General Electric CJ610
(Redirected from General Electric CJ-610)
Template:Infobox Aircraft Engine
File:Aero Commander 1121 Jet Commander, Private JP5962515.jpgEarly 1121 Jet Commanders are powered by thin CJ610 turbojets
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. Civilian versions have powered business jets such as the Learjet 23 and the Hamburger Flugzeugbau HFB 320 Hansa Jet. The engines are also used in the flyable Messerschmitt Me 262 reproductions built by the Me 262 Project in the United States.
A development, the CF700, added a rear-mounted fan mounted directly on the free-running low-pressure turbine.
Variants
- CJ610-1
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- CJ610-2B
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- CJ610-4
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- CJ610-6
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- CJ610-8A
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- CJ610-9
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Applications
- Aero Commander 1121 Jet Commander
- Boom XB-1
- HFB 320 Hansa Jet
- Learjet 23
- Learjet 24
- Learjet 25
- Learjet 28
- Margański & Mysłowski EM-10 Bielik
- Messerschmitt Me 262 replicas A-1c and B-1c.[1][2]
- Transall C-160 (APU)
- Viper Aircraft Viperjet MKII
Other
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- Yak 110Script error: No such module "Unsubst".
Specifications (CJ610-9)
Data from Jane's All the World's Aircraft 1972-73.[3]
General characteristics
- Type: Turbojet
- Length: Template:Convert
- Diameter: Template:Convert
- Dry weight: Template:Convert
Components
- Compressor: 8-stage axial flow
- Combustors: Annular combustion chamber
- Turbine: 2-stage
Performance
- Maximum thrust: Template:Convert (takeoff)
- Specific fuel consumption: 0.98 lb/(lbf·hr)
- Thrust-to-weight ratio: 7.4
See also
Related development
Comparable engines
Related lists
References
Bibliography
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External links
Template:GE aeroengines Template:Aeroengine-specs
- ↑ Gunston, 2006. P. 308
- ↑ The "c" suffix stands for the flyable reproductions equipped with the J85-derived CJ610 engine instead of the original Junkers Jumo 004 jet engine.
- ↑ Taylor 1972, pp. 712-713.