F135-PW-100 is a turbofan engine model used in aircraft.
Engine Family: turbofan
Overall pressure ratio: 28
Bypass ratio: 0.56
Afterburner:
Dry weight: 1701 kilogram
Fan stages: 3
HP compressor stages: 6
HP turbine stages: 1
LP turbine stages: 2
Length: 5.59 metre
Max. continuous thrust: 128.1 kilonewton
Max. takeoff thrust: 191.3 kilonewton
