General Electric CJ610
Turbojet engine
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 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.
| CJ610 | |
|---|---|
| The CJ610 is derived from the military J85, pictured | |
| Type | Turbojet |
| National origin | United States |
| Manufacturer | General Electric |
| First run | 1960s |
| Major applications | Learjet 23 Learjet 24 Learjet 25 Learjet 28 Aero Commander 1121 HFB 320 Hansa Jet |
| Developed from | General Electric J85 |
| Developed into | General Electric CF700 |
A development, the CF700, added a rear-mounted fan mounted directly on the free-running low-pressure turbine.
Variants
- CJ610-1
- 2,850 lbf (12.7 kN) thrust
- CJ610-2B
- 2,400 lbf (11 kN) thrust
- CJ610-4
- 2,850 lbf (12.7 kN) thrust
- CJ610-6
- 2,950 lbf (13.1 kN) thrust
- CJ610-8A
- 2,950 lbf (13.1 kN) thrust
- CJ610-9
- 3,100 lbf (14 kN) thrust
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
- Screaming Sasquatch Jet Waco Biplane[citation needed]
- Yak 110[citation needed]
Specifications (CJ610-9)
Data from Jane's All the World's Aircraft 1972-73.[3]
General characteristics
- Type: Turbojet
- Length: 51.1 in (1.30 m)
- Diameter: 17.7 in (0.45 m)
- Dry weight: 417 lb (189 kg)
Components
- Compressor: 8-stage axial flow
- Combustors: Annular combustion chamber
- Turbine: 2-stage
Performance
- Maximum thrust: 3,100 lbf (14 kN) (takeoff)
- Specific fuel consumption: 0.98 lb/(lbf·hr)
- Thrust-to-weight ratio: 7.4
See also
Related development
Comparable engines
Related lists
