F135-PW-100

Engine model
Military
Manufacturer Pratt & Whitney
Engine type Turbofan

Technical specifications

Design
Afterburner Yes
Fan stages
3
HP compressor stages
6
HP turbine stages
1
LP turbine stages
2
Dimensions
Length
5.59 m
18.34 ft
Performance
Bypass ratio
0.56:1
Pressure ratio
28:1
Thrust limits
Max. continuous thrust
128.1 kN
28,800 lbf
Max. takeoff thrust
191.3 kN
43,010 lbf
Weights
Dry weight
1,701 kg
3,750 lb