The J85 was originally designed to power a large decoy missile, the McDonnell ADM-20 Quail. The T-38A is powered by two General Electric J85-GE-5 turbojet engines. The engine, depending upon additional equipment and specific model, weighs from 300 to 500 pounds (140 to 230 kg). 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. By April … Your input will affect cover photo selection, along with input from other users. 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). Would you like to suggest this photo as the cover photo for this article? The General Electric J85 is a small single-shaft turbojet engine. It was a civilian version of the J79 and differed only in detail. 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. More recently, J85s have powered the Scaled Composites White Knight aircraft, the carrier for the Scaled Composites SpaceShipOne spacecraft, and the Me 262 Project. J85. Vojenské verze poskytují "na sucho" tah 13,1 kN, zatímco varianty s přídavným spalováním dosahují až 22 kN. Re: J85 GE -21 C Engines for sale Reply Quote I am inquiring to see if you have any GE J85-17 , GE J85-21 and GE J85-15 Engines in good working orders ranging from Min. 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. To install click the Add extension button. 22 x 7,5 cm srak m/55 Frida rockets Setup 2. In 1959, its Viper engines were replaced with General Electric J85 engines. The United States Air Force plans to continue using the J85 in aircraft through 2040. It will enhance any encyclopedic page you visit with the magic of the WIKI 2 technology. Military versions produce up to 2,950 lbf of thrust dry; afterburning variants can reach up to 5,000 lbf . It was developed in two versions. 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 CJ805 is a jet engine which was developed by GE Aviation in the late 1950s. 300 hours to fully overhauled conditions and anything in betweens. Several variants were produced. The J85 had the highest thrust-to-weight ratio of production engines built for its time (up to 7.3:1 on the J85-GE-21). The non-afterburning J85-GE-17A powered the Cessna A-37A/B attack aircraft. The J85 had the highest thrust-to-weight ratio of production engines built for its time (up to 7.3:1 on the J85-GE-21). It seems the other pages don't have a clear one-way-or-the-other. [3] the owj engine has a dry thrust of 3,500 lbf (16 kN).[4]. Daha sonra Rockwell Sabreliner olarak satılan Kuzey Amerika Sabreliner , North tarafından geliştirilen bir Amerikan orta ölçekli iş jeti Amerikan Havacılığı . It was introduced in Update 1.87 "Locked On". The General Electric J85 is a small single-shaft turbojet engine. [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. The General Electric J85 is a small single-shaft turbojet engine. The source code for the WIKI 2 extension is being checked by specialists of the Mozilla Foundation, Google, and Apple. SK 60C: Two-seat ground attack/reconnaissance version for the Swedish Air Force with extended camera nose. The J85-GE-5 is rated at 2,680 pounds of thrust (11.921 kilonewtons), and … Utility Trainer Experimental (UTX) programına yanıt olarak Amerika Birleşik Devletleri Hava Kuvvetleri'ne (USAF) teklif edildi. Structural modifications to reduce airframe weight increased performance further and an additional fuel tank occupying the space of the G.91T's rear seat provided extra range. The General Electric J85 is a small single-shaft turbojet engine. 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 Originally designed in 1954, the J85 is expected to power U.S. military aircraft until at least 2040. Saab 105D : A refined business jet variant was considered, but the idea was out of date and there were no takers. I use WIKI 2 every day and almost forgot how the original Wikipedia looks like. You can help our automatic cover photo selection by reporting an unsuitable photo. V závislosti na doplňkovém vybavení a konkrétním modelu motor váží od 140 do 230 kg. 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 General Electric J85 turbine jet engine is used on the F-5 military fighter jet and the T-38 military trainer aircraft. The biggest difference between the two types was the conversion from a single-engine to two General Electric … Military versions produce up to 2,950 lb f (13.1 kN) of thrust dry; afterburning variants can reach up to 5,000 lbf (22 kN). Type. 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. 2 x … The engine, depending upon additional equipment and specific model, weighs from 300 to 500 pounds (140 to 230 kg), giving it the highest thrust-to-weight ratio of any production turbojet in the world. GE's successful T700/CT7 family of turboprop and turboshaft engines powers 25 types of helicopters and fixed-wing aircraft with more than 130 customers in more than 50 countries. Congratulations on this excellent venture⦠what a great idea! The non-afterburning J85-GE-17A powered the Cessna A-37A/B attack aircraft. The engine, depending upon additional equipment and specific model, weighs from 300 to 500 pounds . 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 J85-21 variant added a stage ahead of the base 8-stage compressor for a total of 9 stages, improving thrust. General Electric J85 je malý jednohřídelový proudový motor. It was developed in two versions. The design was unveiled in Denver on November 15, 2016 and it was initially intended to make its first subsonic flight in late 2017, powered by three General Electric CJ610 turbojets (a civilian J85), with subsequent supersonic flight testing at Edwards AFB. Military versions produce up to 2,950 lbf(13.1 kN) of thrust dry, afterburningvariants can reach up to 5,000 lbf(22 kN). The first transition from hover to horizontal flight occurred on 24 May 1958. air Cooling system. Kanat ve kuyruğunun Kuzey Amerika'nın F-86 Sabre jet avcı uçağına benzerliği nedeniyle The introduction of the CJ610 engine brought jet power to business aircraft. Seller Description This unit of GE Engine J-85-GE-21 is being sold by a company as they no longer need it. Military versions produce up to 2,950 lbf13 kN) of thrust dry, afterburning variants can reach up to 5,000 lbf (22 kN). You could also do it yourself at any point in time. The engine, depending upon additional equipment and specific model, weighs from 300 to 500 pounds (140 to 230 kg). From Wikipedia, The Free Encyclopedia The General Electric J85 is a small single-shaft turbojet engine. The J85 is a single-shaft axial-flow turbojet engine with an 8-stage compressor section and 2-stage turbine. One new build prototype and 29 conversions from Sk 60A. V závislosti na doplňkovém vybavení a konkrétním modelu motor váží od 140 do 230 kg. 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 400 km/h Gear. Combat … The engine was presented at a defense exhibition on 22 August 2016. For faster navigation, this Iframe is preloading the Wikiwand page for, Note: preferences and languages are saved separately in https mode. 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. 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. 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