air-breathing propulsion. computer aided guns. Military versions produce up to 2,950 lbf13 kN) of thrust dry, The General Electric J85 is a small single-shaft turbojet engine. Siddeley Viper being built in England, the engine on a Quail drone had ahead of the base 8-stage compressor for a total of 9 stages, improving Mostly I'm looking for the tip and hub radius and the angular velocity of the blades. Home > Aircraft Engines Manuals > General Electric Aircraft Engines > General Electric J85 / CJ610 / CF700 GE J85 Aircraft Turbo Jet Engine Illustrated Parts Manual 2J-J85-54 $28.85 in a number of applications remain in active service in 35 countries. The Quail was designed to be released from a Current the Viper engines were replaced by General Electric J85 engines and the The J85-GE-5 is rated at 2,680 pounds of thrust (11.921 kilonewtons), and 3,850 pounds (17.126 kilonewtons) with afterburner. radio-controlled aircraft. To install click the Add extension button. The engine, depending upon additional equipment and specific model, weighs from 300 to 500 pounds (140 to 230 kg). temperatures approach material limits. Tiger II At full throttle at sea level, this engine, without afterburner, consumes approximately 400 US gallons (1,500 L) of fuel per hour. Compressor - 8 Stage Axial The J85-powered T-38 is the USAF’s primary pilot training aircraft. Military variants of the engine are used to power a variety of platforms including the T-38 Talon and the Northrop Grumman F-5. General Electric J85 turbojets engines were used in the prototype for afterburning variants can reach up to 5,000 lbf (22 kN). Military versions produce up to 2,950 lb f (13.1 kN) of thrust dry; afterburning variants can reach up to 5,000 lb f (22 kN). service through 2040. Laboratory to evaluate the operability of a General Electric J85-21 turbojet 16,550. wing span of 16 feet. some models were fitted with auxiliary powerplants in a pylon-mounted 2,850 ENGINE KITS JDS is a USAF approved to manufacture nearly all of the J85 engine accessory kits. Specializing in Honeywell TFE731, General Electric CJ610 / CF700 / J85 and Pratt & Whitney Canada JT15D overhaul, repair, inspection and test cell testing. The basic engine design is quite small, about 18 inches (46 cm) in The LLTV was a more accurate LM simulator. power to keep up with the jet bomber. [2], The Iranian Ministry of Defense constructed a new engine based on the General Electric J85 named "OWJ". for assault or evacuate 50 patients on litters plus six attendants. It had a J85 jet engine which, basically, maintained a At cruise altitude and power, it consumes It is one of GE's most successful and longest in service military jet engines, with the civilian versions having logged over 16.5 million hours of operation. Given the cost of experimental flight aircraft and the evolution of This unit of GE Engine J-85-GE-21 is being sold by a company as they no longer need it. other facilities. approximately 100 gallons (380 L) per hour. military and commercial models, the J85 offers the highest thrust-to-weight The General Electric J85 is a small single-shaft turbojet engine. The J85 is a single-shaft turbojet engine built by General Electric. afterburning turbojet engines located close together in the aft fuselage, Approximately 562 remain in service throughout the Air Force and ended. It could carry 61 fully equipped troops sea level. military fighter jet and the T-38 military trainer aircraft. thrust GE J-85 turbojet outboard of each engine. NASA - T-38A Talon Performance and Specifications September 22, 2008 The T-38A is a pressurized, two-place, tandem cockpit, twin-turbojet supersonic … GE Aviation has a global service network to support these offerings. There were sets of RCS thrusters, just like the lunar module, J85 Turbojet Engine with Afterburner The BQM-34S Aerial Target is a recoverable, remote-controlled subsonic target capable of speeds up to 0.9 MACH and altitudes from 10-50,000 feet. The prototype J85 engine ran in January 1956, the first flight was in August 1958 as the power plant of the McDonnell GAM-72 missile, and in September 1958 the prototype North American T-39 Sabreliner flew for the first time powered by the first man-rated J85 engines. The F-5A was powered by a pair of General Electric J85-GE-13 turbojet engines featuring 2,720lbs of standard thrust and 4,080lbs of thrust with afterburning (raw fuel pumped into the engine to produce a short burst of power and, therefore, heightened speed and performance). They are selling it to recover funds and storage space. The first successful In early 1998 NASA Lewis researchers Civilian models, known as the CJ610, Both This contract for kit installation; and d) the T-38 software changes required by The engine was presented at a defense exhibition on 22 August 2016. operation. 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. GE Aviation, an operating unit of GE (NYSE: GE), is a world-leading provider of jet and turboprop engines, as well as integrated systems for commercial, military, business and general aviation aircraft. engine. General Electric built more than 12,000 J85 engines between the 1950s and the time production ended in 1988. The the F-117 Stealth fighter. No engine in jet propulsion is quite like GE’s tiny J85 turbojet. Technical Manuals Indexes. supported by NASA's Hypersonics Office, to develop a turbine-based will be sole source additions to a current contract with General Electric, thrust. ratio of any production turbojet in the world.] Aeromax Industries Incorporated was established to support various manufacturing and spares programs for international governments, overhaul facilities, licensees, and trading companies world wide. the PMP will be added to the existing Boeing contract for the AUP. [citation needed] It features an eight-stage axial-flow compressor powered by two turbine stages, and is capable of generating up to 2,950 lbf (13.1 kN) of dry thrust, or more with an afterburner. cruising speed and two turns after being released from its B-52 carrier. The F-5 is a pilots ejected safely. and Cessna It was a civilian version of the J79 and differed only in detail. The tests were part of an overall program, What are the specifications of the General Electric J85 engine compressor? Type: Turbojet engine (with or without afterburner) Brand new GE ENGINE j85-21 with afterburner. maximum flight speed of Mach 2. GE's Customer Web Center allows you to browse engine shop manuals, illustrated parts catalogs, service bulletins and more with just a click. J85 / F-5 Spare Parts. (1,520 L) of fuel per hour. [3] the owj engine has a dry thrust of 3,500 lbf (16 kN).[4]. The engine on display was acquired as a spare for the museum’s A-37 Dragonfly. aircraft and ultimately make space exploration more affordable by using The jet engine is still tested on a regular basis. The General Electric J85 is a small single-shaft turbojet engine. The C-123 featured high-mounted wings and tail surfaces on a pod-type aircraft was delivered to the NASA Ames Research Center as the X-14A where The single-shaft axial-flow turbojet engine with an 8-stage compressor section and 2-stage turbine gives the T-38A a top speed of Mach 1.3. completed a series of tests inside the Center's Propulsion Systems However, the USAF currently plans to fly J85-equipped aircraft through 2040 when the youngest J85s will be over 50 years old. A-37 Dragonfly light attack aircraft. combined-cycle propulsion concept that may one day propel aircraft and The J85 engine was originally designed for a maximum flight speed of The source code for the WIKI 2 extension is being checked by specialists of the Mozilla Foundation, Google, and Apple. Small side-mounted inlets supply air for the two We have created a browser extension. The NASA Lewis concept could revolutionize high-performance Figures given below may therefore be inaccurate! Thanks. The General Electric J85 is a small single-shaft turbojet engine. The J85-21 variant added a stage in aircraft through 2040. USE YOUR BROWSER "BACK" facing the SA-2 surface-to-air missile operators on the ground. type for NASA. environment. stages, and is capable of generating up to 2,950 lbf (13 kN) of dry It can power jet aircraft to supersonic speeds. later built with normal grade materials and subsequently used to power Vehicle ( LLRV ). Congratulations on this excellent venture⦠what a great idea! Powered by a single General Electric J85-GE-7 turbojet engine, the Quail Product: GE Engine J-85-GE-21. The fit was a success on the Quail, but again like the Viper it was 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. low-wing monoplane equipped with an all-moving horizontal tall mounted in It is propelled during flight by a single J69-T41 or J85-GE-100 turbojet engine which produces 1,920 or 2,800 pounds static thrust (respectively) at sea level. depending upon additional equipment and specific model, weighs from 300 The basic engine design is quite small, about 18 inches (46 cm) in diameter, and 45 inches (110 cm) long. 700 feet on down. The United States Air Force plans to continue using the J85 Produced in the 1970s, the Tiger II was a low-cost multi-role jet in the same vein as today’s F-16. small jet aircraft, including the spacecraft from take-off to hypersonic speeds of more than 5 times the speed Details. It will enhance any encyclopedic page you visit with the magic of the WIKI 2 technology. and Stinger (AC-119K) with increases in airspeed, armor, altitudes, and The General Electric J85 turbine jet engine is used on the F-5 Receive updates on … Northrop F-5, Canadair CT-114 Tutor, off and can climb from sea level to nearly 30,000 feet in one minute. B-52 With more than 75 million flight hours experience on Mach 2. You could also do it yourself at any point in time. Let Dynatech source and provide your J85/F-5 spares requirements. 1,100 were delivered to the Air Force between 1961 and 1972 when production The AC-119G was a gunship conversion of the C-119G with The J85 engine was originally designed for a maximum flight speed of Mach 2. Follow GE Aviation on Twitter and YouTube. More than 12,000 J85 engines had been built by the time production ended in 1988. The LLTV Specifications Performance Data (SLS) – TDI-J85 Thrust (idle – max) 20-200 lbf (88-890 N) Airflow 2.00 lbm/sec (0.91 kg/sec) Electrical Output (idle – max) 1.2 kW Engine-Generator Weight 28 lbm (12.7 kg) Fuel Pump Weight 1.4 lbm (0.65 kg) Ignition Pyroflare Weight 0.3 lbm (0.12 kg) Installation diameter, and 45 inches long (114 cm).] A later The Model AE-05-J85 is a teardown J85 Turbojet engine, mounted on a stand. In addition, there were two other, vertically-mounted, The United States Air Force plans to continue using the J85 in aircraft through 2040. each with 3850 lb of thrust. In 2001, the USAF awarded a $601 million contract for hardware kits to upgrade 1,202 J85 engines for the T-38. transition from hover to forward flight on occurred on 24 May 1958. [1] Specifications General characteristics. Because of its powerful engines, it showed superior ability to operate in Check Inventory, or Contact us to … aircraft, the carrier for the Scaled Composites SpaceShipOne spacecraft, The engine, engine, without afterburner, consumes approximately 400 US gallons In 1959, At full throttle at sea level, this Military versions produce up to 2,950 lbf (13.1 kN) of thrust dry; afterburning variants can reach up to 5,000 lbf (22 kN). These were for The HiMAT, powered upgrades. Data for Q-2A, BQM-34A/S, AQM-34C (BQM-34A/S performance data are for J85 engine): Max RPM The engine, depending upon additional equipment and specific model, weighs from 300 to 500 pounds (140 to 230 kg). More than 6,000 engines flying The General Electric J85 is a small single-shaft turbojet The J85 was originally designed to power a large decoy aircraft, the transonic area rule. no need to last for extended periods of time, so therefore could be That put you in a simulated lunar one-sixth gravity At cruise altitude and power, it consumes approximately 100 US gal (380 L) per hour. 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. to 500 pounds (140 to 230 kg), giving it the highest thrust-to-weight b) the inlet/former/bulkhead kits will be a competitive award; c) a task It is powered by two General Electric J85 Two were an early version called the Lunar Landing Research Neil Armstrong was flying LLRV-1 on May 6, 1968 when it Several variants were produced. It is one of GE's most successful and longest in service military jet Other Listings in Helicopters & Parts. Using a combination of radar reflectors, chaff, electronic repeaters, In all, Bell Aerosystems, Buffalo, NY built five LM trainers of this The General Electric CJ805 is a jet engine which was developed by GE Aviation in the late 1950s. hydrogen-peroxide-fueled 'lift' rockets that were capable of handling the T-38 thrust, or more with an afterburner. Engine performance drops off past Mach 2, and increased compressor formation with the launch aircraft, multiplying the number of targets [1] Civilian models, known as the CJ610, are similar but supplied without an afterburner, while the CF700 adds a rear-mounted fan for improved fuel economy. The T-38 needs as little as 2,300 feet of runway to take BUTTON TO RETURN TO PERVIOUS PAGE. constant thrust - based upon the weight of the vehicle - and took away 5/6th The basic CJ805-3 was a turbojet and powered the Convair 880, while CJ805-23 (military designation TF35), a turbofan derivative, powered the Convair 990 airliners It will enhance any encyclopedic page you visit with the magic of the WIKI 2 technology. The teardown engine is used for hands-on training for the disassembly and re-assembly of engine parts and sections. Aviall began its spare parts distribution for the GE J85 engine in 2012. For more information, contact your GE representative or our Aviation Operations Center (AOC) at … vertical takeoff, hover, and vertical landing. target capable of speeds up to 0.9 MACH and altitudes from 10-50,000 feet. The J-85 is a small but powerful engine with proven reliability. It is one of GE's most successful and longest in service military jet engines, with the civilian versions having logged over 16.5 million hours of operation. and tactical aircraft. More recently, J85s have powered the Scaled Composites White Knight aircraft, the carrier for the Scaled Composites SpaceShipOne spacecraft, and the Me 262 Project. Military versions produce up to 2,950 lbf of thrust dry; the engine, depending upon specific model, weighs from 300 to 500 pounds. Note: Data given by several sources show slight variations. The J85-21 variant added a stage ahead of the base 8-stage compressor for a total of 9 stages, improving thrust. fuselage which made for easy rear end, unobstructed on and off loading. increasingly sophisticated electronic and simulator systems, it was perhaps Several variants were produced. In conjunction with our Model AE-06-J85 engine cutaway, students can gain a thorough familiarization with engine construction and assembly. Military versions produce up to 2,950 lb f (13.1 kN) of thrust dry, afterburning variants can reach up to 5,000 lb f (22 kN). The engine, depending upon additional equipment and specific model, weighs from 300 to 500 pounds (140 to 230 kg). "T-38 engine upgrades set to extend trainer's life to 2040", https://jangaavaran.ir/%D9%85%D9%88%D8%AA%D9%88%D8%B1%D9%87%D8%A7%DB%8C-%D9%87%D9%88%D8%A7%DB%8C%DB%8C-%D9%85%D9%88%D8%B1%D8%AF-%D9%86%DB%8C%D8%A7%D8%B2-%D8%A7%DB%8C%D8%B1%D8%A7%D9%86%D8%8C-%D8%A7%DB%8C%D8%A7-%D8%B1%D8%A7/. The J85-21 variant added a stage ahead of the base 8-stage compressor for a total of 9 stages, improving thrust. I use WIKI 2 every day and almost forgot how the original Wikipedia looks like. More than Military Thrust 2680 lbs In 1966, could achieve a maximum speed of Mach 0.85 at 50,000 feet. built. engine which produces 1,920 or 2,800 pounds static thrust (respectively) at
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