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F100
IOC: 1974
Total Production: 7,179
F100-PW-220
IOC: 1984
Origin
United States of America
Contractor/s
United Technologies
Applications
F-15C Eagle
F-15D Eagle
F-16C Block 32
F-16C Block 42
F-16D Block 32
F-16D Block 42
X-47B
Family Members
F100-PW-100
F100-PW-220E
F100-PW-229
F100-PW-232
Derived from:
F100-PW-100
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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 F100-PW-220 engine was more dependable, lighter and smarter than -100 engine. However, in terms of thrust it was less capable than GE's F110 models.
The -220 engines were supplied to F-16C/D fighters produced from 1984 until 1991. F-15C/D fighters were also powered by F100-PW-220 engines.
Specifications
Engine/s Performance: Thrust 23,840 lb (10,814 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: Saturday, November 22, 2008
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