General_Electric_CJ610

General Electric CJ610

General Electric CJ610

Turbojet engine


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.

Quick Facts CJ610, Type ...

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

Early 1121 Jet Commanders are powered by thin CJ610 turbojets

Other

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

See also

Related development

Comparable engines

Related lists


References

  1. Gunston, 2006. P. 308
  2. The "c" suffix stands for the flyable reproductions equipped with the J85-derived CJ610 engine instead of the original Junkers Jumo 004 jet engine.
  3. Taylor 1972, pp. 712-713.

Bibliography

  • Gunston, Bill (2006). World Encyclopedia of Aero Engines, 5th Edition. Phoenix Mill, Gloucestershire, England, UK: Sutton Publishing Limited. ISBN 0-7509-4479-X.
  • Taylor, John W. R. (1972). Jane's all the world's aircraft. 1972-73: 63rd year. London: Jane's Yearbooks. ISBN 0-354-00109-4. OCLC 655668894.

Share this article:

This article uses material from the Wikipedia article General_Electric_CJ610, and is written by contributors. Text is available under a CC BY-SA 4.0 International License; additional terms may apply. Images, videos and audio are available under their respective licenses.