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Turbomeca Marboré
The Turbomeca Marboré is a small turbojet engine that was produced by Turbomeca from the 1950s into the 1970s. The most popular uses of this engine were in the Fouga CM.170 Magister and the Morane-Saulnier MS.760 Paris. It was also licensed for production in the United States as the Teledyne CAE J69. In Spain the Turbomeca model Marboré II was manufactured by ENMASA under license with the name Marboré M21. The original Marboré, as well as Marboré III, IV, and V were not produced in significant numbers. A typical weight for this series of engines is . Fuel consumption is on the Marboré VI at , as compared to on Marboré II engines (same altitude), as well as an increase of fuel consumption of 27% and a decrease in cruise range capabilities.CM-170 Flight Tests, Airplane Cruise Performance Charts, and Aircraft Flight Manuals Variants ;Marboré I:Prototypes and test examples ;Marboré II:The first major production version was the Marboré II, which had a maximum thrust o ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
WikiProject Aircraft
A WikiProject, or Wikiproject, is an affinity group for contributors with shared goals within the Wikimedia movement. WikiProjects are prevalent within the largest wiki, Wikipedia, and exist to varying degrees within Wikimedia project, sibling projects such as Wiktionary, Wikiquote, Wikidata, and Wikisource. They also exist in different languages, and translation of articles is a form of their collaboration. During the COVID-19 pandemic, CBS News noted the role of Wikipedia's WikiProject Medicine in maintaining the accuracy of articles related to the disease. Another WikiProject that has drawn attention is WikiProject Women Scientists, which was profiled by ''Smithsonian Magazine, Smithsonian'' for its efforts to improve coverage of women scientists which the profile noted had "helped increase the number of female scientists on Wikipedia from around 1,600 to over 5,000". On Wikipedia Some Wikipedia WikiProjects are substantial enough to engage in cooperative activities with outsi ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
List Of Aircraft Engines
This is an alphabetical list of aircraft engines by manufacturer. 0–9 2si *2si 215 *2si 230 *Cuyuna 430, 2si 430 *2si 460 *2si 500 *2si 540 *2si 690 3W ''Source: RMV'' *3W 106iB2 *3W-110 *3W-112 *3W-170 *3W-210 *3W-220 A Abadal (Francisco Serramalera Abadal) *Abadal Y-12 350/400 hp ABC ''Source: Lumsden.'' * ABC 8 hp * ABC 30 hp V-4 * ABC 45 hp V-6 * ABC 60 hp V-8 * ABC 85 hp V-6 * ABC 100 hp V-8 * ABC 115 hp * ABC 170 hp V-12 * ABC 225 hp V-16 *ABC Dragonfly *ABC Gadfly *ABC Gnat *ABC Hornet *ABC Mosquito *ABC Scorpion *ABC Wasp *ABC type 10 APU *ABC type 11 APU ABECO ''Source: RMV'' *ABECO GEM Aberg ''Source: RMV'' *Type Sklenar ABLE ''Source: RMV'', Able Experimental Aircraft Engine Co. (Able Experimental Aircraft Engine Co., Altimizer, Hoverhawk (US)) *ABLE 2275 *ABLE 2500 *ABLE VW x 2 Geared Drive Accurate Automation Corp *Accurate Automation AT-1500 *Accurate Automation AT-1700 Ace (Ace Amer ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Stargate YT-33
The Stargate YT-33 is an American homebuilt aircraft that was designed and intended to be produced by Stargate, Inc., of McMinnville, Oregon. It was introduced in 1994. The aircraft is a 2/3 scale replica of the Lockheed T-33 jet trainer. Listed as "under development" in 1998, the YT-33 was planned to be supplied as a kit for amateur construction, but it is unlikely any kits were ever shipped. Design and development The YT-33 features a cantilever low wing, a two-seats-in-tandem enclosed cockpit under a bubble canopy, retractable tricycle landing gear, and a single jet engine. The aircraft is made from composite material. Its span wing has a wing area of . The prototype uses a thrust Turbomeca Marboré IIC jet powerplant. The aircraft has a typical empty weight of and a gross weight of , giving a useful load of . The aircraft has a fuel capacity of or of Jet-A. The ISA standard temperature, sea-level, no-wind, take-off distance is , and the landing roll is . The ma ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
SNCASO Trident
The SNCASO SO.9000 Trident is a French jet and rocket powered interceptor aircraft built by aircraft manufacturer SNCASO during the 1950s. As part of a wider effort to re-build French military power during the late 1940s and to furnish France with advanced, new domestically produced designs, a request for a supersonic-capable point-defence interceptor aircraft to equip the French Air Force was issued to SNCASO. In response, the firm designed the mixed-propulsion Trident, powered by a single SEPR rocket engine, which was augmented by wingtip-mounted turbojet engines, and the Air Force ordered two prototypes. The two SO.9000 Trident Is demonstrated the feasibility of the design concept despite the loss of one aircraft during flight testing and the Air Force ordered a batch of three prototype SO.9050 Trident II fighters in 1954, and a batch of six pre-production aircraft in 1956 to further develop the aircraft so it could serve as a short-range interceptor. Only six of these nine ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
SNCASO Deltaviex
The SNCASO Deltaviex or SNCASO-ONERA Deltaviex was a small French experimental jet aircraft, first flown 30 April 1954 and distinguished by highly swept, small span wings. It was designed to explore the possibility of controlling roll and yaw with fine jets of air bled from the engine's compressor. Design and development The Deltaviex, its name derived from the Delta VX design of Alliet at ONERA and built by SNCASO at Courbevoie, was intended to explore lateral control by blown flaps instead of ailerons. Despite its name it did not have a delta wing but wings which were strongly swept and straight tapered to pointed tips. The leading edge sweep was 70°, that of the trailing edge about 40° and the thickness to chord ratio less than 6%. The wing trailing edges carried flaps from the wing roots almost to the tips and these were blown with air bled from the centrifugal compressor of the Deltaviex's Turbomeca Marboré gas turbine engine, exiting the flap trailing edges via ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Nord Aviation CT20
The Nord Aviation CT20 was a French turbojet-powered radio-controlled target drone introduced in 1957. Developed from the Arsenal / S.F.E.C.M.A.S. T.5.510, the CT.20 was built by Nord Aviation and powered by a Turbomeca Marboré II engine, providing a top speed of and a flying time of 55 to 60 minutes. It has been noted for its similarity to the Ryan Firebee. The unmanned drone was used in the development of air-to-air missiles following the Second World War. After the startup of the turbojet, the target drone is placed on a ramp and launched using two rockets. During its flight, the drone is controlled via radio signals from the ground. As it is made of light material, it is buoyant in water and can be recovered if it is forced to land on water. Variants ;Arsenal T.5.510 / S.F.E.C.M.A.S. T.5.510 : Original design work and development of the CT.20 carried out before SFECMAS was absorbed by SNCAN. ;CT20 :Radio controlled target ;R20 :Battlefield reconnaissance drone. 62 built f ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Miles Student
The Miles M.100 Student was built as a lightweight trainer as a private venture by F.G. and George Miles with development started in 1953. Although not specifically a Miles product, it was promoted as a British Royal Air Force trainer but failed to enter production. Design and development Building on the company's experience with the M.77 "Sparrowjet", the M.100 Student was a two-seat, side-by-side, all-metal jet trainer. The M.100 prototype was powered by a 400 kgf (882 lb) thrust Turbomeca Marbore turbojet and flew for the first time on 15 May 1957. Miles had hoped to secure an RAF order, but the contract went to the Jet Provost. The Student was proposed for several training programmes, but without success. ''G-APLK'', the sole aircraft, was allocated ''XS941'' when developed in the Mark 2 version as a prospective Counter-insurgency type. It was tested by the Royal Air Force but was not accepted and therefore did not go into production. The M.100 Student 2, re-registered ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Hispano HA-200
The Hispano HA-200 Saeta (English: ''Arrow'') is a twin-seat jet advanced trainer designed and produced by Spanish aircraft manufacturer Hispano Aviación. It has the distinction of being the first Spanish aircraft to harness jet propulsion. The German aircraft designer Willy Messerschmitt can be largely credited for his role in designing the HA-200, which reused a substantial portion of the earlier piston-powered HA-100 Triana. On 12 August 1955, the first prototype conducted its maiden flight. It was not until 1962 that the first production aircraft performed its first flight. That same year, deliveries of the trainer aircraft commenced to the Spanish Air Force. It would be used in this capacity by the service for multiple decades. The HA-200 was later further developed into the Hispano Aviación Ha-220 "Super Saeta", which functioned as a dedicated ground attack platform, armed with rockets, bombs, and other munitions. The HA-220 served in the Spanish Air Force througho ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Bölkow Bo 46
The Bölkow Bo 46 was a West German experimental aircraft, experimental helicopter built to test the Derschmidt rotor system that aimed to allow much higher speeds than traditional helicopter designs. Wind tunnel testing showed promise, but the Bo 46 demonstrated a number of problems and added complexity that led to the concept being abandoned. The Bo 46 was one of a number of new designs exploring high-speed helicopter flight that were built in the early 1960s. Background Helicopter rotors operate in a much more challenging environment than a normal aircraft propeller. To start with, helicopters normally use the main rotor both for lift and manoeuvrability, whereas fixed-wing aircraft normally use separate surfaces for these tasks. Pitch and yaw are operated by changing the lift on different sides of the rotor, using a system of bell cranks to adjust the blades to different angle of attack, angles of attack as they rotate. To roll to the right, the blades are adjusted so there i ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
