The General Electric J85 is a small single-shaft turbojet engine. The G.91Y was an increased performance version of the Fiat G.91 funded by the Italian government. Military versions produce up to 2,950 lbf(13.1 kN) of thrust dry, afterburningvariants can reach up to 5,000 lbf(22 kN). [2], The Iranian Ministry of Defense constructed a new engine based on the General Electric J85 named "OWJ". No engine in jet propulsion is quite like GE’s tiny J85 turbojet. SK 60C: Two-seat ground attack/reconnaissance version for the Swedish Air Force with extended camera nose. The engine, depending upon additional equipment and specific model, weighs from 300 to 500 pounds (140 to 230 kg). Based largely on earlier Fiat G.91 fighters, the G.91 YS was a complete redesign but kept the basic shape of the G.91 series. It was developed in two versions. In 1959, its Viper engines were replaced with General Electric J85 engines. The Quail was designed to be released from a B-52 Stratofortress in-flight and fly for long distances in formation with the launch aircraft, multiplying the number of targets facing the SA-2 surface-to-air missile operators on the ground. The engine, depending upon additional equipment and specific model, weighs from 300 to 500 pounds . Cessna, therefore, doubled the engine power by replacing the two Continental J-69 engines with General Electric J85-J2/5 turbojet engines with 2,400 lbf (11 kN) thrust each. During the development of the P.1127, Hawker test pilots Bill Bedford and Hugh Merewether visited NASA Ames to fly the X-14 and acquaint themselves with jet V/STOL aircraft h… Based on the G.91T two-seat trainer variant the single Bristol Orpheus turbojet engine of this aircraft was replaced with two afterburning General Electric J85 turbojets which increased thrust by 60% over the single-engined variant. The General Electric CJ805 is a jet engine which was developed by GE Aviation in the late 1950s. 2 x … The basic engine design is quite small, about 18 inches (46 cm) in diameter, and 45 inches (110 cm) long. The General Electric J85 is a small single-shaft turbojet engine. That year the aircraft was also delivered to the NASA Ames Research Center as the X-14A. This mission demanded a small engine that could nevertheless provide enough power to keep up with the jet bomber. J85 is historically more important -- the others came from it -- but CF610 is much more common. The biggest difference between the two types was the conversion from a single-engine to two General Electric … The engine, depending upon additional equipment and specific model, … 2 х General Electric J85-GE-17B Engine. Lytron J85 / CJ610 Engine Bleed Valve; MRC Annular Ball Bearing (J85 Engine) Trans Pacific Travel F-5 / T-38 Starter Coupler Duct Assy; Bendix Ignition Exciter for GE J85 Engine; General Electric F110 Engine Nozzle Segment; Lockheed C-130 Latch Assembly; T38 / F5 Hydraulic Pump; CF6-80 Engine Starter Valve; Products List. Speed of destruction. General Electric J85 je malý jednohřídelový proudový motor.Vojenské verze poskytují "na sucho" tah 13,1 kN, zatímco varianty s přídavným spalováním dosahují až 22 kN. The first YAT-37D flew in October 1964, followed a year later by the second prototype. 12 x m/56D rockets Setup 3. Military versions produce up to 2,950 lbf of thrust dry; afterburning variants can reach up to 5,000 lbf . The General Electric J85 is a small single-shaft turbojet engine. At cruise altitude and power, it consumes approximately 100 US gal (380 L) per hour. The General Electric J85 is a small single-shaft turbojet engine. The fit was a success on the Quail, but again like the Viper it was later built with normal grade materials and subsequently used to power small jet aircraft, including the Northrop T-38 Talon, Northrop F-5, Canadair CT-114 Tutor, and Cessna A-37 Dragonfly light attack aircraft. The T-38A is powered by two General Electric J85-GE-5 turbojet engines. The G.91 YS is a rank VI Italian jet fighter with a battle rating of 9.7 (AB/RB) and 9.3 (SB). The General Electric J85is a small single-shaft turbojetengine. j85 in propulsion systems laboratory psl tank 3 - tf34 engine in middle of floor - nara - 17499121.jpg 4,853 × 6,171; 22.76 mb J85-13 MOD III PLUG NOZZLE INSTALLATION - NARA - 17426797.jpg 6,217 × 4,846; 25.45 MB Powerplant: 2 × General Electric J85-5A afterburning turbojet engines, 2,050 lbf (9.1 kN) thrust each dry, 2,900 lbf (12,899.84 N) with afterburner (J85-5R after PMP modification) [71] Performance More recently, J85s have powered the Scaled Composites White Knight aircraft, the carrier for the Scaled Composites SpaceShipOne spacecraft, and the Me 262 Project. The G.91 YS is a multi-role fighter which first debuted in 1966. The engine, depending upon additional equipment and specific model, weighs from 300 to 500 pounds (140 to 230 kg). Martin continued development of the P5M-3 under the designation P7M Submaster, introducing two General Electric J85 BLC gas generators, one in the rear of each outer engine nacelle. One new build prototype and 29 conversions from Sk 60A. The success of GE's J85 fighter engine led to the development of the CJ610 for commercial use. Saab 105XT : Export demonstrator; improved version of the SK 60B, re-engined with 12.85 kW (2,850 lbf) General Electric J85 turbojets. The General Electric J85 is a small single-shaft turbojet engine. Military versions produce up to 2,950 lbf13 kN) of thrust dry, afterburning variants can reach up to 5,000 lbf (22 kN). Like the similar Armstrong Siddeley Viper being built in England, the engine on a Quail drone had no need to last for extended periods of time, so therefore could be built of low-quality materials. 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