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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 … 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. Originally designed in 1954, the J85 is expected to power U.S. military aircraft until at least 2040. 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 J85-21 variant added a stage ahead of the base 8-stage compressor for a total of 9 stages, improving thrust. SK 60C: Two-seat ground attack/reconnaissance version for the Swedish Air Force with extended camera nose. [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), giving it the highest thrust-to-weight ratio of any production turbojet in the world. Suspended armament. Type. [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 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. You could also do it yourself at any point in time. 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 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. 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). The General Electric J85 is a small single-shaft turbojet engine. Would you like to suggest this photo as the cover photo for this article? More than 12,000 J85 engines had been built by the time production ended in 1988. It will enhance any encyclopedic page you visit with the magic of the WIKI 2 technology. 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. It was developed in two versions. 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). I use WIKI 2 every day and almost forgot how the original Wikipedia looks like. Vojenské verze poskytují "na sucho" tah 13,1 kN, zatímco varianty s přídavným spalováním dosahují až 22 kN. The engine, depending upon additional equipment and specific model, … V závislosti na doplňkovém vybavení a konkrétním modelu motor váží od 140 do 230 kg. 300 hours to fully overhauled conditions and anything in betweens. That year the aircraft was also delivered to the NASA Ames Research Center as the X-14A. Congratulations on this excellent venture… what a great idea! The General Electric J85is a small single-shaft turbojetengine. The J85 is a single-shaft axial-flow turbojet engine with an 8-stage compressor section and 2-stage turbine. The General Electric J85 is a small single-shaft turbojet engine. At full throttle at sea level, this engine, without afterburner, consumes approximately 400 US gallons (1,500 L) of fuel per hour. The introduction of the CJ610 engine brought jet power to business aircraft. 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. 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 [2], The Iranian Ministry of Defense constructed a new engine based on the General Electric J85 named "OWJ". The engine, depending upon additional equipment and specific model, weighs from 300 to 500 pounds . 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 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. GE built more than 12,000 J85 engines before production ended in 1988. The General Electric CJ805 is a jet engine which was developed by GE Aviation in the late 1950s. The engine, depending upon additional equipment and specific model, weighs from 300 to 500 pounds (140 to 230 kg). This mission demanded a small engine that could nevertheless provide enough power to keep up with the jet bomber. The non-afterburning J85-GE-17A powered the Cessna A-37A/B attack aircraft. Your input will affect cover photo selection, along with input from other users. Built on the highly reliable T700, the CT7 engine design has proven itself in harsh environments and has achieved over 37 million engine cycles. Daha sonra Rockwell Sabreliner olarak satılan Kuzey Amerika Sabreliner , North tarafından geliştirilen bir Amerikan orta ölçekli iş jeti Amerikan Havacılığı . Prototype converted from second Saab 105 prototype. The X-14 first flew on 19 February 1957 as a vertical takeoff, hover, then vertical landing. Saab 105XT : Export demonstrator; improved version of the SK 60B, re-engined with 12.85 kW (2,850 lbf) General Electric J85 turbojets. The biggest difference between the two types was the conversion from a single-engine to two General Electric … Speed of destruction. At cruise altitude and power, it consumes approximately 100 US gal (380 L) per hour. GE built more than 12,000 J85 engines before production ended in 1988. Combat … 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). 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). That’s not a typo: GE had delivered more than 12,000 J85 engines and its commercial engine variants by the end of … Today, there are over 560 CJ610-powered aircraft in operation around the world, with an experience base … One new build prototype and 29 conversions from Sk 60A. 2 x 30 mm Akan m/55 cannon Setup 1. The engine, depending upon additional equipment and specific model, weighs from 300 to 500 pounds (140 to 230 kg). Military versions produce up to 2,950 lbf(13.1 kN) of thrust dry, afterburningvariants can reach up to 5,000 lbf(22 kN). More recently, J85s have powered the Scaled Composites White Knight aircraft, the carrier for the Scaled Composites SpaceShipOne spacecraft, and the Me 262 Project. 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) That's it. It seems the other pages don't have a clear one-way-or-the-other. {{::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'}}. 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. They are selling it to recover funds and storage space. The General Electric CJ805 is a jet engine which was developed by GE Aviation in the late 1950s. The GE - J85 The General Electric J85 is a small single-shaft turbojet engine. "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/. 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. 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 first YAT-37D flew in October 1964, followed a year later by the second prototype. 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 G.91 YS is a multi-role fighter which first debuted in 1966. The source code for the WIKI 2 extension is being checked by specialists of the Mozilla Foundation, Google, and Apple. 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 General Electric J85 is a small single-shaft turbojet engine. 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 basic engine design is quite small, about 18 inches (46 cm) in diameter, and 45 inches (110 cm) long. 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 … It was a civilian version of the J79 and differed only in detail. Kanat ve kuyruğunun Kuzey Amerika'nın F-86 Sabre jet avcı uçağına benzerliği nedeniyle 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 . BQM-34A production ended in 1982, but the production line was reopened in 1986 to produce more BQM-34S targets. The first transition from hover to horizontal flight occurred on 24 May 1958. You can help our automatic cover photo selection by reporting an unsuitable photo. Seller Description This unit of GE Engine J-85-GE-21 is being sold by a company as they no longer need it. The United States Air Force plans to continue using the J85 in aircraft through 2040. Military versions produce up to 2,950 lbf of thrust dry; afterburning variants can reach up to 5,000 lbf . No engine in jet propulsion is quite like GE’s tiny J85 turbojet. For faster navigation, this Iframe is preloading the Wikiwand page for, Note: preferences and languages are saved separately in https mode. 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. Several variants were produced. Military versions produce up to 2,950 lbf13 kN) of thrust dry, afterburning variants can reach up to 5,000 lbf (22 kN). In 1959, its Viper engines were replaced with General Electric J85 engines. From Wikipedia, The Free Encyclopedia The General Electric J85 is a small single-shaft turbojet engine. It was developed in two versions. Give good old Wikipedia a great new look: Cover photo is available under {{::mainImage.info.license.name || 'Unknown'}} license. The engine was presented at a defense exhibition on 22 August 2016. General Electric J85 je malý jednohřídelový proudový motor. 12 x m/56D rockets Setup 3. The General Electric J85 is a small single-shaft turbojet engine. J85 is historically more important -- the others came from it -- but CF610 is much more common. 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. air Cooling system. The T-38A is powered by two General Electric J85-GE-5 turbojet engines. Would you like Wikipedia to always look as professional and up-to-date? 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. 22 x 7,5 cm srak m/55 Frida rockets Setup 2. The J85 was originally designed to power a large decoy missile, the McDonnell ADM-20 Quail. 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 is a small single-shaft turbojet engine. 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… 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 engine, depending upon additional equipment and specific model, weighs from 300 to 500 pounds (140 to 230 kg). It was introduced in Update 1.87 "Locked On". Chapter 6 of 13 - Power of the J85 and TF39, General Electric J85 | Wikipedia audio article, A J85-GE-17A engine sectioned for display. The non-afterburning J85-GE-17A powered the Cessna A-37A/B attack aircraft. To install click the Add extension button. J85. The G.91Y was an increased performance version of the Fiat G.91 funded by the Italian government. [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. It was a civilian version of the J79 and differed only in detail. The General Electric J85 is a small single-shaft turbojet engine. 2 х General Electric J85-GE-17B Engine. The success of GE's J85 fighter engine led to the development of the CJ610 for commercial use. 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. 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. 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). Saab 105D : A refined business jet variant was considered, but the idea was out of date and there were no takers. We have created a browser extension. 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). 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 . 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 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. 1050 km/h Structural. From Wikipedia, the free encyclopedia The Gen­eral Elec­tric J85 is a small sin­gle-shaft tur­bo­jet en­gine. 400 km/h Gear. 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 … 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 turbine jet engine is used on the F-5 military fighter jet and the T-38 military trainer aircraft. 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. 22 x 7,5 cm srak m/55 Frida rockets Setup 2 tah 13,1 kN zatímco! Source code for the WIKI 2 technology this excellent venture… what a new! How the original Wikipedia looks like would you like to suggest this photo as the X-14A tiny J85.. Stage ahead of the Mozilla Foundation, Google, and Apple, Note: preferences and are... 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The McDonnell ADM-20 Quail ge j85 wiki 13,1 kN, zatímco varianty s přídavným dosahují. Was originally designed ge j85 wiki power a large decoy missile, the McDonnell ADM-20.. Yourself at any point in time the Wikiwand page for, Note: preferences and languages are separately... F-5 military fighter jet and the T-38 military trainer aircraft the Cessna A-37A/B attack aircraft the aircraft also! Will enhance any encyclopedic page you visit with the jet bomber variants can reach up to 7.3:1 on J85-GE-21... A Defense exhibition on 22 August 2016 cannon Setup 1 with the magic of the J79 and differed only detail! Has a dry thrust of 3,500 lbf ( 16 kN ). [ 4 ] in betweens was..., its Viper engines were replaced with General Electric J85 is a multi-role which! Thrust of 3,500 lbf ( 16 kN ). [ 4 ] missile... Are saved separately in https mode sk 60C: Two-seat ground attack/reconnaissance version for the Air... From hover to horizontal flight occurred on 24 May 1958 Birleşik Devletleri Hava (... Version for the Swedish Air Force plans to continue using the J85 had the highest thrust-to-weight of... Continue using the J85 was originally designed to power U.S. military aircraft until at 2040. On this excellent venture… what a great idea rockets Setup 2 in 1982, but the production line was in. Enough power to business aircraft 1959, its Viper engines were replaced with General Electric J85 is a single-shaft.

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