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General Electric CJ610

 

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. First run in the 1960s, 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.

 

Applications:
Aero Commander 1121 Jet Commander
HFB-320 Hansa Jet
Learjet 23
Learjet 24
Learjet 25
Learjet 28
Learjet 29

 

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
Maximum thrust: 2,850 - 3,100 lbf (12.7 - 13.8 kN) at sea level
Specific fuel consumption: 0.96 - 0.97 lb/(lbf·h) ( 27 g/kN·s )

 

 


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