That's it. The GE - J85 The General Electric J85 is a small single-shaft turbojet engine. The engine, depending upon additional equipment and specific model, weighs from 300 to 500 pounds (140 to 230 kg). V závislosti na doplňkovém vybavení a konkrétním modelu motor váží od 140 do 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 General Electric J85 is a small single-shaft turbojet engine. Military versions produce up to 2,950 lbf(13.1 kN) of thrust dry, afterburningvariants can reach up to 5,000 lbf(22 kN). A mock-up was built, but the P7M, Convair XP6Y and Grumman G-132 were all cancelled when the US Navy abandoned their open-ocean seaplane requirement. 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. 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. 400 km/h Gear. Military versions produce up to 2,950 lbf of thrust dry; afterburning variants can reach up to 5,000 lbf . Would you like to suggest this photo as the cover photo for this article? The G.91 YS is a multi-role fighter which first debuted in 1966. 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. The G.91Y was an increased performance version of the Fiat G.91 funded by the Italian government. At full throttle at sea level, this engine, without afterburner, consumes approximately 400 US gallons (1,500 L) of fuel per hour. Military versions produce up to 2,950 lbf13 kN) of thrust dry, afterburning variants can reach up to 5,000 lbf (22 kN). The General Electric J85 is a small single-shaft turbojet engine. The biggest difference between the two types was the conversion from a single-engine to two General Electric … It was developed in two versions. 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. The G.91 YS is a rank VI Italian jet fighter with a battle rating of 9.7 (AB/RB) and 9.3 (SB). 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. 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. Give good old Wikipedia a great new look: Cover photo is available under {{::mainImage.info.license.name || 'Unknown'}} license. Air Force and Navy Firebees have received further upgrades since that time, most refitted beginning in 1989 with the improved J85-GE-100 engine (also with 2,450 lb f (10.9 kN) thrust) as V závislosti na doplňkovém vybavení a konkrétním modelu motor váží od 140 do 230 kg. 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). The engine, depending upon additional equipment and specific model, weighs from 300 to 500 pounds (140 to 230 kg). You can help our automatic cover photo selection by reporting an unsuitable photo. Speed of destruction. 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. 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. Vojenské verze poskytují "na sucho" tah 13,1 kN, zatímco varianty s přídavným spalováním dosahují až 22 kN. The General Electric J85 is a small single-shaft turbojet engine. [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 basic engine design is quite small, about 18 inches (46 cm) in diameter, and 45 inches (110 cm) long. The General Electric J85is a small single-shaft turbojetengine. It will enhance any encyclopedic page you visit with the magic of the WIKI 2 technology. Type. 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 Congratulations on this excellent venture… what a great idea! 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. The J85-GE-5 is rated at 2,680 pounds of thrust (11.921 kilonewtons), and … The General Electric CJ805 is a jet engine which was developed by GE Aviation in the late 1950s. V závislosti na doplňkovém vybavení a konkrétním modelu motor váží od 140 do 230 kg. Daha sonra Rockwell Sabreliner olarak satılan Kuzey Amerika Sabreliner , North tarafından geliştirilen bir Amerikan orta ölçekli iş jeti Amerikan Havacılığı . Maury 15:04, 30 January 2007 (UTC) I'd suggest merge to J85 but rename to General Electric J85/CJ610 Akradecki 16:30, 30 January 2007 (UTC) The engine, depending upon additional equipment and specific model, weighs from 300 to 500 pounds . The first YAT-37D flew in October 1964, followed a year later by the second prototype. 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). V závislosti na doplňkovém vybavení a konkrétním modelu motor váží od 140 do 230 kg. Today, there are over 560 CJ610-powered aircraft in operation around the world, with an experience base … This mission demanded a small engine that could nevertheless provide enough power to keep up with the jet bomber. Saab 105XT : Export demonstrator; improved version of the SK 60B, re-engined with 12.85 kW (2,850 lbf) General Electric J85 turbojets. {{::mainImage.info.license.name || 'Unknown'}}, {{current.info.license.usageTerms || current.info.license.name || current.info.license.detected || 'Unknown'}}, Uploaded by: {{current.info.uploadUser}} on {{current.info.uploadDate | date:'mediumDate'}}. It seems the other pages don't have a clear one-way-or-the-other. 12 x m/56D rockets Setup 3. Chapter 6 of 13 - Power of the J85 and TF39, General Electric J85 | Wikipedia audio article, A J85-GE-17A engine sectioned for display. Saab 105D : A refined business jet variant was considered, but the idea was out of date and there were no takers. The engine, depending upon additional equipment and specific model, weighs from 300 to 500 pounds . 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. By April … ゼネラル・エレクトリック(英語: General Electric Company、略称: GE )は、アメリカ合衆国を主な拠点とし電気事業をルーツとする多国籍コングロマリット企業である。 世界最大のアメリカ合衆国の総合 … 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 The engine, depending upon additional equipment and specific model, … The introduction of the CJ610 engine brought jet power to business aircraft. Your input will affect cover photo selection, along with input from other users. The General Electric J85 is a small single-shaft turbojet engine. 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 T-38A is powered by two General Electric J85-GE-5 turbojet engines. [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. [2], The Iranian Ministry of Defense constructed a new engine based on the General Electric J85 named "OWJ". The General Electric CJ805 is a jet engine which was developed by GE Aviation in the late 1950s. Utility Trainer Experimental (UTX) programına yanıt olarak Amerika Birleşik Devletleri Hava Kuvvetleri'ne (USAF) teklif edildi. Military versions produce up to 2,950 lbf of thrust dry; afterburning variants can reach up to 5,000 lbf . We have created a browser extension. Prototype converted from second Saab 105 prototype. The X-14 first flew on 19 February 1957 as a vertical takeoff, hover, then vertical landing. GE built more than 12,000 J85 engines before production ended in 1988. It was developed in two versions. 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). No engine in jet propulsion is quite like GE’s tiny J85 turbojet. 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 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. air Cooling system. For faster navigation, this Iframe is preloading the Wikiwand page for, Note: preferences and languages are saved separately in https mode. Would you like Wikipedia to always look as professional and up-to-date? The General Electric J85 turbine jet engine is used on the F-5 military fighter jet and the T-38 military trainer aircraft. You could also do it yourself at any point in time. The J85 was originally designed to power a large decoy missile, the McDonnell ADM-20 Quail. The engine, depending upon additional equipment and specific model, weighs from 300 to 500 pounds (140 to 230 kg). 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. The engine was presented at a defense exhibition on 22 August 2016. One new build prototype and 29 conversions from Sk 60A. That’s not a typo: GE had delivered more than 12,000 J85 engines and its commercial engine variants by the end of … 2 x 30 mm Akan m/55 cannon Setup 1. The United States Air Force plans to continue using the J85 in aircraft through 2040. The General Electric J85 is a small single-shaft turbojet engine. Built on the highly reliable T700, the CT7 engine design has proven itself in harsh environments and has achieved over 37 million engine cycles. 300 hours to fully overhauled conditions and anything in betweens. It was introduced in Update 1.87 "Locked On". The J85 is a single-shaft axial-flow turbojet engine with an 8-stage compressor section and 2-stage turbine. 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… The source code for the WIKI 2 extension is being checked by specialists of the Mozilla Foundation, Google, and Apple. More recently, J85s have powered the Scaled Composites White Knight aircraft, the carrier for the Scaled Composites SpaceShipOne spacecraft, and the Me 262 Project. [3] the owj engine has a dry thrust of 3,500 lbf (16 kN).[4]. The engine, depending upon additional equipment and specific model, weighs from 300 to 500 pounds (140 to 230 kg). The first transition from hover to horizontal flight occurred on 24 May 1958. 1050 km/h Structural. 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. 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. GE built more than 12,000 J85 engines before production ended in 1988. 22 x 7,5 cm srak m/55 Frida rockets Setup 2. 2 x … 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. It was a civilian version of the J79 and differed only in detail. The General Electric J85 is a small single-shaft turbojet engine. 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. 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). J85. General Electric J85 je malý jednohřídelový proudový motor. 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 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. BQM-34A production ended in 1982, but the production line was reopened in 1986 to produce more BQM-34S targets. They are selling it to recover funds and storage space. It will enhance any encyclopedic page you visit with the magic of the WIKI 2 technology. 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). Combat … The General Electric J85 is a small single-shaft turbojet engine. The success of GE's J85 fighter engine led to the development of the CJ610 for commercial use. Kanat ve kuyruğunun Kuzey Amerika'nın F-86 Sabre jet avcı uçağına benzerliği nedeniyle More than 12,000 J85 engines had been built by the time production ended in 1988. 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. From Wikipedia, The Free Encyclopedia The General Electric J85 is a small single-shaft turbojet engine. Several variants were produced. I use WIKI 2 every day and almost forgot how the original Wikipedia looks like. Suspended armament. Originally designed in 1954, the J85 is expected to power U.S. military aircraft until at least 2040. J85 is historically more important -- the others came from it -- but CF610 is much more common. 2 х General Electric J85-GE-17B Engine. The J85-21 variant added a stage ahead of the base 8-stage compressor for a total of 9 stages, improving thrust. That year the aircraft was also delivered to the NASA Ames Research Center as the X-14A. From Wikipedia, the free encyclopedia The Gen­eral Elec­tric J85 is a small sin­gle-shaft tur­bo­jet en­gine. In 1959, its Viper engines were replaced with General Electric J85 engines. To install click the Add extension button. Seller Description This unit of GE Engine J-85-GE-21 is being sold by a company as they no longer need it. At cruise altitude and power, it consumes approximately 100 US gal (380 L) per hour. SK 60C: Two-seat ground attack/reconnaissance version for the Swedish Air Force with extended camera nose. Military versions produce up to 2,950 lbf13 kN) of thrust dry, afterburning variants can reach up to 5,000 lbf (22 kN). It was a civilian version of the J79 and differed only in detail. 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). The non-afterburning J85-GE-17A powered the Cessna A-37A/B attack aircraft. 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). 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