp (410 kW) and

driving a four-blade McCauley fully-feathering, constant-speed propeller, 6 ft 4 in (1.93 m) diameter

Performance:

Maximum speed: 199 mph (320 km/h, 173 kn) at sea level

Cruise speed: 144 mph (232 km/h, 125 kn) at 10,000 ft (3,000 m) (econ cruise)

Stall speed: 69 mph (111 km/h, 60 kn)

Range: 1421 mi (2.288 km, 1.243 nmi) at 10.000 ft (3.050 m) altitude and economy cruise

Service ceiling: 19,500 ft (5,900 m)

Rate of climb: 1,200 ft/min (6.1 m/s)

Takeoff distance to 50 ft (15m): 1,545 ft (471 m)

Landing distance from 50 ft (15m): 1,650 ft (500 m)

The kit and its assembly:

This build is the combination of ingredients that had already been stashed away for a long time, and the “Red Lights” Group Build at whatifmodellers.com in early 2021 was a good motivator and occasion to finally put everything together.

The basis is an ARII 1:72 Cessna T337 model kit – I had purchased it long ago with the expectation to create a military Skymaster from it, but I was confused by a fixed landing gear which would make it a 336? Well, without a further concrete plan the kit preliminarily landed in The Stash™…

However, the ARII model features the optional observation windows in the doors on the starboard side, in the form of a complete(!) fuselage half, so that it lends itself to a police or firefighter aircraft of some sort. This idea was furthermore fueled by a decal sheet that I had been given from a friend, left over from a 1:72 Italeri JetRanger, with three optional police helicopter markings.

The final creative element was the real-world “Pelican” conversion of six O-2As for the US Navy, as mentioned in the background above: the front engine was replaced with a longer nose and the engine configuration changed to a pusher-only aircraft with a single powerful turboprop engine. This looked so odd that I wanted to modify the ARII Cessna in a similar fashion, too, and all these factors came together in this model.

My Arii Cessna 337 kit is a re-boxing from 2009, but its origins date back to Eidai in 1972 and that’s just what you get: a vintage thing with some flash and sinkholes, raised (but fine) surface details and pretty crude seams with bulges and gaps. Some PSR is direly necessary, esp. the fit of the fuselage halves is cringeworthy. The clear parts were no source of joy, either; especially the windscreen turned out to be thick, very streaky (to a degree that I’d almost call it opaque!) and even not fully molded! The side glazing was also not very clear. I tried to improve the situation through polishing, but if the basis is already poor, there’s little you can do about it. Hrmpf.

However, the kit was built mostly OOB, including the extra O-2 glazing in the lower doors, but with some mods. One is a (barely visible) extra tank in the cabin’s rear, plus a pilot and an observer figure placed into the tight front seats. The extended “Pelican” nose was a lucky find – I was afraid that I had had to sculpt a nose from scratch with 2C putty. But I found a radome from a Hasegawa RA-5C, left over from a model I built in the Eighties and that has since long fallen apart. However, this nose fitted almost perfectly in size and shape, I just “blunted” the tip a little. Additionally, both the hull in front of the dashboard and the Vigilante radome were filled with as many lead beads as possible to keep the nose down.

The kit’s OOB spatted, fixed landing gear was retained – even though it is dubious for a Cessna 337, because this type had a fully retractable landing gear, and the model has the landing gear covers actually molded into the lower fuselage. On the other side, the Cessna 336’s fixed landing gear looks quite different, too! However, this is a what-if model, and a fixed landing gear might have been a measure to reduce maintenance costs?

The propeller was replaced with a resin four-blade aftermarket piece (from CMK, probably the best-fitting thing on this build!) on my standard metal axis/styrene tube adapter arrangement. The propeller belongs to a Shorts Tucano, but I think that it works well on the converted Cessna and its powerful pusher engine, even though in the real world, the SA-550 is AFAIK driven by a three-blade prop. For the different engine I also enlarged the dorsal air intake with a 1.5 mm piece of styrene sheet added on top of the molded original air scoop and added a pair of ventral exhaust stubs (scratched from sprue material).

Another addition is a pair of winglets, made from 0.5 mm styrene sheet – an upgrade which I found on several late Cessna 337s in various versions. They just add to the modernized look of the aircraft. For the intended observation role, a hemispherical fairing under the nose hides a 180° camera, and I added some antennae around the hull.

However, a final word concerning the model kit itself: nothing fits, be warned! While the kit is a simple affair and looks quite good in the box, assembling it turned out to be a nightmare, with flash, sinkholes, a brittle styrene and gaps everywhere. This includes the clear parts, which are pretty thick and blurry. The worst thing is the windscreen, which is not only EXTRA thick and EXTRA blurry, it was also not completely molded, with gaps on both sides. I tried to get it clearer through manual polishing, but the streaky blurs are integral – no hope for improvement unless you completely replace the parts! If I ever build a Cessna 337/O-2 again, I will give the Airfix kit a try, it can only be better…

Painting and markings:

The choice between the operator options from the JetRanger sheet was hard, it included Sweden and Italy, but I eventually settled for the LAPD because the livery looks cool and this police department not only operates helicopters, but also some fixed-wing aircraft.

I adapted the LAPD’s classic black-and-white police helicopter livery (Gloss White and Black, Humbrol 22 and 21, respectively) to the Cessna and extended it to the wings. At this point – already upset because of the poor fit of the hardware – disaster struck in the form of Humbrol’s 22 turning into a pinkish ivory upon curing! In the tin, the paint and its pigments looked pretty white and “clean”, and I assume that it’s the thinner that caused this change. What a crap! It’s probably the third tin with 22 that causes trouble, even though in different peculiarities!

The result was total rubbish, though, and I tried to rub the paint off as good as possible on the small model with its many windows, the fixed, delicate landing gear and the wing support struts. Then I overpainted the areas with Revell 301 (Semi-matt White). While this enamel yielded the intended pure white tone, the paint itself is rather gooey and not easy to work with, so that the overall finish turned out worse than desired. At least the black paint worked properly. The demarcations were created with black decal stripes (TL Modellbau), because the tiny model left little room for complex masking measures – and I did not risk any more painting accidents.

Since the aircraft would be kept shiny and clean, I just did a light black ink washing to emphasize surface details and did a light panel post-shading on the black areas, not for weathering but rather to accent surface structures. No further weathering was done (and necessary).

The markings/decals come – as mentioned above – from an Italeri 1:72 JetRanger, but they were augmented with some additional markings, e. g. grey walkways on the wings and “L-A-P-D” in large black letters under the wings, to distract from the poor finish of the white paint around them…

Finally, the kit was sealed overall with Italeri semi-gloss acrylic varnish, just with a matt anti-glare shield in front of the windscreen, which received thin white trim lines (generic decal stripes).

A challenging build due to the Arii kit’s rather poor basis, the massive rhinoplasty and the crisp paint scheme. However, I like the result – what-if models do not always have to be armed military vehicles, there’s potential in other genres, too. And this mono-engine “Pelican” Skymaster plays its role as a “flying eye” in police service credibly and well. However, this was my first and last Eidai kit…

Bus no.: 8076

Classification: Airconditioned Provincial Operation Bus

Seating Configuration: 2x2

Seating Capacity: 45 Passengers

Model: Kinglong XMQ6110Y

Manufacturer: Xiamen KingLong United (KingLong Bus)

Chassis:

Engine: Cummins C300-20

Suspension: Leaf Spring Suspension

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

Shot Location: NLEX Access Road Dau-Mabalacat, Pampanga