General Electric CJ610

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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.

[edit] Aircraft used on

[edit] Specifications

  • Compressor stages: 8t
  • Turbine stages: 2
  • Maximum diameter: 17.7 inches
  • Length: 45.4 to 51.1 inches (depending on accessory equipment installed)
  • Dry weight: 396 - 421 pounds (depending on accessory equipment installed)
  • Max power specific fuel consumption: 0.96 - 0.97
  • Max power at sea level: 2850 - 3100 lb/thrust

[edit] References


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