View allAll Photos Tagged Testbed
Airbus A350-941 [A350 XWB™]
MSN 0002
F-WWCF '002' [Second prototype]
A380-861
MSN 004 [Engine Alliance testbed]
F-WWDD 'VNO' ['#A380' 'iflyA380.com' decals]
Airbus S.A.S.
Copyright © 2016 A380spotter. All rights reserved.
Description: The X-15 #2 (56-6671) launches away from the B-52 mothership with its rocket engine ignited. The white patches near the middle of the ship are frost from the liquid oxygen used in the propulsion system, although very cold liquid nitrogen was also used to cool the payload bay, cockpit, windshields, and nose.
The X-15 was a rocket-powered aircraft 50 ft long with a wingspan of 22 ft. It was a missile-shaped vehicle with an unusual wedge-shaped vertical tail, thin stubby wings, and unique fairings that extended along the side of the fuselage. The X-15 weighed about 14,000 lb empty and approximately 34,000 lb at launch. The XLR-99 rocket engine, manufactured by Thiokol Chemical Corp., was pilot controlled and was capable of developing 57,000 lb of rated thrust (actual thrust reportedly climbed to 60,000 lb). North American Aviation built three X-15 aircraft for the program.
The X-15 research aircraft was developed to provide in-flight information and data on aerodynamics, structures, flight controls, and the physiological aspects of high-speed, high-altitude flight. A follow-on program used the aircraft as a testbed to carry various scientific experiments beyond the Earth's atmosphere on a repeated basis.
For flight in the dense air of the usable atmosphere, the X-15 used conventional aerodynamic controls such as rudder surfaces on the vertical stabilizers to control yaw and canted horizontal surfaces on the tail to control pitch when moving in synchronization or roll when moved differentially.
For flight in the thin air outside of the appreciable Earth's atmosphere, the X-15 used a reaction control system. Hydrogen peroxide thrust rockets located on the nose of the aircraft provided pitch and yaw control. Those on the wings provided roll control.
Because of the large fuel consumption, the X-15 was air launched from a B-52 aircraft at 45,000 ft and a speed of about 500 mph. Depending on the mission, the rocket engine provided thrust for the first 80 to 120 sec of flight. The remainder of the normal 10 to 11 min. flight was powerless and ended with a 200-mph glide landing.
Generally, one of two types of X-15 flight profiles was used: a high-altitude flight plan that called for the pilot to maintain a steep rate of climb, or a speed profile that called for the pilot to push over and maintain a level altitude.
The X-15 was flown over a period of nearly 10 years—June 1959 to Oct. 1968—and set the world's unofficial speed and altitude records of 4,520 mph (Mach 6.7) and 354,200 ft (over 67 mi) in a program to investigate all aspects of piloted hypersonic flight. Information gained from the highly successful X-15 program contributed to the development of the Mercury, Gemini, and Apollo manned spaceflight programs, and also the Space Shuttle program.
The X-15s made a total of 199 flights and were manufactured by North American Aviation. X-15-1, serial number 56-6670, is now located at the National Air and Space Museum, Washington DC. North American X-15A-2, serial number 56-6671, is at the United States Air Force Museum, Wright-Patterson AFB, Ohio. The X-15-3, serial number 56-6672, crashed on November 15, 1967, resulting in the death of Maj. Michael J. Adams.
Credit: NASA
Image Number: EC88-0180 -1
Date: Circa 1962
N50CR North American Rockwell NA-265 Sabre 50 Rockwell Collins Evergreen Aviation & Space Museum McMinnville 12 November 2017. Avionics Testbed.
Several Generation Three testbed aircraft were developed to test newer engines and radar, but none made it into production. However, in 1971, the MiG-21SMT (“Fishbed-J”) was developed with increased fuel capacity. This variant is easily spotted due to its larger dorsal saddle tank. These variants were very unpopular with pilots and subsequently rebuilt with smaller tanks. These conversions were known as the MiG-21ST (Model 50, NATO “Fishbed-J”).
In this image, you can see the larger dorsal saddle tank of this MiG-21SMT (Fishbed-J) from the 18th Guards Fighter Aviation Regiment, stationed in Merseberg, East Germany. The outer pylons are holding the Kh-66 Grom (NATO: AS-7 ‘Kerry’) ASM missile. Also visible are the R-3S AAM missiles and the built-in GSh-23L cannon mounted above the centre-line drop tank.
On July 19, 2013, a C-17 aircraft from Buckley Air Force Base outside of Denver, Colo. delivered Lockheed Martin’s full-sized, functional GPS III satellite prototype to Cape Canaveral Air Force Station (CCAFS), Fla. The GPS III Non-Flight Satellite Testbed (GNST) came to CCAFS to help test facilities and pre-launch processes, further reducing risk and gaining efficiencies, prior the first GPS III flight satellite’s expected delivery to the U.S. Air Force in 2014 and launch in 2015.
First time visit to Russia to present "Highspeed WiFi" copabilities.
Pictured here on very short finals to Vnukovo RWY19
For many years the District Railway, officially entitled the Metropolitan District Railway and that was promoted to complete what is now the Circle line of the London Underground thus 'matching' the northern section constructed and operated by the Metropolitan Railway, oversaw the issue of various maps of the Metropolis that were offered for public sale. These, needless to say, heavily promoted the company's lines and services as well as other railways and omnibus lines operated 'in connection' with their services - often in quite wilful ignorance of alternatives!
This, from 1903, shows some still familiar District line services along with sections of lines that have seen services withdrawn, transferred or indeed closed such as the services beyond Addison Road (Olympia) towards Latimer Road via Uxbridge Rd station. This issue also shows the original layout of lines around Hounslow, subsequently altered as well as now being part of the Piccadilly line as well as the Uxbridge section, beyond South Harrow, that was under construction and that the MDR would eventually run under powers obtained to have right of use of the Metropolitan's Uxbridge extension that would open in 1904.In fact the section of line running off from Mill Hill Park (now Acton Town) through the largely open fields of Middlesex was to be the testbed in these years for the four-rail electrification system adopted for the wider London Underground system following the purchase of the MDR by American interests to assist in the development of deep tube lines and the infusion of US finance and know-how. The reverse of the map shows various announcements and tables of services and fares. This includes the famous and long-standing through trains from stations on the District direct to Southend on Sea via the London, Tilbury & Southern Railway.
This map would have been priced a half-penny had it been sold but it appears, as was quite common, slightly cropped and folded tipped into a 1903 Black's Guide Book to "Around London".
The Central London Railway was formed in 1891 to build a tube railway along the east-west axis of London, connecting the western suburbs to the City. The line, which opened in 1900, ran straight along Oxford Street and its extensions to each end - Bayswater Road and High Holborn. The original western terminus was Shepherd's Bush, from which a single line ran to a surface depot at Wood Lane.
The line used electric locomotives for a short time, but problems with excessive vibration caused them to be replaced by multiple-unit stock, the last loco-hauled train running on 1903-06-07. There were also two steam locos, used mostly in the depots to allow stock to be moved without using power rails. Later some of the electric locos were fitted with trolley poles to draw power from overhead wires in the depots.
Though there were initial plans to provide two classes of seating, these were abandoned before opening (the resulting variety of seats remained for many years). Instead the company went to the other extreme: not only was there only one class of seat, but the fare was 2d irrespective of distance, leading to the nickname "The Twopenny Tube" (the flat fare was abandoned on 1907-07-01 with the introduction of a 3d fare for long journeys).
The company used the telegraphic address RHEOMOTOR.
When the 1908 Franco-British Exhibition made it desirable to open a station at Wood Lane, it was built on a new loop track with platforms on both sides and the depot inside the loop. The existing depot entrance line was retained as the westbound track (to stay under the streets this line makes what is still the sharpest curve - the Caxton Curve - on the entire Underground system). This meant that, to fit into the available space, the new eastbound track had to pass underneath the westbound and trains ran anticlockwise around the loop. When trains became longer, the platform inside the loop could not be lengthened without fouling the depot access track, and the solution was to extend it with a movable section 11 m (36') long which could swivel back about 0.9 m (3') to clear the access track when necessary.
The company was sold to the Yerkes group on 1913-01-01.
Back in 1905, the GWR had sponsored a separate company, the Ealing & Shepherd's Bush, to build a goods line branching off the GWR east of Ealing Broadway and joining with the West London Railway near Uxbridge Road. In 1911 the Central agreed to build an extension from Wood Lane to meet this line (at Wood Lane Junction) and to provide passenger service over it. Because of the intervention of World War I, the work was not completed until 1917, and passenger service did not start until 1920.
At Wood Lane, a new pair of platforms was added for through trains on the new track north of the existing station, but terminating trains continued to use the platforms on the loop track. The through lines joined on to the east and west sides of the loop, with the loop platform in between; since the loop ran anticlockwise, right-hand running was in use from there to a flyover at Wood Lane Junction where the link met the E&SB. This arrangement of tracks is still in use, though White City station has replaced the awkwardly arranged Wood Lane.
Although the two lines had been under common ownership since 1913, there was no station on the Central Line where it crossed the Piccadilly Line at Holborn. This was rectified in 1933 when a new interchange replaced the nearby British Museum station; unlike most of the original stations, this one had the platforms on the outside to simplify the work needed.
For a while the line was known as the Central London Line, but by 1937 this had been abbreviated to its present form.
The Central Line was significantly affected by the 1935-40 New Works Programme, where government guarantees were made available for various improvements. In the case of the Central, these came in three parts: the eastern and western extensions, and the central reconstruction.
In the west, the E&SB was crossed on the level at North Acton by the GWR line from Old Oak Common to South Ruislip and (as the GWR/GCR joint line) High Wycombe. The extension work involved adding new tracks for the Central parallel to the GWR from North Acton as far as West Ruislip; further extension to Denham was cancelled when the area was designated as Green Belt. Much of the work was done to main-line standards, as it was originally planned to run District Line trains on it as well (via Castle Bar and Greenford).
The original tubes had a nominal diameter of 3.56m (11'8¼"). However, the tubes were not well aligned, and in practice trains had to be significantly smaller than would be expected for this size (the very first CLR locomotive didn't fit into the tube until the rails had been replaced by shallower ones). This meant that stock from other lines could not be used on the Central. So in the late 1930s the tubes were expanded and realigned and the stations lengthened from 99m (325') to 130m (427'). Furthermore, the line had been built with a central positive rail 4cm (1½") above the running rails and energized at 550 V, with return through the running rails. On 1940-05-05 this was replaced with the standard LU 4-rail power system. Because of the way the tunnel was enlarged, it is no longer quite round, and for clearance reasons the outside positive rail is of a special shape and placed 4cm (1½") higher than usual.
Deep shelter tunnels (see the Northern Line for details) were built at Chancery Lane, though not opened to the public, and started but abandoned at St. Paul's.
The eastern extension was designed to allow the Central to take over several of the LNER steam branches in northeast London, reducing the congestion into Liverpool Street (some other branches were electrified at the same time). The work was delayed by World War II, but was eventually done to plan. A new tube was extended eastward, surfacing at Stratford, where the main line is on an embankment (including a bridge over the North London Line). The Central tracks come up on to the embankment, cross the bridge, and immediately dive down again; the station is on this surface section, and cross-platform interchange with the main-line services is provided. The lines then tunnel to the edge of Temple Mills Yard, where they emerge and connect to the LNER line. The latter consisted of a route to Ongar, with a loop from Woodford back to the main line at Ilford. A new shallow tube ran from Leytonstone to this loop at Newbury Park, with the section south of there abandoned.
When construction was interrupted for World War II, the eastern extension tunnels were largely complete, and were used for other purposes. One purpose was as air raid shelters, but the only access was by dimly lit stairs not intended for full-time use, and a crowd-crush disaster at Bethnal Green station killed 111 adults and 62 children (this total of 173 can be compared with the number killed in the worst bomb strike - 68 at Balham - or peacetime incident - 43 at Moorgate). Apart from a short section at the west end (bricked off from the rest), the tube tunnels between Leytonstone and Newbury Park had a different use: they became a factory for aircraft parts. Extensive work was done on them for this purpose, including fitting air conditioning throughout, digging two pairs of lift shafts (one west of Wanstead and one between Redbridge and Gants Hill) for additional access, and installing a 46cm (18") narrow gauge goods-only railway along each tunnel to provide transport within the factory. (The Germans set up similar operations in Berlin and occupied Paris, except that existing lines were used).
Floodgates are fitted in the tunnels each side of where it crosses under the River Roding.
LNER/BR passenger services were withdrawn as Central Line trains took over, though local freight services lasted much longer and the first and last trains to Epping continued to run from Liverpool Street into the 1960s. Once taken over, the section from Hainault to Woodford was operated as a self-contained shuttle, with only the occasional peak-hour trains running on to the rest of the line (and no trains ever running right round the loop). This changed to the present arrangement in the early 1990s. The north side of the loop was used as a testbed for the Automatic Train Operation later adopted on the Victoria Line.
The section from Epping to Ongar provided a refuge for steam for 8 years while a shuttle was worked by BR on behalf of LU. When electrification was completed in 1957, there still wasn't enough power to start a full-length train at Ongar, and the shuttle service remained, but now worked by one or two half-length trains. The section was eventually closed in 1994, and in 1998 it was sold to Pilot Developments, a private operator. Although the track under the M11 bridge was lowered enough to allow main-line stock to fit, no services were ever run. At the start of 2001 Pilot was released from the obligation to run the line and their operating licence was withdrawn. In 2004 the Epping-Ongar Railway Volunteer Society started a Sunday service along most of the route.
The closed station at British Museum was apparently used for the Army's London Flood Control Centre, but the access shafts have since all been filled with concrete as part of the foundations of a new building. The lift shafts at St. Paul's, disused since escalators came into use at the start of 1939, were used from 1940 to 1945 for an emergency control centre for the Central Electricity Generating Board.
On 2003-01-25 a motor fell off a train approaching Chancery Lane station after the bolts holding it in place failed, derailing the train despite the safety bracket intended to prevent this. There was a fear that the same problem might affect other trains, possibly with much more serious consequences, and the decision was taken to close the entire line (and the Waterloo & City Line, which uses the same rolling stock) until the cause was determined and rectified. The final solution required a new type of bolt and a new safety bracket. The extensiveness of the work meant it was only possible to modify a few trains a day and therefore service could only be restored gradually and in stages; the exact schedule was chosen to match the availability of stock and of alternative routes.
Pratt & Whitney Canada 747SP C-GTFF.
Originally built for Korean Air on January 30, 1981, this is 1 of only 2 747SP still flying anywhere in the world.
Still equipped with JT9D engines, she serves as a testbed for Pratt & Whitney Canada.
Arriving runway 36L at KOSH.
Air Venture 2025.
In her striking red, white and yellow paint scheme, Royal Aircraft Establishment Bedford's smart looking BAC One Eleven Series 201AC 'XX105' sits at Farnborough during the 1982 SBAC Airshow.
Acquired from British Caledonian Airways, this former BUA 'Bus Stop' jet, joined the RAE in 1971 and was the first One Eleven to adopt UK military markings being used by Bedford's BLEU (Blind Landing Experimental Unit) developing various related aids including having a coloured ‘glass’ cockpit fitted with touch screen flying controls.
Escaping the generalised Mod(PE) implemented 'Raspberry Ripple' RAE colour scheme of red, white and blue, she spent all her remaining 'life' in the red & yellow, with Bedford's Flight Systems, then at Farnborough until finally moving to Boscombe Down where after retirement with QinetiQ, she was eventually scrapped in 2010.
Scanned from an underexposed Kodak 35mm Transparency
Virgin Orbit test flight of Cosmic Girl with its rocket attached under the left wing.
The plan is to launch a payload (Up to 500kg) into space by taking the rocket up with the donated 747 (From Virgin Airways), point the aircraft upwards towards space and launch the rocket. One trip around the World and then deploy the payload,
Sounds easy but it has yet to establish itself.
The rationale is that you dont need an air base, a launch pad or a big expensive rocket to get loads into space. This 747 can take off and land at any airport and without months of prior planning refuelling etc.
Lets see if it works and what impact it will have on the space delivery market.
Speeding north through Sutton Park with a light-engine move from Derby RTC to Bescot is Network Rail Class 97's, 97304 and 97302, formerly Class 37's, 37217 and 37170, respectively.
The proud and powerful workhorse that even 50 years after its construction, continues to be a major part of the British Rail scene. I am of course talking of one of the most successful diesel locomotives of all time, the Class 37.
In the 1950's, British Rail was in desperate need to replace its ageing fleet of steam locomotives on both freight and passenger usage, and even though the new BR Standard locomotives were starting to make inroads into the Victorian built fleet, it was apparent that diesel and electric haulage was the only way forward. As such, English Electric, who had already had success with the construction of the Class 20 light freight loco and the Class 40 heavy passenger loco, were assigned to help deliver a new mulit-purpose diesel locomotive with a power output of more than 1,500bhp. Although the Class 40 could have been easily capable of handling this task, problems with these locomotives were that it was far too heavy and underpowered, which meant that in addition to hauling a heavy train, it also had the added task of hauling the actual locomotive itself! The earlier Class 40's were especially known for their unreliability, having to be frequently rescued by the steam locomotives they were built to replace!
Essentially, what English Electric did was build a scaled down version of the Class 40, shorter than its predecessor by 8 feet, weighting 33 tons less, and being powered by a much more reliable English Electric 12CSVT engine developing 1,750bhp. A batch of 42 locomotives were delivered in 1960 from the Vulcan Foundry in Newton-le-Willows, these being initially designated English Electric Type 3's, but this order was increased to 309 following the initial success of these engines, with production finishing in 1965. Work on the class was separated between several different plants, with construction primarily taking place at Vulcan Foundry, but also with assistance from Robert Stephenson & Hawthorns factory in Darlington.
The class was initially tasked with both freight and passenger workings, but the rough n' tumble nature of these engines meant they were more at home on goods trains. Some of the earlier locomotives were fitted with Steam Heating Boilers to warm passenger carriages as earlier coaches did not feature Electric Train Heating, although other locomotives had boilers added in 1967/68. Beyond the end of steam in 1968 and throughout the 1970's the Class 37's were dispersed among the many administrative Regions of British Rail, travelling the length and breadth of the country and working all manner of trains from Class 1 Express Passenger services to lower class breakdown trains and short goods services. This became apparent in its variety of liveries, especially following sectorisation of British Rail in the 1980's, with Class 37's sporting the livery of InterCity, Regional Railways and Railfreight Distribution.
Throughout their time however the fleet continued to be interchanged, especially after the introduction of the TOPS computer system which designated them Class 37. The variety of Class 37 sub-classes included:
- Class 37/3: Extended fuel tanks replacing the steam heating boiler
- Class 37/4: Addition of Electric Train Heating for use in passenger service
- Class 37/5: No major changes, a designation for engines with original split headcodes
- Class 37/6: Engines modified for use with Eurostar Class 373 units
- Class 37/7: Heavily modified for heavy freight workings, with extra ballast for more dragging power
- Class 37/9: Used as testbed for experimental Mirrlees MB275T engine
However, as the 1990's drew in and with privatisation on the horizon, it was apparent that the Class 37's were starting to look very tired. Their reliability was starting to falter, and the demands on the class were much greater than before. As such, newly formed primary freight operator EWS, made an order for a new fleet of Class 66 locomotives from General Motors to replace the many ageing British Rail classes. Upon their introduction in 1999, these engines were quick to see off many Class 37's, which went on a variety of their own journeys. In the summer of 2000 and 2001, many Class 37's were exported to France and Spain to help with the construction of their many High Speed Lines, including the LGV Méditerranée route from Lyon to Marseilles. While many of the French ones have since returned, a small fleet of Class 37's continued to work in the sun of Spain on the High Speed route between Perpignan and Figueres, but have since returned upon its opening in 2010.
In 2007, EWS was taken over by DB of Germany to become DB Schenker, which continued to operate a small fleet of Class 37's until 2010 when the last engines were retired. Throughout the 2000's these locomotives were placed into storage and scrapped, this particular era being their darkest hour. But as said, many continued to find their way into new leases of life, their reliable nature and flexible abilities making them a key part of many private fleets.
Direct Rail Services, the former rail arm of British Nuclear Fuels, took on a batch of Class 37's to operate their various freight trains, including the haulage of Nuclear Flasks, a task they continue to do till this day, with 29 of the class still on its books and in regular service. Colas Rail took on a fleet of 4 Class 37's in 2014 to expand their fleet, whilst charter company West Coast Railways owns four and four others were converted for use with Network Rail on engineering services.
Either way, it is apparent that these plucky and powerful little locomotives, of which 48 are preserved and 38 remain in mainline operation, will continue to be an integral part of the British Railway scene for many years to come.
Who knows, maybe they'll live to see mainline service when they're 100!
OY-APZ - Boeing B-720-051B - Conair of Scandinavia
at Copenhagen-Kastrup Airport (CPH) in Sept. 1984
c/n 18.384 - built in 1951
operated by TWA and later by Northwest Airlines -
operated by Maersk Air from 01/1973 -
leased to Conair between 02/1981 and 12/1987-
this aircraft was used as a flying engine testbed between 1988 and 2008 by Allied Signal / Honeywell International as N720GT and N720H -
broken-up 06/2008 (was the last airworthy 720 in the United States)
scanned from Kodachrome-slide
3-6-2004 - British Airways, British Aerospace ATP.
Info:
The aircraft was built in 1986 and was used a testbed aircraft. It was later delivered as G-BMYM, to British Midland in July 1989.
Manx Airlines were next to operate the aircraft - they took delivery as G-MAUD in December 1993.
British Airways took delivery of the aircraft in March 1997.
The aircraft went on to serve with West Air, after being converted into a freighter - they took delivery as SE-MAF in December 2006.
Today the aircraft still flies as a cargo aircraft as SE-MAF for ATP Cargo - They took delivery in August 2019.
C/n - 2002
Airbus A220-300
[Bombardier Aerospace 'CSeries' CS300 (BD-500-1A11)]
MSN 55002
C-FFDO [Airbus S.A.S. livery]
C Series Aircraft Limited Partnership (CSALP)
A380-841
MSN 006
9H-MIP ['Save the coral reefs - whose side are you on?' decals 2018]
Hi fly Malta (Hi Fly Malta Ltd)
HFM 5M
Copyright © 2018 A380spotter. All rights reserved.
CBG 18/09/12 Built 1967 Ex 66-8558 Delivered 1967 Retired 31/03/2001. Used as an engine testbed for the A400M by Marshall's of Cambridge from 2005
Nikkormat FTn w/Nikkor 50mm f 2.0 Prime
Disney World
Walt Disney World Resort (commonly known as Walt Disney World or Disney World) is an entertainment and vacation resort complex located about 20 miles (32 km) southwest of Orlando, Florida, United States. Opened on October 1, 1971, the resort is operated by Disney Experiences, a division of the Walt Disney Company.
Covering an approximate 27,000 acres (42 sq mi; 109 km2), Walt Disney World contains numerous recreational facilities designed to attract visitors for extended stays, including four theme parks, two water parks, four golf courses, conference centers, a competitive sports complex and a major shopping, dining and entertainment complex. Additionally, there are 31 Disney-owned resort hotels and one camping resort on the property, and many other non-Disney-operated hotels on and near the property.
Designed to supplement Disneyland in Anaheim, California, which had opened in 1955, the complex was planned and conceptualized by Walt Disney in the 1960s. Walt's vision for the complex was to build a new, self-contained destination resort on ample land, as he felt Disneyland had become limited by the third-party establishments that had sprung up around it. "The Florida Project", as it was then known, was intended to present a distinct vision with its own diverse set of attractions. Walt's original plans called for the inclusion of an "Experimental Prototype Community of Tomorrow" (EPCOT), a planned community intended to serve as a testbed for new city-living innovations. Walt's original vision would not progress past conceptualization, as he died on December 15, 1966, during the initial planning of the complex before construction had begun. After his death, the company wrestled with the idea of whether to bring the Disney World project to fruition; however, Walt's older brother, Roy O. Disney, came out of retirement to ensure the project was realized.
Construction began in 1967, with the company abandoning the planned community concept, instead choosing to build a theme park resort similar to Disneyland. Magic Kingdom was the first theme park to open in the complex in 1971, followed by EPCOT (then known as EPCOT Center) in 1982, Disney's Hollywood Studios (then known as the Disney-MGM Studios Theme Park) in 1989, and Disney's Animal Kingdom in 1998. Initially known as Disney World, the name of the entire resort was named Walt Disney World at Roy's insistence, to memorialize his brother.
In 2024, Walt Disney World was the most visited vacation resort in the world, with an average annual attendance of more than 49 million, while Magic Kingdom has been the most visited theme park in the world for at least the past 24 years. The opening of Walt Disney World helped turn Central Florida into a major global tourism destination and the resort has contributed singificantly to Florida's economy, generating billions in economic activity and supporting a large number of jobs across the state. The resort is the largest single-site employer in the United States, the flagship destination of Disney's worldwide corporate enterprise and has become a staple of American popular culture.
Stacks of networking switches in one rack of the DETER testbed at the USC Information Sciences Institute (ISI) in Marina Del Rey, CA.
Gloster Meteor
From Wikipedia, the free encyclopedia
Gloster Meteor Centenary of Military Aviation 2014
The only F.8 in flying condition is operated by the RAAF’s Historic Flight
RoleFighter aircraft
National originUnited Kingdom
ManufacturerGloster Aircraft Company
First flight5 March 1943
Introduction27 July 1944
Produced1943–1955
Number built3,947
The Gloster Meteor was the first British jet fighter and the Allies' only jet aircraft to engage in combat operations during the Second World War. The Meteor's development was heavily reliant on its ground-breaking turbojet engines, pioneered by Frank Whittle and his company, Power Jets Ltd. Development of the aircraft began in 1940, although work on the engines had been under way since 1936. The Meteor first flew in 1943 and commenced operations on 27 July 1944 with No. 616 Squadron RAF. The Meteor was not a sophisticated aircraft in its aerodynamics, but proved to be a successful combat fighter. Gloster's 1946 civil Meteor F.4 demonstrator G-AIDC was the first civilian-registered jet aircraft in the world.[1] Several major variants of the Meteor incorporated technological advances during the 1940s and 1950s. Thousands of Meteors were built to fly with the RAF and other air forces and remained in use for several decades.
Slower and less heavily armed than its German counterpart, the jet-powered Messerschmitt Me 262,[2] the Meteor saw limited action in the Second World War. Meteors of the Royal Australian Air Force (RAAF) fought in the Korean War. Several other operators such as Argentina, Egypt and Israel flew Meteors in later regional conflicts. Specialised variants of the Meteor were developed for use in photographic aerial reconnaissance and as night fighters.
The Meteor was also used for research and development purposes and to break several aviation records. On 7 November 1945, the first official airspeed record by a jet aircraft was set by a Meteor F.3 at 606 miles per hour (975 km/h). In 1946, this record was broken when a Meteor F.4 reached a speed of 616 miles per hour (991 km/h). Other performance-related records were broken in categories including flight time endurance, rate of climb, and speed. On 20 September 1945, a heavily modified Meteor I, powered by two Rolls-Royce Trent turbine engines driving propellers, became the first turboprop aircraft to fly.[3] On 10 February 1954, a specially adapted Meteor F.8, the "Meteor Prone Pilot", which placed the pilot into a prone position to counteract inertial forces, took its first flight.[4]
In the 1950s, the Meteor became increasingly obsolete as more nations developed jet fighters, many of these newcomers having adopted a swept wing instead of the Meteor's conventional straight wing; in RAF service, the Meteor was replaced by newer types such as the Hawker Hunter and Gloster Javelin. As of 2018, two Meteors, G-JSMA and G-JWMA, remain in active service with the Martin-Baker company as ejection seat testbeds.[5] One further aircraft in the UK remains airworthy, as does another in Australia.
See also: Frank Whittle
The development of the turbojet-powered Gloster Meteor was a collaboration between the Gloster Aircraft Company and Frank Whittle's firm, Power Jets Ltd. Whittle formed Power Jets Ltd in March 1936 to develop his ideas of jet propulsion, Whittle himself serving as the company's chief engineer.[6] For several years, attracting financial backers and aviation firms prepared to take on Whittle's radical ideas was difficult; in 1931, Armstrong-Siddeley had evaluated and rejected Whittle's proposal, finding it to be technically sound but at the limits of engineering capability.[7] Securing funding was a persistently worrying issue throughout the early development of the engine.[8] The first Whittle prototype jet engine, the Power Jets WU, began running trials in early 1937; shortly afterwards, both Sir Henry Tizard, chairman of the Aeronautical Research Committee, and the Air Ministry gave the project their support.[9]
On 28 April 1939, Whittle made a visit to the premises of the Gloster Aircraft Company, where he met several key figures, such as George Carter, Gloster's chief designer.[10] Carter took a keen interest in Whittle's project, particularly when he saw the operational Power Jets W.1 engine; Carter quickly made several rough proposals of various aircraft designs powered by the engine. Independently, Whittle had also been producing several proposals for a high-altitude jet-powered bomber; following the start of the Second World War and the Battle for France, a greater national emphasis on fighter aircraft arose.[11] Power Jets and Gloster quickly formed a mutual understanding around mid-1939.[12]
The Gloster E.28/39. The yellow undersides were standard for RAF training and prototype aircraft of the period.
In spite of ongoing infighting between Power Jets and several of its stakeholders, the Air Ministry contracted Gloster in late 1939 to manufacture a prototype aircraft powered by one of Whittle's new turbojet engines.[13] The single-engined proof-of-concept Gloster E28/39, the first British jet-powered aircraft, conducted its maiden flight on 15 May 1941, flown by Gloster's chief test pilot, Flight Lieutenant Philip "Gerry" Sayer.[14][15] The success of the E.28/39 proved the viability of jet propulsion, and Gloster pressed ahead with designs for a production fighter aircraft.[16] Due to the limited thrust available from early jet engines, it was decided that subsequent production aircraft would be powered by a pair of turbojet engines.[17]
In 1940, for a "military load" of 1,500 lb (680 kg), the Royal Aircraft Establishment (RAE) had advised that work on an aircraft of 8,500 lb (3,900 kg) all-up weight, with a total static thrust of 3,200 lbf (14 kN) should be started, with an 11,000 lb (5,000 kg) design for the expected, more powerful, W.2 and axial engine designs. George Carter's calculations based on the RAE work and his own investigations were that a 8,700-to-9,000-pound (3,900-to-4,100-kilogram) aircraft with two or four 20 mm cannons and six 0.303 machine guns would have a top speed of 400–431 miles per hour (644–694 km/h) at sea level and 450–470 miles per hour (720–760 km/h) at 30,000 feet (9,100 m). In January 1941 Gloster were told by Lord Beaverbrook that the twin jet fighter was of "unique importance", and that the company was to stop work on a night-fighter development of their F.9/37 to Specification F.18/40.[18]
Prototypes
Prototype Meteor DG202/G on display at the Royal Air Force Museum London in 2011. The "/G" appended to the aircraft serial denoted that the aircraft was to have an armed guard at all times while it was on the ground.
In August 1940, Carter presented Gloster's initial proposals for a twin-engined jet fighter with a tricycle undercarriage.[Note 1] On 7 February 1941, Gloster received an order for twelve prototypes (later reduced to eight) under Specification F9/40.[20] A letter of intent for the production of 300 of the new fighter, initially to be named Thunderbolt, was issued on 21 June 1941; to avoid confusion with the USAAF Republic P-47 Thunderbolt which had been issued with the same name to the RAF in 1944, the aircraft's name was subsequently changed to Meteor.[21][22][Note 2] During the aircraft's secretive development, employees and officials made use of the codename Rampage to refer to the Meteor, as similarly the de Havilland Vampire would initially be referred to as the Spider Crab. Test locations and other key project information were also kept secret.[24]
Although taxiing trials were carried out in 1942, it was not until the following year that any flights took place due to production and approval holdups with the Power Jets W.2 engine powering the Meteor.[14][25] On 26 November 1942 production of the Meteor was ordered to stop due to the delays at subcontractor Rover, which was struggling to manufacture the W.2 engines on schedule[Note 3]; considerable interest was shown in Gloster's E.1/44 proposal for a single-engine fighter, unofficially named Ace.[27] Gloster continued development work on the Meteor and the production-stop order was overturned in favour of the construction of six (later increased to eight) F9/40 prototypes alongside three E.1/44 prototypes.[28] Rover's responsibilities for development and production of the W.2B engine were also transferred to Rolls-Royce that year.[29]
On 5 March 1943, the fifth prototype, serial DG206, powered by two substituted de Havilland Halford H.1 engines owing to problems with the intended W.2 engines, became the first Meteor to become airborne at RAF Cranwell, piloted by Michael Daunt.[14] On the initial flight, an uncontrollable yawing motion was discovered, which led to a redesigned larger rudder; however, no difficulties had been attributed to the groundbreaking turbojet propulsion.[30][31] Only two prototypes flew with de Havilland engines because of their low flight endurance.[32] Before the first prototype aircraft had even undertaken its first flight, an extended order for 100 production-standard aircraft had been placed by the RAF.[33]
The first Whittle-engined aircraft, DG205/G,[Note 4] flew on 12 June 1943 (later crashing during takeoff on 27 April 1944) and was followed by DG202/G on 24 July. DG202/G was later used for deck handling tests aboard aircraft carrier HMS Pretoria Castle.[35][36] DG203/G made its first flight on 9 November 1943, later becoming a ground instructional airframe. DG204/G, powered by Metrovick F.2 engines, first flew on 13 November 1943; DG204/G was lost in an accident on 4 January 1944, the cause believed to have been an engine compressor failure due to overspeed.[37] DG208/G made its début on 20 January 1944, by which time the majority of design problems had been overcome and a production design had been approved. DG209/G was used as an engine testbed by Rolls-Royce, first flying on 18 April 1944. DG207/G was intended to be the basis for the Meteor F.2 with de Havilland engines, but it did not fly until 24 July 1945, at which time the Meteor 3 was in full production and de Havilland's attention was being redirected to the upcoming de Havilland Vampire; consequently the F.2 was cancelled.[38][39][40][41]
Into production
Gloster Meteor being deployed in March 1945
On 12 January 1944, the first Meteor F.1, serial EE210/G, took to the air from Moreton Valence in Gloucestershire. It was essentially identical to the F9/40 prototypes except for the addition of four nose-mounted 20 mm (.79 in) Hispano Mk V cannon and some changes to the canopy to improve all-round visibility.[42] Due to the F.1's similarity to the prototypes, they were frequently operated in the test program to progress British understanding of jet propulsion, and it took until July 1944 for the aircraft to enter squadron service.[43] EE210/G was later sent to the U.S. for evaluation in exchange for a pre-production Bell YP-59A Airacomet, the Meteor being flown first by John Grierson at Muroc Army Airfield on 15 April 1944.[44]
Originally 300 F.1s were ordered, but the total produced was reduced to 20 aircraft as the follow-on orders had been converted to the more advanced models.[45] Some of the last major refinements to the Meteor's early design were trialled using this first production batch, and what was to become the long-term design of the engine nacelles was introduced upon EE211.[46] The original nacelles had been discovered by the RAE to suffer from compressibility buffeting at higher speeds, causing increased drag; the re-designed longer nacelles eliminated this and provided an increase in the Meteor's maximum speed. The lengthened nacelles were introduced on the final fifteen Meteor IIIs.[3] EE215 was the first Meteor to be fitted with guns; EE215 was also used in engine reheat trials,[47] the addition of reheat increasing top speed from 420 mph to 460 mph.[3] and was later converted into the first two-seat Meteor.[48] Due to the radical differences between jet-powered aircraft and those that it replaced, a special Tactical Flight or T-Flight unit was established to prepare the Meteor for squadron service, led by Group Captain Hugh Joseph Wilson.[49] The Tactical Flight was formed at Farnborough in May 1944, the first Meteors arriving the following month, upon which both tactical applications and limitations were extensively explored.[50]
On 17 July 1944, the Meteor F.1 was cleared for service use. Shortly afterwards, elements of the Tactical Flight and their aircraft were transferred to operational RAF squadrons.[51] The first deliveries to No. 616 Squadron RAF, the first operational squadron to receive the Meteor, began in July 1944.[33] When the F.2 was cancelled, the Meteor F.3 became the immediate successor to the F.1 and alleviated some of the shortcomings of the F.1.[52] In August 1944, the first F.3 prototype flew; early F.3 production aircraft were still fitted with the Welland engine as the Derwent engine's production was just starting at this point. A total of 210 F.3 aircraft were produced before they were in turn superseded by production of the Meteor F.4 in 1945.[53]
Several Meteor F.3s were converted into navalised aircraft. The adaptations included a strengthened undercarriage and arrester hook. Operational trials of the type took place aboard HMS Implacable. The trials included carrier landings and takeoffs.[54] Performance of these naval prototype Meteors proved to be favourable, including takeoff performance, leading to further trials with a modified Meteor F.4 fitted with folding wings; a 'clipped wing' was also adopted.[55] The Meteor later entered service with the Royal Navy, but only as a land-based trainer, the Meteor T.7, to prepare pilots of the Fleet Air Arm for flying other jet aircraft such as the de Havilland Sea Vampire.[56]
While various marks of Meteor had been introduced by 1948, they had remained very similar to the prototypes of the Meteor; consequently, the performance of the Meteor F.4 was beginning to be eclipsed by new jet designs. Gloster therefore embarked on a redesign programme to produce a new version of the Meteor with better performance.[57] Designated 'Meteor F.8', this upgraded variant was a potent fighter aircraft, forming the bulk of RAF Fighter Command between 1950 and 1955. The Meteor continued to be operated in a military capacity by several nations into the 1960s.[58]
Night fighter
To replace the increasingly obsolete de Havilland Mosquito as a night fighter, the Meteor was adapted to serve in the role as an interim aircraft. Gloster had initially proposed a night fighter design to meet the Air Ministry specification for the Mosquito replacement, based on the two seater trainer variant of the Meteor, with the pilot in the front seat and the navigator in the rear.[59] Once accepted however, work on the project was swiftly transferred to Armstrong Whitworth to perform both the detailed design process and production of the type; the first prototype flew on 31 May 1950. Although based on the T.7 twin seater, it used the fuselage and tail of the F.8, and the longer wings of the F.3. An extended nose contained the AI Mk 10 (the 1940s Westinghouse SCR-720) Air Intercept radar. As a consequence the 20 mm cannons were moved into the wings, outboard of the engines. A ventral fuel tank and wing mounted drop tanks completed the Armstrong Whitworth Meteor NF.11.[60][61]
Operational Meteor NF.14 of No. 264 Squadron RAF in 1955
As radar technology developed, a new Meteor night fighter was developed to use the improved US-built APS-21 system. The NF.12 first flew on 21 April 1953. It was similar to the NF.11 but had a nose section 17 inches (43 cm) longer;[62] the fin was enlarged to compensate for the greater keel area of the enlarged nose and to counter the airframe reaction to the sideways oscillating motion of the radar scanner which caused difficulty aiming the guns, an anti-tramp motor operating on the rudder was fitted midway up the front leading edge of the fin. The NF.12 also had the new Rolls-Royce Derwent 9 engines and the wings were reinforced to handle the new engine.[63][64] Deliveries of the NF.12 started in 1953, with the type entering squadron service in early 1954,[65] equipping seven squadrons (Nos 85, 25, 152, 46, 72, 153 and 64);[66] the aircraft was replaced over 1958–1959.
The final Meteor night fighter was the NF.14. First flown on 23 October 1953, the NF.14 was based on the NF.12 but had an even longer nose, extended by a further 17 inches to accommodate new equipment, increasing the total length to 51 ft 4 in (15.65 m) and a larger bubble canopy to replace the framed T.7 version.[67] Just 100 NF.14s were built; they first entered service in February 1954 beginning with No. 25 Squadron and were being replaced as early as 1956 by the Gloster Javelin. Overseas, they remained in service a little longer, serving with No. 60 Squadron at Tengah, Singapore until 1961. As the NF.14 was replaced, some 14 were converted to training aircraft as the NF(T).14 and given to No. 2 Air Navigation School on RAF Thorney Island until transferring to No. 1 Air Navigation School at RAF Stradishall where they served until 1965.[68]
Design
Meteor F.8 in flight at RAF Greenham Common, May 1986
Gloster Meteor F.8 Cockpit
The first operational version of the Meteor, designated as the Meteor F.1, apart from the minor airframe refinements, was a straightforward 'militarisation' of the earlier F9/40 prototypes.[69] The dimensions of the standard Meteor F.1 were 41 ft 3 in (12.57 m) long with a span of 43 ft 0 in (13.11 m), with an empty weight of 8,140 lb (3,690 kg) and a maximum takeoff weight of 13,795 lb (6,257 kg).[42] Despite the revolutionary turbojet propulsion used,[70] the design of the Meteor was relatively orthodox and did not take advantage of many aerodynamic features used on other, later jet fighters, such as swept wings; the Meteor shared a broadly similar basic configuration to its German equivalent, the Messerschmitt Me 262, which was also aerodynamically conventional.[71]
It was an all-metal aircraft with a tricycle undercarriage and conventional low, straight wings with mid-mounted turbojet engines and a high-mounted tailplane clear of the jet exhaust.[Note 5][Note 6] The Meteor F.1 exhibited some problematic flying characteristics typical of early jet aircraft; it suffered from stability problems at high transonic speeds, large trim changes, high stick forces and self-sustained yaw instability (snaking) caused by airflow separation over the thick tail surfaces.[73] The longer fuselage of the Meteor T.7, a two-seater trainer, significantly reduced the aerodynamic instability that the early Meteors were known for.[74]
Later Meteor variants would see a large variety of changes from the initial Meteor F.1 introduced to service in 1944. Much attention was given to raising the aircraft's top speed, often by improving the airframe's aerodynamic qualities, incorporating the latest engine developments, and increasing the strength of the airframe.[69][75] The Meteor F.8, which emerged in the late 1940s, was considered to have substantially improved performance over prior variants;[76] the F.8 was reportedly the most powerful single-seat aircraft flying in 1947, capable of ascending to 40,000 feet (12,000 m) within five minutes.[77]
Construction
From the outset, each Meteor was constructed from several modular sections or separately produced units, a deliberate design choice to allow for production to be dispersed and for easy disassembly for transport.[78] Each aircraft comprised five main sections: nose, forward fuselage, central section, rear fuselage and tail units; the wings were also built out of lengthwise sections.[79] The forward section contained the pressure cabin, gun compartments, and forward undercarriage. The centre section incorporated much of the structural elements, including the inner wing, engine nacelles, fuel tank, ammunition drums, and main undercarriage. The rear fuselage was of a conventional semi-monocoque structure. Various aluminium alloys were the primary materials used throughout the structure of the Meteor, such as the stressed duralumin skin.[80]
Across the Meteor's production life, various different companies were subcontracted to manufacture aircraft sections and major components; due to the wartime workload on producing fighter aircraft such as the Hawker Hurricane and Hawker Typhoon, neither Gloster nor the wider Hawker Siddeley Group were able to internally meet the production demand of 80 aircraft per month.[23] Bristol Tramways produced the forward fuselage of the aircraft, the Standard Motor Company manufactured the central fuselage and inner wing sections, the Pressed Steel Company produced the rear fuselage, and Parnall Aircraft made the tail unit.[81] Other main subcontractors included Boulton Paul Aircraft, Excelsior Motor Radiator Company, Bell Punch, Turner Manufacturing Company, and Charlesworth Bodies; as many of these firms had little or no experience producing aircraft, both quality and interchangeability of components were maintained by contractually enforced adherence to Gloster's original drawings.[82]
From the Meteor F.4 onwards, Armstrong Whitworth began completing whole units at their Coventry facility in addition to Gloster's own production line.[83] Belgian aviation firm Avions Fairey also produced the Meteor F.8 under licence from Gloster for the Belgian Air Force; a similar licence manufacturing arrangement was made with Dutch company Fokker to meet the Royal Netherlands Air Force's order.[84]
Engines
Rolls-Royce Welland engine on display. The rear of the engine is at the left.
The Meteor F.1 was powered by two Rolls-Royce Welland turbojet engines, Britain's first production jet engines, which were built under licence from Whittle's designs.[29] The Meteor embodied the advent of practical jet propulsion; in the type's service life, both military and civil aviation manufacturers rapidly integrated turbine engines into their designs, favouring its advantages such as smoother running and greater power output.[85] The Meteor's engines were considerably more practical than those of the German Me 262 as, unlike the Me 262, the engines were embedded into the wing in nacelles between the front and rear spars rather than underslung, saving some weight due to shorter landing gear legs and less massive spars.[86][Note 7]
The W.2B/23C engines upon which the Welland was based produced 1,700 lbf (7.6 kN) of thrust each, giving the aircraft a maximum speed of 417 mph (671 km/h) at 9,800 feet (3,000 m) and a range of 1,000 miles (1,600 km).[42] It incorporated a hydraulically driven engine starter developed by Rolls-Royce, which was automated following the press of a starter button in the cockpit.[Note 8] The engines also drove hydraulic and vacuum pumps as well as a generator via a Rotol gearbox fixed on the forward wing spar;[29] the cockpit was also heated by bleed air from one of the engines.[80] The acceleration rate of the engines was manually controlled by the pilot; rapid engine acceleration would frequently induce compressor stalls early on; the likelihood of compressor stalls was effectively eliminated upon further design refinements of both the Welland engine and the Meteor itself.[88] At high speeds the Meteor had a tendency to lose directional stability, often during unfavourable weather conditions, leading to a 'snaking' motion; this could be easily resolved by throttling back to reduce speed.[89]
Based upon designs produced by Power Jets, Rolls-Royce produced more advanced and powerful turbojet engines. Beyond numerous improvements made to the Welland engine that powered the early Meteors, Rolls-Royce and Power Jets collaborated to develop the more capable Derwent engine, which as the Rover B.26 had undergone a radical re-design from the W.2B/500 while at Rover. The Derwent engine, and the re-designed Derwent V based on the Nene, was installed on many of the later production Meteors; the adoption of this new powerplant led to considerable performance increases.[29][86][Note 9] The Meteor often served as the basis for the development of other early turbojet designs; a pair of Meteor F.4s were sent to Rolls-Royce to aid in their experimental engine trials, RA435 being used for reheat testing, and RA491 being fitted with the Rolls-Royce Avon, an axial-flow engine.[29][91] From their involvement in the development of the Meteor's engines, Armstrong-Siddeley, Bristol Aircraft, Metropolitan-Vickers, and de Havilland also independently developed their own gas turbine engines.[92]
Performance
Meteor NF.11 (right) flying with a Hawker Hunter T7A at the Cotswold Air Show in 2009
During development, sceptical elements of the Air Ministry had expected mature piston-powered aircraft types to exceed the capabilities of the Meteor in all respects except that of speed; thus, the performance of early Meteors was considered favourable for the interceptor mission, being capable of out-diving the majority of enemy aircraft.[93] The conclusion of in-service trials conducted between the Meteor F.3. and the Hawker Tempest V was that the performance of the Meteor exceeded the Tempest in almost all respects and that, barring some manoeuvrability issues, the Meteor could be considered a capable all-round fighter.[94] Pilots formerly flying piston-engine aircraft often described the Meteor as being exciting to fly. British politician Norman Tebbit stated of his experience flying the Meteor in the RAF: "Get airborne, up with the wheels, hold it low until you were about 380 knots, pull it up and she would go up, well we thought then, like a rocket".[95]
Early jet engines consumed a lot more fuel than the piston engines they replaced so the Welland engines imposed considerable flight-time limitations on the Meteor F.1, leading to the type being used for local interception duties only. In the post-war environment, there was considerable pressure to increase the range of interceptors to counter the threat of bombers armed with nuclear weapons.[96] The long-term answer to this question was in-flight refuelling; several Meteors were provided to Flight Refuelling Limited for trials of the newly developed probe-and-drogue refuelling techniques. This capability was not incorporated in service Meteors, which had already been supplanted by more modern interceptor aircraft at this point.[97]
A total of 890 Meteors were lost in RAF service (145 of these crashes occurring in 1953 alone), resulting in the deaths of 450 pilots. Contributory factors in the number of crashes were the poor brakes, failure of the landing gear, the high fuel consumption and consequent short flight endurance (less than one hour) causing pilots to run out of fuel, and difficult handling with one engine out due to the widely set engines. The casualty rate was exacerbated by the lack of ejection seats in early series Meteors;[98] the much higher speed that the aircraft was capable of meant that to bail out pilots might have to overcome high g forces and fast-moving airflow past the cockpit; there was also a greater likelihood of the pilot striking the horizontal tailplane.[99] Ejection seats were fitted in the later F.8, FR.9, PR.10 and some experimental Meteors.[100][101][page needed] The difficulty of baling out of the Meteor had been noted by pilots during development, reporting several contributing design factors such as the limited size and relative position of the cockpit to the rest of the aircraft, and difficulty in using the two-lever jettisonable hood mechanism.[102]
Operational service
Second World War
Gloster Meteor F.1 of No. 616 Squadron
No. 616 Squadron RAF was the first to receive operational Meteors: a total of 14 aircraft were initially delivered. The squadron was based at RAF Culmhead, Somerset and had been equipped with the Spitfire VII.[103] The conversion to the Meteor was initially a matter of great secrecy.[104] Following a conversion course at Farnborough attended by the squadron's six leading pilots, the first aircraft was delivered to Culmhead on 12 July 1944.[14][Note 10] The squadron and its seven Meteors moved on 21 July 1944 to RAF Manston on the east Kent coast and, within a week, 32 pilots had been converted to the type.[105]
The Meteor was initially used to counter the V-1 flying bomb threat. 616 Squadron Meteors saw action for the first time on 27 July 1944, when three aircraft were active over Kent. These were the first operational jet combat missions for the Meteor and for the Royal Air Force. After some problems, especially with jamming guns, the first two V-1 "kills" were made on 4 August.[106] By war's end, Meteors had accounted for 14 flying bombs.[107] After the end of the V-1 threat, and the introduction of the ballistic V-2 rocket, the RAF was forbidden to fly the Meteor on combat missions over German-held territory for fear of an aircraft being shot down and salvaged by the Germans.
No. 616 Squadron briefly moved to RAF Debden to allow United States Army Air Forces (USAAF) bomber crews to gain experience and create tactics in facing jet-engined foes before moving to Colerne, Wiltshire. For a week from 10 October 1944 a series of exercises were carried out in which a flight of Meteors made mock attacks on a formation of 100 B-24s and B-17s escorted by 40 Mustangs and Thunderbolts. These suggested that, if the jet fighter attacked the formation from above, it could take advantage of its superior speed in the dive to attack the bombers and then escape by diving through the formation before the escorts could react. The best tactic to counter this was to place a fighter screen 5,000 ft above the bombers and attempt to intercept the jets early in the dive.[108] The exercise was also useful from No. 616 Squadron's perspective, giving valuable practical experience in Meteor operations.[109]
Meteor F.3s with original short engine nacelles
No. 616 Squadron exchanged its F.1s for the first Meteor F.3s on 18 December 1944. These first 15 F.3s differed from the F.1 in having a sliding canopy in place of the sideways hinging canopy, increased fuel capacity and some airframe refinements. They were still powered by Welland I engines.[110] Later F.3s were equipped with the Derwent I engines. This was a substantial improvement over the earlier mark, although the basic design still had not reached its potential. Wind tunnel and flight tests demonstrated that the original short nacelles, which did not extend far fore and aft of the wing, contributed heavily to compressibility buffeting at high speed. New, longer nacelles not only cured some of the compressibility problems but added 75 miles per hour (120 km/h) at altitude, even without upgraded powerplants. The last batch of Meteor F.3s featured the longer nacelles; other F.3s were retrofitted in the field with the new nacelles. The F.3 also had the new Rolls-Royce Derwent engines, increased fuel capacity, and a new larger, more strongly raked bubble canopy.[53]
Judging the Meteor F.3s were ready for combat over Europe, the RAF finally decided to deploy them on the continent. On 20 January 1945, four Meteors from 616 Squadron were moved to Melsbroek in Belgium and attached to the Second Tactical Air Force,[111] just under three weeks after the Luftwaffe's surprise Unternehmen Bodenplatte attack on New Year's Day, in which Melsbroek's RAF base, designated as Allied Advanced Landing Ground "B.58", had been struck by piston-engined fighters of JG 27 and JG 54. The 616 Squadron Meteor F.3s' initial purpose was to provide air defence for the airfield, but their pilots hoped that their presence might provoke the Luftwaffe into sending Me 262 jets against them.[103] At this point the Meteor pilots were still forbidden to fly over German-occupied territory, or to go east of Eindhoven, to prevent a downed aircraft being captured by the Germans or the Soviets.[112]
Ground crew servicing a Meteor of 616 Squadron at Melsbroek, Belgium, 1945. The all-white finish used by the four F.3s sent to Belgium was to aid recognition by ground troops during familiarisation training before the operational F.3 aircraft arrived
In March, the entire squadron was moved to Gilze-Rijen Air Base and then in April, to Nijmegen. The Meteors flew armed reconnaissance and ground attack operations without encountering any German jet fighters. By late April, the squadron was based at Faßberg, Germany and suffered its first losses when two aircraft collided in poor visibility. The war ended with the Meteors having destroyed 46 German aircraft through ground attack.[citation needed] Friendly fire through misidentification as Messerschmitt Me 262s by Allied anti-aircraft gunners was more of a threat than the already-diminished forces of the Luftwaffe; to counter this, continental-based Meteors were given an all-white finish as a recognition aid.[109][111][113]
Post-war
The next-generation Meteor F.4 prototype first flew on 17 May 1945, and went into production in 1946 when 16 RAF squadrons were already operating Meteors.[113] Equipped with Rolls-Royce Derwent 5 engines, the smaller version of the Nene, the F.4 was 170 mph (270 km/h) faster than the F.1 at sea level (585 against 415), but the reduced wings impaired its rate of climb.[114][Note 11] The F.4 wingspan was 86.4 cm shorter than the F.3 and with blunter wing tips, derived from the world speed record prototypes. Improvements included a strengthened airframe, fully pressurised cockpit, lighter ailerons to improve manoeuvrability, and rudder trim adjustments to reduce snaking. The F.4 could be fitted with a drop tank under each wing, and experiments were carried out with carriage of underwing stores and also in lengthened fuselage models.
Because of increased demand, F.4 production was divided between Gloster and Armstrong Whitworth. The majority of early F.4s did not go to the RAF: 100 were exported to Argentina, seeing action on both sides in the 1955 revolution;[115] in 1947, only RAF Nos. 74 and 222 squadrons were fully equipped with the F.4. Nine further RAF squadrons converted from 1948 onwards. From 1948, 38 F.4s were exported to the Dutch, equipping four squadrons (322, 323, 326 and 327) split between bases in Soesterberg and Leeuwarden until the mid-1950s. In 1949, only two RAF squadrons were converted to the F.4, Belgium was sold 48 aircraft in the same year (going to 349 and 350 squadrons at Beauvechain) and Denmark received 20 over 1949–1950. In 1950, three more RAF squadrons were upgraded, including No. 616 and, in 1951, six more.
WA742, a two-seat Meteor T7 in 1961
A modified two-seater F.4 for jet-conversion and advanced training was tested in 1949 as the T.7. It was accepted by the RAF and the Fleet Air Arm and became a common addition to the various export packages (for example 43 to Belgium between 1948 and 1957, a similar number to the Netherlands over the same period, two to Syria in 1952, six to Israel in 1953, etc.). Despite its limitations – unpressurised cockpit, no armament, limited instructor instrumentation – more than 650 T.7s were manufactured.[116][117] The T.7 remained in RAF service into the 1970s.[118]
As improved jet fighters emerged, Gloster decided to modernise the F.4 while retaining as much of the manufacturing tooling as possible. The result was the definitive production model, the Meteor F.8 (G-41-K), serving as a major RAF fighter until the introduction of the Hawker Hunter and the Supermarine Swift. The first prototype F.8 was a modified F.4, followed by a true prototype, VT150, that flew on 12 October 1948 at Moreton Valence.[119] Flight testing of the F.8 prototype led to the discovery of an aerodynamic problem: after ammunition was expended, the aircraft became tail-heavy and unstable around the pitch axis due to the weight of fuel in fuselage tanks no longer being balanced by the ammunition. Gloster solved the problem by substituting the tail of the abortive G 42 single-engined jet fighter. The F.8 and other production variants successfully used the new tail design, giving the later Meteors a distinctive appearance, with taller straighter edges compared with the rounded tail of the F.4s and earlier marks.[120]
Meteor F.8 at the Danish Flight Museum, 2006
The F.8 also featured a fuselage stretch of 76 cm (30 in), intended to shift the aircraft's centre of gravity and also eliminate the use of ballast formerly necessary in earlier marks due to the subsequent elimination from the design of two of the originally designed six installed cannon. The F.8 incorporated uprated engines, Derwent 8s, with 3,600 lbf (16 kN) thrust each combined with structural strengthening, a Martin Baker ejection seat and a "blown" teardrop cockpit canopy that provided improved pilot visibility.[121] Between 1950 and 1955, the Meteor F.8 was the mainstay of RAF Fighter Command, and served with distinction in combat in Korea with the RAAF as well as operating with many air forces worldwide, although it was clear that the original design was obsolete compared with contemporary swept-wing fighters such as the North American F-86 Sabre and the Soviet MiG-15.[122]
Initial deliveries of the F.8 to the RAF were in August 1949, with the first squadron receiving its fighters in late 1950. Like the F.4, there were strong export sales of the F.8. Belgium ordered 240 aircraft, the majority assembled in The Netherlands by Fokker. The Netherlands had 160 F.8s, equipping seven squadrons until 1955. Denmark had 20, ordered in 1951, the last F.8s in front-line service in Europe. The RAAF ordered 94 F.8s, which served in the Korean War. Despite arms embargoes, both Syria and Egypt received F.8s from 1952, as did Israel, each using their Meteors during the Suez Crisis. Brazil ordered 60 new Meteor F.8s and 10 T.7 trainers in October 1952, paying with 15,000 tons of raw cotton.[123]
In the 1950s, Meteors were developed into effective photo-reconnaissance, training and night fighter versions. The fighter reconnaissance (FR) versions were the first to be built, replacing the ageing Spitfires and Mosquitos then in use. Two FR.5s were built on the F.4 body; one was used for nose section camera tests, the other broke up in midair while in testing over Moreton Valence. On 23 March 1950, the first FR.9 flew. Based on the F.8, it was 20 cm longer with a new nose incorporating a remote control camera and window and was also fitted with additional external ventral and wing fuel tanks. Production of the FR.9 began in July. No. 208 Squadron, then based at Fayid, Egypt was the first to be upgraded followed by the 2nd Tactical Air Force in West Germany, No. 2 Squadron RAF at Bückeburg and No. 79 Squadron RAF at RAF Gutersloh flew the FR.9 from 1951 until 1956. In Aden, No. 8 Squadron RAF was given FR.9s in November 1958 and used them until 1961.[124] Ecuador (12), Israel (7) and Syria (2) were foreign customers for the FR.9.[125]
In 1951, 29, 141, 85 and 264 squadrons each received a number of NF.11 aircraft, the first of the Meteor night fighters.[126] It was rolled out across the RAF until the final deliveries in 1954.[127] A "tropicalised" version of the NF.11 for the Middle East was developed; first flying on 23 December 1952 as the NF.13. The aircraft equipped No. 219 Squadron RAF at Kabrit and No. 39 Squadron at Fayid, both in Egypt. The aircraft served during the Suez crisis and remained with No. 39 Squadron after they were withdrawn to Malta until 1958. Several problems were encountered: the heavily framed T.7 canopy made landings tricky due to limited visibility, the under-wing external fuel tanks tended to break up when the wing cannons were fired, and gun harmonisation, normally set to about 400 yards, was poor due to the wings flexing in flight. Belgium (24), Denmark (20) and France (41) were foreign customers for the NF.11.[128] Ex-RAF NF.13s were sold to France (two), Syria (six), Egypt (six) and Israel (six).[129]
In addition to the armed, low altitude operation, tactical FR.9 variant, Gloster also developed the PR.10 for high altitude missions.[130] The first prototype flew on 29 March 1950 and was actually converted into the first production aircraft. Based on the F.4, it had the F.4-style tail and the longer wings of the earlier variant. All the cannons were removed and a single camera placed in the nose with two more in the rear fuselage; the canopy was also changed. The PR.10 was delivered to the RAF in December 1950 and were given to No. 2 and No. 541 squadrons in Germany and No. 13 Squadron RAF in Cyprus. The PR.10 was rapidly phased out from 1956; rapid improvements in surface-to-air missile technology and the introduction of newer aircraft capable of flying at greater altitudes and speeds had rendered the aircraft obsolete.
Reshade 0.15 Extreme Eyecancer Mod Testbed 0.1A
Blackfire's mod + TOD + Reli2
Ini tweaks + POM enabled
Lite TOD, light shadows, nohud, dof %25-50, adjusted brightess, contrast and gamma + exposure
80º FoV
SMAA (sweetfx+master effect) FXAA (custom settings)
Tonemap
Lensdirt
Vibrance
GPC Dof
Chromatic Aberration
Grain + noise
Letterbox
N757HW - Boeing B-757-225 - Honeywell International Inc.
"Connected Aircraft"-titles and various other stickers
at Hamilton International Airport (YHM)
c/n 22.194 - built in 1982 for Eastern Airlines -
operated by Honeywell since 2005 as a flying testbed
76529 (cn 073410308) PD-14 engine flight testbed.
www.airliners.net/photo/Gromov-Flight-Research-Institute/...
Handley Page HP 137 Jetstream G RAVL at Cranfield Bedfordshire (EGTC), first flown in 1969 but with Racal/Decca Navigation from 1974, last used by Cranfield University as a flying equipment testbed WFU in 2004.
12/2024 - NS 1000 is still around. This is the engine testbed unit used mostly in the 90s and early 2000. It's been quite a while since this unit was used. It's a former EL SD45 that wore a bicentennial scheme.
NASA tested new "eyes" for its next Mars rover mission on a rocket built by Masten Space Systems in Mojave, California, thanks in part to NASA's Flight Opportunities Program, or FOP.
The agency's Jet Propulsion Laboratory in Pasadena, California, is leading development of the Mars 2020 rover and its Lander Vision System, or LVS. In 2014, the prototype vision system launched 1,066 feet (325 meters) into the air aboard Masten's rocket-powered "Xombie" test platform and helped guide the rocket to a precise landing at a predesignated target. LVS flew as part of a larger system of experimental landing technologies called the Autonomous Descent and Ascent Powered-flight Testbed, or ADAPT.
LVS, a camera-based navigation system, photographs the terrain beneath a descending spacecraft and matches it with onboard maps allowing the craft to detect its location relative to landing hazards, such as boulders and outcroppings.
The system can then direct the craft toward a safe landing at its primary target site or divert touchdown toward better terrain if there are hazards in the approaching target area. Image matching is aided by an inertial measurement unit that monitors orientation.
The Northrop N-1M, also known by the nickname "Jeep" (although I'm not sure why) was an American experimental aircraft used in the development of the flying wing concept during the 1940s.
The aircraft designer Jack Northrop became involved in innovative all-wing aircraft designs in the late-1920s, with his first flying wing being built in the 1928–1930 time period. That first prototype, the 1929 Flying Wing X-216H, had an open cockpit in the centre-wing section and single, rear-facing, pusher propeller connected to a piston engine blended into the all-wing shape. It was first test-flown in 1929 with Edward Bellande at the controls; the aircraft displayed adequate performance and was noted for its unique all-metal stressed skin and multi-cellular construction. At about this same time, Jack Northrop became aware of Walter and Reimar Horten's record-setting "tailless" flying wing glider designs being tested in Germany beginning in 1934.
The N-1M was one of a progression of experimental aircraft that further developed Northrop's all-wing concept. The aircraft was developed during 1939 and 1940 as a flying test-bed for the purpose of proving Northrop's vision of a practical flying wing. Built mostly of specially-laminated layers of glued wood, the design of both wooden wings allowed for easy configuration changes with the central blended fuselage, which was made of tubular steel. The diminutive, twin-engine test aircraft served its purpose well, first taking to the skies on 3 July 1941 at Baker Dry Lake in California.
Northrop's chief test pilot, Vance Breese, flew the N-1M on its maiden flight, unexpectedly bouncing into the air during a planned high-speed taxi run. He reported that the aircraft could fly no higher than five feet off the ground. Flight could only be sustained by maintaining a precise angle of attack, but Theodore von Kármán solved the problem by making adjustments to the trailing edges of the elevons. Control of the aircraft was achieved through the use of a system of elevons and wingtip rudders. The elevons served in tailless type aircraft both as elevators and ailerons, while split flaps on the downward angled wingtips took the place of a conventional rudder; they were later straightened after that angle proved unnecessary during flight testing.
The flight test programme continued with Moye W Stephens, Northrop test pilot and secretary to the Northrop Corporation, serving as a test pilot. The early tests showed the N-1M to be satisfactory in stability and control, but overweight and underpowered. The aircraft's two 65-hp Lycoming 0-145 four-cylinder engines (buried in the wing to reduce drag) were replaced by two 120-hp six-cylinder 6AC264F2 air-cooled Franklin engines. By November 1941, after having made some 28 flights, Stephens reported that when attempting to move the N-1M about its vertical axis, the aircraft had a tendency to "Dutch roll." The oscillations proved to be manageable when adjustments were made to the aircraft's wing configuration.
The N-1M proved to be basically sound, paving the way for Northrop's later and much larger Northrop YB-35 and YB-49 aircraft. The -1M was then donated to the US Army Air Forces in 1945 and placed in the storage collection of the National Air Museum the following year. It sat there for nearly 30 years but was finally brought back to static, non-flying status, in its final flight configuration, after several years of painstaking restoration during the 1980s. It is now on public display at the National Air and Space Museum's Steven F Udvar-Hazy Center (above).
The aircraft is tiny (5.46m long, 11.8m wide, 1.5m high and 1.77 tonnes in weight). That's in stark contrast another Northrop aircraft, the later WWII-era P-61C Black Widow night fighter which can be partially seen, towering over the rear of the -1M.
What you're looking at here is the Rolls Royce Camargue, very much the Rolls Royce that time forgot. What can you even say about it? It's one of the most iconic automotive failures in history, and certainly a car that Rolls Royce fans are always very quick to wince at when I mention it at RREC conventions.
So where did this curious car come from? To truly understand this mighty machine you need to go back to 1969, where a massive change in the image and style of the world was starting to hold sway. In the world of autos, the curvature of the 1950's and early 60's was giving way to the angles of the 1970's, the decade that gave us the 'Wedge' sportsers and boxy saloon cars.
Rolls Royce, who at this point were building three cars, the Phantom VI, the Silver Shadow, and the Silver Shadow Two-Door Saloon (later to be known as the Corniche), were looking for a new design that would drastically alter its image from that of the Shadow. Originally, the intention was to use their new brainchild to replace the Two-Door Saloon, but due to financial difficulty within the Rolls Royce company, later followed by bankruptcy after the RB211 Jet Engine project, the company chose instead to save costs and rebrand it as the Corniche instead.
For their new car, Rolls Royce chose not to have it designed in-house like previous models, but went for the first time to Pininfarina of Italy. Throughout the remainder of 1969 the company toyed with many sketches, until in 1970 a final design was chosen and given the go by the Rolls Royce management, with the intention for a launch in either late 1972 or early 1973. Within the company, the project was dubbed "Delta", but was later changed to DY20, with ‘D’ signifying Delta, ‘Y’ signifying it was based on the SY (Silver Shadow) platform, and '20' shortened from 120 which was the car’s wheelbase of 120 inches.
But as mentioned, following the amount of money poured into the new Rolls Royce RB211 Jet Engine Project for the Lockheed Tristar, the company was bankrupt as of the 4th February 1971. The result was that the Motor Car Division, whose future now rested in the hands of the Official Receiver, had to look closely at all aspects of the business. This led to the splitting of the Rolls Royce company, with Rolls Royce Motors Ltd. being founded and placed under the ownership of Vickers, whilst the bankrupt Rolls Royce Ltd. was nationalised.
During this turbulent period, the DY20 project was closely scrutinised and the Receiver gave the go-ahead to commence the project, but following a critical review of the engineering specification for the car, a decision was taken to delay the launch date until 1975.
With development continuing, HJ Mulliner Park Ward, who already built the bodies for the Corniche, were chosen to manufacture the bodies of the DY20 project. In the summer of 1972, the first prototype D1 was released and tested heavily to maintain the standard of reliable excellence that Rolls Royce had been known for. At first the car's initial reception was warm, with people noting that it looked far more futuristic than the Shadow on which it was heavily based. Aside from sharing the same running gear, platform, Rolls Royce V8 engine and a majority of the internal features as the Shadow, the car was endearing in that it was fitted with a new and highly sophisticated bi-level automatic air conditioning system that at that time was the very first car in the world to have such a unit fitted. It was declared that this feature alone was more expensive than a British Leyland Mini! Another change was an instrument board, which many commented wouldn't have looked out of place on the flight deck of a Boeing 747!
Throughout 1972 and 73 more prototypes continued to be released and tested, with Rolls Royce giving paramount assistance to HJ Mulliner Park Ward's staff as they rigorously put these cars together. On the 18 January 1973 the body of the first production prototype, assigned D3, was attached to the front and rear sub frame assemblies on the normal Silver Shadow production line with maximum security in place and, following the production line assembly, the car was delivered to the experimental department to begin a period of intensive development work.
From May 1973 and all through 1974 production increased but still subject to extreme security. The production sequence was shared between MPW and Crewe. Once the body had been produced in the London factory and despatched to Crewe it was ‘finished painted’, attached to the front and rear sub frames and sent in a part built state back to MPW for all trim, general finishing and testing to take place at Hythe Road.
In January 1975, the car was officially launched in Catania, Sicily, and christened the name Camargue, an area situated in the delta of the River Rhône in France. Following a very successful press launch, the car was unveiled to the world on 5 March 1975 and the price quoted was £29,250, which made it the most expensive production car in the world ever at that time. Today, this figure translates out to £272,000. To put the price in perspective with other Rolls-Royce models at the time the Corniche saloon car cost £19,013 and the “Flagship of the Fleet” Phantom VI only cost £21,352!
The car was launched in the United States a year later after delays in fitting the cars with US Specification running gear meant that production didn't begin until August 1975. The cost of these cars in the US was $147,000, which today is about $588,000.
So, after a turbulent development mired in bankruptcy, a complicated building strategy and a delayed launch in America, did Rolls Royce's gamble with an audaciously designed car pay off?
Not in the slightest!
Purists recoiled at the sight of the angular corners and straight lines, with its big round headlights and chunky panels that made it look less like a Rolls Royce and more like a Lincoln Continental. They argued that for much, much less, owners could buy a Corniche or a Shadow which looked twice as good and performed just as well. This was then added to by the fuel crisis of the late 1970's, upon which that 6.75L Rolls Royce V8 soaking up petrol at a gallon every 15 miles looked deeply undesirable.
In all, only 531 of these cars were ever produced during its 11 year lifetime, but with a few variations. In 1985 a specialist hunting car called the Sbarro was reengineered for an Arabian aristocrat, whilst in 1979 two Camargues were used as testbeds for developments that would later find their way into the Silver Spirit/Spur range, including headlights and other features. In 1985 a single Bentley Camargue was also built, identical except for the changed badge and Grille, although many aftermarket conversions are known to exist. The last two cars rolled off the production line on Christmas Eve 1986 bound for Japan, at a price of £83,000.
Today, the Rolls Royce Camargue is a very, very rare car, and you would be hard pressed to find them routinely. In the United States a few continue to roam the countryside, with around 200 of the cars being exported there. Reception of these cars sadly continues to be very critical, with the car often topping people's lists for worst car ever made or ugliest car ever made. Although James May is one of a few people who defend this car, dubbing it "like that pug-faced but well-dressed bloke down the pub", for the most part all people can do is laugh at this car, laugh for the fact that it didn't sell, didn't look good and went through so much trouble to design and build that it was just a rushed embarrassment for the Rolls Royce company.
The reputation of these cars is so bad that in spite of its rarity, owners can't even give these things away, with most that I've seen going for as little as £20,000. But a word of advice, stop laughing, and buy their car! £20,000 for a two-door luxury saloon, a pedigree Rolls Royce, and one that once held the distinction of being the world's most expensive production car, you not only get this car for the cost of an equivalent Ford or Vauxhall, but you also make a saving on the original price tag of £252,000, that's over a quarter of a million pounds!
Me personally, I absolutely adore these cars! Indeed they're not as pretty as other Rollers, but I consider this a car that you not only have to feel sorry for, considering the background troubles that trailed its development from the start, but one that you have to admire as well. I feel that it's a car that's stood the test of time, a bit of automotive history from the 1970's that shows how reckless and ambitious we were with our car construction, like the Aston Martin Lagonda, brash in the extreme, but lovable all the same.
In fact if I had £20,000 right now I'd gladly go out and buy one, not only because I'd be saving a fortune, but also because it's a very personable little car, the kind of car you can't take your eyes off of, the car you could really give a name and love forever.
I'd name mine Christie! :D
On 2 September 2005, 37109 tows 960201 (formed from class 310 vehicles) from Ramsgate to Ilford. This unit was used as a testbed for the class 395 traction equipment.
Also featured elsewhere, here is another chance to see 8620 with its nice line in badges, dummy Olympian radiator panel and pre-Olympian testbed ventilation grille.
Manchester, crossing over High Street, from Cannon Street into Church Street (all very pre-Metrolink), 24/04/1990.
The Japan Maritime Self-Defense Force (JMSDF)'s Mitsubishi USH-60K Seahawk (8901) testbed helicopter assigned to the Air Development Squadron 51 based at Atsugi Air Base is statically displayed at Naval Air Facility (NAF) Atsugi (NJA / RJTA), Japan, April 27, 2019, during the NAF Atsugi Spring Festival 2019.
"Clipper Ocean Spray". Former "Clipper Star of the Union",
Later to General Electric N747GE as an engine testbed.
Withdrawn from use and stored at Victorville Southern California Logistics Airport, USA 25 January 2017 - 15 November 2018.
Preserved at Davis–Monthan Air Force Base, USA 15 November 2018, at the Pima Air and Space Museum.
This year I plan on attending Brickfair Virginia and like last year, will be participating in a military collaboration themed “eXperimental military”. This is the second set of models which I plan on displaying with many more in the works. From left to right is the Heinkel 178 then, the Gloster E.28 Pioneer. Both of these models represent a milestone in aviation and served as testbeds for the early jet engine. The E.28 was the RAFs test aircraft to test Frank Whittle’s new jet engine. Technically, the British designed and patented the jet first, however the Germans got their jet airborne making its maiden flight in 1939 betting the British to the first jet. The Germans saw the potential in the jet. Hitler wanted an aircraft far superior to anything the allies had and was willing to fund more experimental projects. The British government however, did not see the jet as a viable replacement to propeller driven aircraft which delayed the development of the first British jet fighter. Both countries did end up finally making a jet fighter. Germany made the Me-262 and the British eventually came up with the Meteor.
My models have functioning undercarriages and are scaled to mini figure scale. I plan on contributing more to the collab but thought that this would be a nice addition.
Airbus A380-861
MSN 004 [Engine Alliance testbed]
F-WWDD 'VNO' ['#A380' 'iflyA380.com' decals]
Airbus S.A.S.
Copyright © 2016 A380spotter. All rights reserved.
Reportedly broken up in Sept. 2014
----
en.wikipedia.org/wiki/Boeing_YAL-1
DSC_0472 Anx2 V2 900h Q90 0.5k-5k
The F-8 Digital Fly-By-Wire flight research project validated the principal concepts of all-electric flight control systems now used on nearly all modern high-performance aircraft and on military and civilian transports. The first flight of the 13-year project was on May 25, 1972, with research pilot Gary E. Krier at the controls of a modified F-8C "Crusader" that served as the testbed for the fly-by-wire technologies. The project was a joint effort between the NASA Flight Research Center (now Armstrong Flight Research Center) and LaRC. It included a total of 211 flights. The last flight was December 16, 1985, with research pilot Ed Schneider at the controls. This technology was also honored in the Space Technology Hall of Fame.
This year I plan on attending Brickfair Virginia and like last year, will be participating in a military collaboration themed “eXperimental military”. This is the second set of models which I plan on displaying with many more in the works. From left to right is the Heinkel 178 then, the Gloster E.28 Pioneer. Both of these models represent a milestone in aviation and served as testbeds for the early jet engine. The E.28 was the RAFs test aircraft to test Frank Whittle’s new jet engine. Technically, the British designed and patented the jet first, however the Germans got their jet airborne making its maiden flight in 1939 betting the British to the first jet. The Germans saw the potential in the jet. Hitler wanted an aircraft far superior to anything the allies had and was willing to fund more experimental projects. The British government however, did not see the jet as a viable replacement to propeller driven aircraft which delayed the development of the first British jet fighter. Both countries did end up finally making a jet fighter. Germany made the Me-262 and the British eventually came up with the Meteor.
My models have functioning undercarriages and are scaled to mini figure scale. I plan on contributing more to the collab but thought that this would be a nice addition.
Honeywell's flight test 757 taxis out at Phoenix, AZ on March 6, 2013. This was the 5th 757 off the production line and was delivered to Eastern Airlines in February 1983 as N504EA.
Copyright
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