F100
IOC: 1974
Total Production: 7,221
F100-PW-100
Origin
United States of America
Contractor/s
United Technologies
Applications
F-15A Eagle
F-15B Eagle
F-16A Fighting Falcon
F-16B Fighting Falcon
F100-PW-220
F100-PW-220E
F100-PW-229
F100-PW-232
Family Members
F100-PW-220
F100-PW-220E
F100-PW-220U
F100-PW-229
F100-PW-232
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Description:
The F100 engine was developed to power the twin-engine F-15 Eagle air defense fighter. Subsequently it was adopted by the F-16 Fighting Falcon multipurpose fighter.
The initial F100 engine variant, F100-PW-100, powered the F-15A/B fighter and F-16A/B models.
Specifications
Engine/s Performance: Thrust 23,830 lb (10,809 kg)
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Notes
(*) lead contractor
IOC: Initial Operating Capability
FOC: Full Operating Capability
CEP: Circular Error Probable
Comm: Commissioning Date
Meters (m) Kilometers (km) Nautic Miles (nm) Inch (in) Yard (yd) Foot (ft) Millimeter (mm)
Pound (lb) Kilogram (kg) kN (KiloNewton) Ton (t)
Meters per Second (mps) Kilometers per Hour (kph) Knot (kt) Miles per Hour (mph)
Liter (l) Galon (gl)
Year (yr) Minutes (min) Second (sec)
Shaft-Horse-Power (shp)
Last Updated: Sunday, March 07, 2010
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