JT3C-4 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: 42.26 kilonewton
Max. takeoff thrust: 49.82 kilonewton
Max. takeoff thrust (wet): 55.6 kilonewton
N1 RPM: 6195
N2 RPM: 9980
Water injection:
