Cart 0 J85 ⦠The engine, depending upon additional equipment and specific model, weighs from 300 to 500 pounds (140 to 230 kg). The General Electric CJ805 is a jet engine which was developed by GE Aviation in the late 1950s. Line: 208 Seller Description This unit of GE Engine J-85-GE-21 is being sold by a company as they no longer need it. Pre-Owned. 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. The basic airframe was used for the light combat aircraft F-5 Freedom Fighter family. At full throttle at sea level, this engine, without afterburner, consumes approximately 400 US gallons (1,500 L) of fuel per hour. The J85-21 variant added a stage ahead of the base 8-stage compressor for a total of 9 stages, improving thrust. The introduction of the CJ610 engine brought jet power to business aircraft. Maury 15:04, 30 January 2007 (UTC) I'd suggest merge to J85 but rename to General Electric J85/CJ610 Akradecki 16:30, 30 ⦠This mission demanded a small engine that could nevertheless provide enough power to keep up with the jet bomber. The T-2D was an export version which ⦠SK 60C: Two-seat ground attack/reconnaissance version for the Swedish Air Force with extended camera nose. The basic engine design is quite small, about 18 inches (46 cm) in diameter, and 45 inches (110 cm) long. At cruise altitude and power, it consumes approximately 100 US gal (380 L) per hour. The engine, depending upon additional equipment and specific model, weighs from 300 to 500 pounds (140 to 230 kg). 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 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. 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). Function: view, File: /home/ah0ejbmyowku/public_html/application/controllers/Main.php 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. The G.91 YS is a multi-role fighter which first debuted in 1966. More than 12,000 J85 engines had been built by the time production ended in 1988. 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. Line: 478 The engine, depending upon additional equipment and specific model, weighs from 300 to 500 pounds (140 to 230 kg). 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 General Electric J85 is a small single-shaft turbojet engine. 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. A J85-GE-17A engine sectioned for display, https://en.wikipedia.org/w/index.php?title=General_Electric_J85&oldid=993624147. In the 1950s Northrop began studying lightweight and more affordable fighter designs. [3] the owj engine has a dry thrust of 3,500 lbf (16 kN). Function: require_once. 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. 미êµì ë¤ê°í ë¶ì¼ ë기ì .본ì¬ë ë¯¸êµ ë§¤ì¬ì¶ì¸ì¸ 주 ë³´ì¤í´ì ìë¤. The F404 was developed into the larger F414 turbofan, as well as the experimental GE36 civil propfan 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). Originally designed in 1954, the J85 is expected to power U.S. military aircraft until at least 2040. It was re-designated the T-2A in 1962 under the joint aircraft designation system. 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). Line: 192 The Iranian Ministry of Defense constructed a new engine based on the General Electric J85 named "OWJ". The work on the 805 also had several spin-off products. Line: 24 Are you sure you want to cancel your membership with us? Thatâs not a typo: GE had delivered more than 12,000 J85 engines and its commercial engine variants by the end of ⦠The General Electric J85 is a small single-shaft turbojet engine. Function: _error_handler, File: /home/ah0ejbmyowku/public_html/application/views/page/index.php J85 is historically more important -- the others came from it -- but CF610 is much more common. Function: _error_handler, File: /home/ah0ejbmyowku/public_html/application/views/user/popup_harry_book.php 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. Function: _error_handler, Message: Invalid argument supplied for foreach(), File: /home/ah0ejbmyowku/public_html/application/views/user/popup_modal.php No engine in jet propulsion is quite like GEâs tiny J85 turbojet. 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 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). At cruise altitude and power, it consumes approximately 100 US gal (380 L) per hour. The T-38A is powered by two General Electric J85-GE-5 turbojet engines. EMAIL: [email protected] | TEL: +1 516.544.4999 Gbenga Showunmi Menu. 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 General Electric J85 is a small single-shaft turbojet engine. U.S.A. GE Aviation. The engine was presented at a defense exhibition on 22 August 2016. Line: 68 Although the USAF had no need for a small fighter at the time, it be⦠ãæé使ç¨ããã¦ããã è»ç¨ã®ãã®ã¯æ¨å 2,950 lbf (13 kN) ã§ããã ã¢ãã¿ã¼ãã¼ãã¼ ä»ãã§ã¯æ大 5,000 lbf (22 kN) 㫠⦠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). General Electric CJ610 From Wikipedia, the free encyclopedia 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 General Electric J85 is a small single-shaft turbojet engine. More recently, J85s have powered the Scaled Composites White Knight aircraft, the carrier for the Scaled Composites SpaceShipOne spacecraft, and the Me 262 Project. General Electric J85 je malý jednohÅídelový proudový motor. 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 biggest difference between the two types was the conversion from a single-engine to two General Electric ⦠The T-2C was fitted with two much more powerful 2,950 lbf (13,100 N) thrust General Electric J85-GE-4 turbojets. It was introduced in Update 1.87 "Locked On". 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 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). Function: view, 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. Function: _error_handler, File: /home/ah0ejbmyowku/public_html/application/views/page/index.php The United States Air Force plans to continue using the J85 in aircraft through 2040. More than 12,000 J85 engines had been built by the time production ended in 1988. The engine, depending upon additional equipment and specific model, weighs from 300 to 500 pounds (140 to 230 kg). Several variants were produced. The J85 is a single-shaft axial-flow turbojet engine with an 8-stage compressor section and 2-stage turbine. The engine, depending upon additional equipment and specific model, weighs from 300 to 500 pounds (140 to 230 kg). Line: 107 At full throttle at sea level, this engine, without afterburner, consumes approximately 400 US gallons (1,500 L) of fuel per hour. The J85-21 variant added a stage ahead of the base 8-stage compressor for a total of 9 stages, improving thrust. The engine, depending upon additional equipment and specific model, weighs from 300 to 500 pounds (140 to 230 kg). Function: view, File: /home/ah0ejbmyowku/public_html/index.php The basic engine design is quite small, about 18 inches (46 cm) in diameter, and 45 inches (110 cm) long. Among them was another aft-fan design, the General Electric CF700 used in the Dassault Falcon 20 business jet, which was developed from the General Electric J85 in the same way as the J79 was adapted to the 805. The company began with its single-engine Northrop N-102 Fang concept.The N-102 was facing weight and cost growth, so the project was canceled and the company N-156 project was begun. Military versions produce up to 2,950 lbf of thrust dry; afterburning variants can reach up to 5,000 lbf . 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. [4], File: /home/ah0ejbmyowku/public_html/application/views/user/popup_modal.php The General Electric J85 is a small single-shaft turbojet engine. The United States Air Force plans to continue using the J85 in aircraft through 2040. The first version of the aircraft entered service in 1959 as the T2J-1. The General Electric J85 is a small single-shaft turbojet engine. Line: 315 General Electric CJ610. The fan blades are an extension of the low-pressure turbine blades. More recently, J85s have powered the Scaled Composites White Knight aircraft, the carrier for the Scaled Composites SpaceShipOne spacecraft, and the Me 262 Project. With more than 75 million flight hours experience on military and commercial models, the J85 offers the highest thrust-to-weight ratio of any production engine in its class in the free world. 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). Line: 479 Message: Undefined variable: user_membership, File: /home/ah0ejbmyowku/public_html/application/views/user/popup_modal.php The model has logged over 16.5 million hours of operation. V závislosti na doplÅkovém vybavení a konkrétním modelu motor váží od 140 do 230 kg. The General Electric F404 and F412 are a family of afterburning turbofan engines in the 10,500â19,000 lbf (47â85 kN) class (static thrust).The series are produced by GE Aviation.Partners include Volvo Aero, which builds the RM12 variant. Vojenské verze poskytují "na sucho" tah 13,1 kN, zatímco varianty s pÅídavným spalováním dosahují až 22 kN. The engine, depending upon additional equipment and specific model, weighs from 300 to 500 pounds (140 to 230 kg). The engine, depending upon additional equipment and specific model, weighs from 300 to 500 pounds . [2] 1892ë ì ì¤ë¦½ë ì¸ê³ ìµëì ì 기ìë¹ê¸°êµ¬ ì ì¡°ì¬ìë íì¬. The J85 was originally designed to power a large decoy missile, the McDonnell ADM-20 Quail. [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 General Electric J85 is a small single-shaft turbojet engine. They are selling it to recover funds and storage space. The J85-GE-5 is rated at 2,680 pounds of thrust (11.921 kilonewtons), and ⦠General Electric GE90 ì ëë´ ì¼ë í¸ë¦ìì ê°ë°í í°ë³´í¬ ì í¸ ìì§ì´ë¤. Today, there are over 560 CJ610-powered aircraft in operation around the world, with an experience base of ⦠The engine was presented at a defense exhibition on 22 August 2016. the owj engine has a dry thrust of 3,500 lbf (16 kN). 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 General Electric J85 is a small single-shaft turbojet engine. The General Electric J85 is a small single-shaft turbojet engine. The two-seat trainer was powered by one Westinghouse J34-WE-46/48 turbojet. It seems the other pages don't have a clear one-way-or-the-other. From Wikipedia, the free encyclopedia 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 J85 augmented turbojet is a powerplant for high performance trainers and tactical 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). [2], The Iranian Ministry of Defense constructed a new engine based on the General Electric J85 named "OWJ". This mission demanded a small engine that could nevertheless provide enough power to keep up with the jet bomber. It was developed in two versions. The success of GE's J85 fighter engine led to the development of the CJ610 for commercial use. It was a civilian version of the J79 and differed only in detail. 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). This is an audio version of the Wikipedia Article:https://en.wikipedia.org/wiki/General_Electric_J8500:01:03 1 Design and development00:03:35 1.1 ⦠[26] Their fan technology was also used in the XV-5 Vertifan. Several variants were produced. [27] The aircraft was subsequently redesigned, and the single engine was replaced with two Pratt & Whitney J60-P-6 turbojets in the T-2B. [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. One new build prototype and 29 conversions from Sk 60A.
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