JT3C-6 is a turbojet engine model used in aircraft.
Engine Family: turbojet
Dry weight: 1921 kilogram
Fan diameter: 0.97 metre
HP compressor stages: 7
HP turbine stages: 1
LP compressor stages: 9
LP turbine stages: 2
Length: 3.52 metre
Max. continuous thrust: 44.48 kilonewton
Max. takeoff thrust: 49.82 kilonewton
Max. takeoff thrust (wet): 57.83 kilonewton
Water injection:
N1 RPM: 6195
N2 RPM: 9980
ICAO: B701
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