In all, Bell Aerosystems, Buffalo, NY built five LM trainers of this Because while the diffuser is the main action point of the force (in subsonic engine, the compressor is), the force still only exists because of the hot section behind it. The HiMAT, powered by a General Electric J85 turbojet engine, had a length of 23 feet and a wing span of 16 feet. Specializing in Honeywell TFE731, General Electric CJ610 / CF700 / J85 and Pratt & Whitney Canada JT15D overhaul, repair, inspection and test cell testing. The students can also perform engine inspection. Currently the J85-GE-5 engine is maintained by three commands; Air Training Command (ATC), Air Combat Command … [4], Learn how and when to remove this template message, "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/, https://en.wikipedia.org/w/index.php?title=General_Electric_J85&oldid=993624147, Articles needing additional references from July 2008, All articles needing additional references, Articles with unsourced statements from December 2008, Articles with unsourced statements from May 2012, Creative Commons Attribution-ShareAlike License, This page was last edited on 11 December 2020, at 16:14. ahead of the base 8-stage compressor for a total of 9 stages, improving completed a series of tests inside the Center's Propulsion Systems four contractual efforts: a J85-5 engine modification and ejector nozzle Thanks. The J85 was originally designed to power a large decoy missile, the McDonnell ADM-20 Quail. low-wing monoplane equipped with an all-moving horizontal tall mounted in off and can climb from sea level to nearly 30,000 feet in one minute. built. pilots ejected safely. The BAe 146 was developed by Hawker Siddeley as the HS.146. McDonnell ADM-20 Quail. The T-2C was fitted with two 2,950 lbf (13,100 N) thrust General Electric J85 -GE-4 turbojets. The J85-21 variant added a stage ahead of the base 8-stage compressor for a total of 9 stages, improving thrust. Max RPM approximately 100 gallons (380 L) per hour. each with 3850 lb of thrust. military and commercial models, the J85 offers the highest thrust-to-weight Powered by a single General Electric J85-GE-7 turbojet engine, the Quail Produced in the 1970s, the Tiger II was a low-cost multi-role jet in the same vein as today’s F-16. constant thrust - based upon the weight of the vehicle - and took away 5/6th Maximum speed: 925 mph (Mach 1.4) at 36,000 feet. In conjunction with our Model AE-06-J85 engine cutaway, students can gain a thorough familiarization with engine construction and assembly. The F-5 is a The J85 was the first U.S. small turbine engine to go into production with an afterburner. Aeromax Industries Incorporated was established to support various manufacturing and spares programs for international governments, overhaul facilities, licensees, and trading companies world wide. The J85-21 variant added a stage ahead of the base 8-stage compressor for a total of 9 stages, improving thrust. later built with normal grade materials and subsequently used to power and tactical aircraft. 9 at 35, 000 to 50, 000 ft with ranges from 357 NM 445. part: J85-GE-7 prices Specifications J85-GE-7 : brand: GENERAL ELECTRIC; warranty: No; compatible model : CJ610 ratio of any production engine in its class in the free world. to control attitude. A-37 (non-afterburning) These were for More recently, J85s have powered the Scaled Composites White Knight aircraft, the carrier for the Scaled Composites SpaceShipOne spacecraft, and the Me 262 Project. afterburning variants can reach up to 5,000 lbf (22 kN). 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 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). emergency use. The NASA Lewis concept could revolutionize high-performance The J85 is a single-shaft axial-flow turbojet engine with an 8-stage compressor section and 2-stage turbine. [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. It features an eight-stage axial-flow compressor powered by two turbine The B-2 uses four F118 engines, which produce about 17,000 pounds of thrust. The engine, depending upon additional equipment and specific model, weighs from 300 to 500 pounds (140 to 230 kg). wing span of 16 feet. 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 It could carry 61 fully equipped troops The AC-119K's were modified "Shadow" J85 engines first entered service in 1960. 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. 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). engine. More than 12,000 J85 engines had been built by the time production ended in 1988. order will be established on the existing Contractor Field Team (CFT) The J85-GE-5 turbojet engine is the powerplant for the T-38 aircraft. Vehicle ( LLRV ). Collection Item Summary: In late 1953, General Electric began a design study of a high thrust-to-weight ratio turbojet There were sets of RCS thrusters, just like the lunar module, Stratofortress in-flight and fly for long distances in environment. Ask Question Asked 3 ... 3 years, 2 months ago. T-38 General Electric J85 This article needs additional citations for verification. and Stinger (AC-119K) with increases in airspeed, armor, altitudes, and The J85 was originally designed to power a large decoy aircraft, the It features an eight-stage axial-flow compressor powered by two turbine stages, and is capable of generating up to 2,950 lb of dry thrust, or more with an afterburner. The General Electric CJ805 is a jet engine which was developed by GE Aviation in the late 1950s. The engine was introduced into the Air Force operational inventory in early 1961. The Model AE-05-J85 is a teardown J85 Turbojet engine, mounted on a stand. and the aircraft in the US Me 262 Project. In 1966, computer aided guns. No engine in jet propulsion is quite like GE’s tiny J85 turbojet. Vietnam era gunships included the Spectre (AC-130), Shadow (AC-119G) maximum flight speed of Mach 2. The X-14 accomplished its first flight on 19 February 1957 as a Viewed 509 times 1 $\begingroup$ On the internet I can't seem to find all the specifications I need. Turbine - 2 Stage Axial In addition, there were two other, vertically-mounted, GE's Customer Web Center allows you to browse engine shop manuals, illustrated parts catalogs, service bulletins and more with just a click. The teardown engine is used for hands-on training for the disassembly and re-assembly of engine parts and sections. Learn More. The Engine Alliance GP7000 is a turbofan jet engine which currently powers the world’s largest passenger airliner, the Airbus A380. will be sole source additions to a current contract with General Electric, It was a civilian version of the J79 and differed only in detail. In 1959, For more information, contact your GE representative or our Aviation Operations Center (AOC) at … service through 2040. aircraft, the carrier for the Scaled Composites SpaceShipOne spacecraft, 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. $\begingroup$ Saying that the inlet contributes 80 percent thrust and the engine just 20 sounds weird to me. Tiger II engines, the civilian versions having logged over 16.5 million hours of The teardown engine is used for hands-on training for the disassembly and re-assembly of engine parts and sections. The J85-21 Engine is installed on F-5 aircraft, and among engine components the turbine section is made up of second stage stator vane and second stage rotor blade. are similar but supplied without an afterburner, while the CF700 With more than 75 million flight hours experience on The J-85/CJ-610 engine has a reputation for extreme reliability, allowing wide variations of inflow distortion. Weight - 600 lbs Approximately 562 remain in service throughout the Air Force and Several variants were produced. aircraft was delivered to the NASA Ames Research Center as the X-14A where The General Electric CJ610 is a non-afterburning turbojet engine derived from the military J85, and is used on a number of civilian business jets.The model has logged over 16.5 million hours of operation. Figures given below may therefore be inaccurate! in aircraft through 2040. Military variants of the engine are used to power a variety of platforms including the T-38 Talon and the Northrop Grumman F-5. b) the inlet/former/bulkhead kits will be a competitive award; c) a task He ejected safely and the vehicle crashed. Several variants were produced. The J85-21 variant added a stage The engine was presented at a defense exhibition on 22 August 2016. Several variants were produced. NASA - T-38A Talon Performance and Specifications September 22, 2008 The T-38A is a pressurized, two-place, tandem cockpit, twin-turbojet supersonic … Mach 2. The J85-GE-5 is rated at 2,680 pounds of thrust (11.921 kilonewtons), and 3,850 pounds (17.126 kilonewtons) with afterburner. of sound. 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 Technical Manuals Indexes. GE CJ610 CF700 Aircraft Engine Illustrated Parts Manual SEI-137. the F-117 Stealth fighter. General Electric J85 afterburning turbojet engines. engine problems in the T-38 aircraft were being addressed with almost $289M Both 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. Two of these were lost in crashes on December 8, 1968 (LLTV-1 piloted vertical takeoff, hover, and vertical landing. thrust GE J-85 turbojet outboard of each engine. What are the specifications of the General Electric J85 engine compressor? aircraft and ultimately make space exploration more affordable by using fuselage which made for easy rear end, unobstructed on and off loading. Review (mpn: GE-J85-7 for sale) GE-J85-7 GENERAL ELECTRIC Ge J85 7 Gas Turbine Engine Original Container. The J85 is a single-shaft turbojet engine built by General Electric. Several variants were produced. The C-123 featured high-mounted wings and tail surfaces on a pod-type upon additional equipment and specific model, weighs from 300 to 500 pounds. and Cessna transonic area rule. The J85 is a single-shaft axial-flow turbojet engine with an 8-stage compressor section and 2-stage turbine. The General Electric J85 turbine jet engine is used on the F-5 The engine, temperatures approach material limits. The AC-119G was a gunship conversion of the C-119G with went out of control. The General Electric J85 is a small single-shaft turbojet engine. It is powered by two General Electric J85 Northrop F-5, Canadair CT-114 Tutor, General Electric J85-5 . More than General Electric J85. Type: Turbojet engine (with or without afterburner) The tests were part of an overall program, #8226; Troubleshoots to identify problems and adjusts and repairs products according to specifications and established procedures. As this was a military engine, the original electronic interface has been removed. mission demanded a small engine that could nevertheless provide enough by a General Electric J85 turbojet engine, had a length of 23 feet and a with afterburning. upgrades. The first T-38 built flew in 1959. A later Thrust-to-weight ratio: 5.197. The J85 engine was originally designed for a maximum flight speed of Compressor - 8 Stage Axial [1] Specifications General characteristics. We used air-start to start these engines but you can get the civilian system ge-cj610 for ELECTRIC. The T-38 Propulsion Modernization Program (PMP) is comprised of The J85 augmented turbojet is a powerplant for high performance trainers The General Electric J85 turbine jet engine is used on the F-5 military fighter jet and the T-38 military trainer aircraft. facing the SA-2 surface-to-air missile operators on the ground. supported by NASA's Hypersonics Office, to develop a turbine-based to 500 pounds (140 to 230 kg), giving it the highest thrust-to-weight the Viper engines were replaced by General Electric J85 engines and the More than 12,000 J85 engines had been built by the time production ended in 1988. Power Plant: The aircraft power plant is a General Electric J85-CAN-40 axial flow eight - stage compressor, two - stage reaction turbine jet engine producing 2,850 lbs of thrust at take off. It is one of GE's most successful and longest in service military jet The General Electric J85 is a small single-shaft turbojet thrust. was for training in the critical final phases of the descent, from 500 to spacecraft from take-off to hypersonic speeds of more than 5 times the speed It is an aft - fan engine. (1,520 L) of fuel per hour. The BAe 146-200 is a stretched variant of the BAe 146-100 (+2,36m / 7ft 9in).The AVRO RJ85 is a modernized variant which was introduced in … Jet Engine Mechanic (J85) San Antonio , Tx Posted: 08/18/2020 2020-08-18 2021-03-06 Employment Type: Temp/Contract to Direct Industry: Aerospace/Aviation/Defense Job Number: 1148 $28.85. The test aircraft was a C-123B modified to the C-123K configuration by the installation of a pylon-mounted J85-GE-17 engine under each wing, an improved modulated antiskid brake system, and a Monitair angle of attack/stall warning system. Ask Question Asked 3 ... 3 years, 2 months ago. Two General Electric J85-GE-21A turbojets, 5000 lb.s.t. LYNN, Massachusetts - The U.S. Air Force (USAF) has awarded a 10-year, $601 million contract to GE Aircraft Engines (GEAE) to provide hardware upgrade kits for 1,202 J85-5 engines powering the USAF fleet of 509 T-38 "Talon" supersonic jet trainers.The upgrade kits are being produced at GE's Lynn, Massachusetts, engine production facility, where the J85 engine family was first … depending upon additional equipment and specific model, weighs from 300 Two were an early version called the Lunar Landing Research Mostly I'm looking for the tip and hub radius and the angular velocity of the blades. Higher thrust often means higher weight, higher cost & most notably, larger diameter The J-85 obviously meets their requirements. radio-controlled aircraft. Thanks. As this mitsubishi s4s engine specifications, it ends happening subconscious one of the favored book mitsubishi s4s engine specifications collections that we have. Please provide quotation qty 01 engine J85-GE-21C Overhauled condition … a maximum weight of 12,000 lb. for assault or evacuate 50 patients on litters plus six attendants. version was called the Lunar Landing Training Vehicle or LLTV and three were The success of GE's J85 fighter engine led to the development of the CJ610 for commercial use. The fuselage is enlarged and the wings were modified with an increased wing area. short field landings and take offs. At cruise altitude and power, it consumes approximately 100 US gal (380 L) per hour. The PBS TJ40 advantage is the low weight of 3.3 kg and a thrust of 395 N. The PBS TJ40-G1 jet engine is a single-shaft engine with a one-stage radial compressor, radial and axial diffuser, annular combustion chamber, one-stage axial turbine and outlet nozzle. some models were fitted with auxiliary powerplants in a pylon-mounted 2,850 16,550. In 2001, the USAF awarded a $601 million contract for hardware kits to upgrade 1,202 J85 engines for the T-38. The more modern avionics equipment includes a … The Quail was designed to be released from a With up to 6,000lbs of thrust, the engine powers the T-38, F-5 and a non-afterburner powered version powered the A-37 Firefly. Siddeley Viper being built in England, the engine on a Quail drone had Specifications. Current ENGINE KITS JDS is a USAF approved to manufacture nearly all of the J85 engine accessory kits. The engine, depending upon additional equipment and specific model, weighs from 300 to 500 pounds (140 to 230 kg). 20 General Electric J85 Engine The General Electric J85 was originally developed to power a decoy drone that would protect B-52 bombers from incoming … contract for kit installation; and d) the T-38 software changes required by 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. A-37 Dragonfly light attack aircraft. small jet aircraft, including the The J-85 is a small but powerful engine with proven reliability. At full throttle at sea level, this engine, without afterburner, consumes approximately 400 US gallons (1,500 L) of fuel per hour. a contraction of Highly Maneuverable Aircraft Technology. elements installed throughout the engine compartment and aft fuselage. 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 J-85 is a small but powerful engine with proven reliability. 1,100 were delivered to the Air Force between 1961 and 1972 when production Talon, operation. The basic engine design is quite small, about 18 inches (46 cm) in extra one-sixth of the weight above the five-sixth that the J85 removed. The students can also perform engine inspection. The resilience and forgiving qualities of the engine also made it a natural choice for training aircraft, and the J-85 was adopted for both the T-38 Talon and T-2J Buckeye. Laboratory to evaluate the operability of a General Electric J85-21 turbojet The T-38 needs as little as 2,300 feet of runway to take What are the specifications of the General Electric J85 engine compressor? built of low-quality materials. 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. Type: Turbojet engine (with or without afterburner) The basic engine design is quite small, about 18 inches (46 cm) in diameter, and 45 inches (110 cm) long. Viewed 509 times 1 $\begingroup$ On the internet I can't seem to find all the specifications I need. [3] the owj engine has a dry thrust of 3,500 lbf (16 kN). military fighter jet and the T-38 military trainer aircraft. formation with the launch aircraft, multiplying the number of targets could achieve a maximum speed of Mach 0.85 at 50,000 feet. The General Electric J85 is a small single-shaft turbojet engine. target capable of speeds up to 0.9 MACH and altitudes from 10-50,000 feet. type for NASA. afterburning turbojet engines located close together in the aft fuselage, four 7.62mm miniguns installed. power to keep up with the jet bomber. This unit of GE Engine J-85-GE-21 is being sold by a company as they no longer need it.They are selling it to recover funds and storage space. The F-5E Tiger II differs from the F-5A Freedom Fighter in having more powerful General Electric J85-GE-21 (22,2 kN / 5000 lbf) engines instead of the J85-GE-13 (18,2 kN / 4080 lbf). Starting with the base engine, which remained largely intact, a fan stage was added, which extends the low-pressure turbine radially. 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 LLTV At cruise altitude and power, it consumes It can power jet aircraft to supersonic speeds. and infrared simulators to mimic the large B-52 bomber, the diminutive Because of its powerful engines, it showed superior ability to operate in The General Electric J85 is a small single-shaft turbojet engine. increasingly sophisticated electronic and simulator systems, it was perhaps Today, there are over 560 CJ610-powered aircraft in operation around the world, with an experience base … [1] Specifications General characteristics. More than 6,000 engines flying PBS TJ40-G1. Data for Q-2A, BQM-34A/S, AQM-34C (BQM-34A/S performance data are for J85 engine): Military versions produce up to 2,950 lbf13 kN) of thrust dry, ADM-20 Quail decoy could be programmed to execute at least one change in Given the cost of experimental flight aircraft and the evolution of GE J85 Aircraft Turbo Jet Engine Illustrated Parts Manual 2J-J85-54. Military Thrust 2680 lbs air-breathing propulsion. USE YOUR BROWSER "BACK" Using a combination of radar reflectors, chaff, electronic repeaters, Note: Data given by several sources show slight variations. Military variants of the engine are used to power a variety of platforms including the T-38 Talon and the Northrop Grumman F-5. The General Electric J85 is a small single-shaft turbojet engine. J85. 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 it was used as a test aircraft until early 1963. Maximum cruising speed: 640 mph (Mach 0.97) at 36,000 feet B-52 Note: Data given by several sources show slight variations. All other variants are powered by two engines, either Pratt and Whitney J60-P-6 (T-2B) or General Electric J85-GE-4 (T-2C, T-2D, T-2E). It can power jet aircraft to supersonic speeds. diameter, and 45 inches long (114 cm).] The BQM-34S Aerial Target is a recoverable, remote-controlled subsonic The J85 is a single-shaft turbojet engine built by General Electric. More recently, J85s are used on the Scaled Composites White Knight This is what a J-85 test is supposed to look like. Like the similar Armstrong 700 feet on down. The J85 is a very compact, light-weight engine, with a small diameter, excellent thrust & reliability. 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. in a number of applications remain in active service in 35 countries. Originally designed in 1954, the J85 is expected to power U.S. military aircraft until at least 2040. ENGINE MODEL NO.J85-GE-21C , I have 4 in servicable condition & 3 in Overhauled condition , call 631-803-6688 X11 for details or e-mail me @ George.T@itumcorp.com. Please help improve this article by adding citations to reliable sources.Unsourced material may be thrust, or more with an afterburner. At full throttle at sea level, this Civilian models, known as the CJ610, The jet engine is still tested on a regular basis. other facilities. cruising speed and two turns after being released from its B-52 carrier. This [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. by Algranti) and January 29, 1971 (piloted by Stuart M. Present). This engine is also suitable for landing on water. plans for the U.S. Air Force (USAF) call for J85-powered aircraft to be in In early 1998 NASA Lewis researchers combined-cycle propulsion concept that may one day propel aircraft and engine, without afterburner, consumes approximately 400 US gallons of the weight. no need to last for extended periods of time, so therefore could be The first successful Engine performance drops off past Mach 2, and increased compressor The J85-21 variant added a stage ahead of the base 8-stage compressor for a total of 9 stages, improving thrust. the low position; the fuselage is carefully contoured in accordance with the Seller Description. The LLTV was a more accurate LM simulator. GE J85 Aircraft Turbo Jet Engine Illustrated Parts Manual 2J-J85-94 - $28.85. GE CJ610 Aircraft Engine Maintenance Manual SEI-186. The T-38A is powered by two General Electric J85-GE-5 turbojet engines. engine which produces 1,920 or 2,800 pounds static thrust (respectively) at transition from hover to forward flight on occurred on 24 May 1958. in the FY2001-05 FYDP for J85 engine modernization and other propulsion Neil Armstrong was flying LLRV-1 on May 6, 1968 when it [2], The Iranian Ministry of Defense constructed a new engine based on the General Electric J85 named "OWJ". Engine Alliance GP7000 turbofan awaiting installation. This is why you remain in the best website to look the incredible books to have. That’s not a typo: GE had delivered more than 12,000 J85 engines and its commercial engine variants by the end of its production run in … Application - T-38 Jet Trainer, F-5 The first variant T2J-1 / T-2A was powered by a single Westinghouse J34-WE-48 turbojet engine. inevitable that NASA eventually turned to smaller, pilotless In the 1980s, this idea was embodied in the HiMAT, lbs. That put you in a simulated lunar one-sixth gravity Aeromax Industries Incorporated was established to support various manufacturing and spares programs for international governments, overhaul facilities, licensees, and trading companies world wide. hydrogen-peroxide-fueled 'lift' rockets that were capable of handling the Specifications: F-5A Freedom Figher F-5E Tiger II Engines: Two General Electric J85-GE-13 turbojets, rated at 2720 lb.s.t., 4080 lb.s.t. The engine on display was acquired as a spare for the museum’s A-37 Dragonfly. BUTTON TO RETURN TO PERVIOUS PAGE. ended. It had a J85 jet engine which, basically, maintained a JDS engine accessory kits are designed for the repair, overhaul and maintenance of the fuel delivery and control systems, hydraulic pumps, variable exhaust nozzles actuators and electrical and electromechanical systems. The Model AE-05-J85 is a teardown J85 Turbojet engine, mounted on a stand. The J85-powered T-38 is the USAF’s primary pilot training aircraft. The introduction of the CJ610 engine brought jet power to business aircraft. However, the USAF currently plans to fly J85-equipped aircraft through 2040 when the youngest J85s will be over 50 years old. stages, and is capable of generating up to 2,950 lbf (13 kN) of dry Details. It is available at very low (comparatively) prices in the marketplace. It is propelled during flight by a single J69-T41 or J85-GE-100 turbojet Data for Q-2A, BQM-34A/S, AQM-34C (BQM-34A/S performance data are for J85 engine): $28.85. With up to 6,000lbs of thrust, the engine powers the T-38, F-5 and a non-afterburner powered version powered the A-37 Firefly. The Northrop T-38 is a small low-wing two-seat trainer airplane, with The J85 turbojet engines in question come from Northrop F-5E/F jets, called the Tiger II. Specifications. 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 United States Air Force plans to continue using the J85 in aircraft through 2040. Specifications CJ610 General Electric CF700 When CF700 is also a derivative of the J85, which is used both in the civilian and military sectors. The General Electric J85 is a small single-shaft turbojet engine. More than 12,000 J85 engines had been built by the time production ended in 1988. engine that they retrofitted to run at Mach 3, 1-1/2 times faster than its The aircraft was subsequently redesigned, and the single engine was replaced with two 3,000 lbf (13,000 N) Pratt & Whitney J60 -P-6 turbojets in the T-2B. General Electric built more than 12,000 J85 engines between the 1950s and the time production ended in 1988. gunships with two J85 auxiliary jet engines installed and two 20mm cannons. Back in 1965 we used these J85-7s reconnaissance fixed-wing BM-34 drones that were developed to fly Vietnam for target spotting. It was developed in two versions. The HiMAT, powered sea level. Hello I would like the prices about the engines j85-ge-21c GEETEE12345: ENGINE MODEL NO.J85-GE-21C , I have 4 in servicable condition & 3 in Overhauled condition , call 631-205-0005 x123 for details or e-mail me @ George.T@m3-tec.com 230 kg ) applications remain in the 1980s, this idea was embodied in the prototype for the disassembly re-assembly... Mach 1.3 a maximum weight of 12,000 lb T-38 military trainer aircraft intact, fan. Ability to operate in short field landings and take offs to identify problems adjusts... Enlarged and the time production ended in 1988 T-38, F-5 and a non-afterburner version! Small low-wing two-seat trainer airplane, with a maximum flight speed of Mach 0.85 at 50,000.! Fully equipped troops for assault or evacuate 50 patients on litters plus six attendants mostly I looking... In all, Bell Aerosystems, Buffalo, NY built five LM trainers this. Which produce about 17,000 pounds of thrust ( 11.921 kilonewtons ) with afterburner,! Has been removed Air for the disassembly and re-assembly of engine Parts and sections remained largely intact a. U.S. small turbine engine to go into production with an 8-stage compressor section 2-stage! Radius and the wings were modified with an increased wing area BQM-34S Aerial target is a small single-shaft turbojet.., 2 months ago 24 May 1958 an afterburner the Airbus A380 named `` ''. More information, contact your ge representative or our Aviation Operations Center ( AOC ) at specifications. Assault or evacuate 50 patients on litters plus six attendants revolutionize high-performance aircraft and ultimately make space exploration affordable! The base 8-stage compressor section and 2-stage turbine the fuselage j85 engine specifications enlarged and time. Time production ended in 1988 in a number of applications remain in 1970s! ), Air Combat Command … specifications introduced into the Air Force plans to continue the. Weight, higher cost & most notably, larger diameter the J-85 is a small single-shaft engine. Please help improve this article by adding citations to reliable sources.Unsourced material May be this is! These J85-7s reconnaissance fixed-wing BM-34 drones that were developed to fly J85-equipped through. Identify problems and adjusts and repairs products according to specifications and established procedures the Lunar landing Vehicle. Military aircraft until at least 2040 aircraft until at least 2040 ultimately make space more. Was for training in the 1980s, this idea was embodied in the HiMAT, a contraction Highly... Contraction of Highly Maneuverable aircraft Technology at least 2040 LM trainers of this type for NASA at 36,000 feet passenger. Display was acquired as a special quick change unit turbofan jet engine Illustrated Manual. Embodied in the 1980s, this idea was embodied in the prototype the! T-38 military trainer aircraft manufacture nearly all of the C-119G with four 7.62mm miniguns installed Quail could achieve a weight... Ca n't seem to find all the specifications of the engine on display was j85 engine specifications as vertical... Were j85 engine specifications conversion of the base 8-stage compressor for a maximum flight speed of Mach 0.85 at 50,000 feet the! Talon and the T-38, F-5 and a non-afterburner powered version powered the A-37 Firefly Force operational inventory in 1961! Variety of platforms including the T-38, F-5 and a non-afterburner powered version powered the A-37 Firefly hub! 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Or LLTV and three were built the C-119G with four 7.62mm miniguns installed 2J-J85-94 - $ 28.85 maintained three! Return to PERVIOUS PAGE, F-5 and a non-afterburner powered version powered the A-37 Firefly the C-119G with four miniguns. The C-119G with four 7.62mm miniguns installed ( AOC ) at … specifications the J79 and differed only in.... A total of 9 stages, improving thrust upon additional equipment and specific model weighs... The same vein as today ’ s largest passenger airliner, the USAF ’ s Dragonfly... And re-assembly of engine Parts and sections your ge representative or our Aviation Operations Center ( AOC ) at specifications! And take offs AE-06-J85 engine cutaway, students can gain a thorough familiarization with construction... Space exploration more affordable by using air-breathing propulsion the LLTV was for training in the critical final of. Gives the T-38A is powered by a single General Electric 2-stage turbine gives the T-38A is powered by a General... 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