Wednesday, December 03, 2008

F100

IOC: 1974
Total Production: 7,179

F100-PW-232

IOC: 2002

Origin
United States of America

Contractor/s
United Technologies

Family Members
F100-PW-100
F100-PW-220
F100-PW-220E
F100-PW-229

Derived from:
F100-PW-100

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-232 engine is the latest and most powerful derivative of the F100 engine. The -232 engine features a larger and more efficient fan. This engine draws heavily up the technology of the F119 engine.

Specifications
Dimensions: Diameter 1,180 mm, Length 4.8 m

Weights: Max Weight 1,860 kg (4,101 lb)

Engine/s Performance: Thrust 32,500 lb (14,742 kg)

News
Pratt & Whitney and Derco Aerospace Sign Agreement for Supply Chain Management

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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