CJ610-1 is a turbojet engine model used in aircraft.
Engine Family: turbojet
Length: 1.03 metre
Dry weight: 183 kilogram
HP turbine stages: 2
HP compressor stages: 8
Max. continuous thrust: 12.01 kilonewton
Max. takeoff thrust: 12.68 kilonewton
ICAO: LJ23
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