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.
A development, the CF700 added a rear-mounted fan mounted directly on the free-running low-pressure turbine.
 Specifications (CJ610)
- Type: Turbojet
- Length: 45.4 to 51.1 inches (1.15 - 1.30 m) (depending on accessory equipment installed)
- Diameter: 17.7 inches (0.45 m)
- Dry weight: 396 - 421 pounds (180 - 191 kg)(depending on accessory equipment installed)
- Compressor: 8-stage axial flow
- Turbine: 2-stage
 See also
- Related development
- Related lists
- Gunston, Bill (2006). World Encyclopedia of Aero Engines, 5th Edition. Phoenix Mill, Gloucestershire, England, UK: Sutton Publishing Limited. ISBN 0-7509-4479-X.
 External links