Initial Operational Capability (IOC):
Origin: United States of America
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Description: The F100 engine was developed in the 1970s 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.
Fan Diameter: 1,180 millimeter (46 inch)
Length: 4.84 meter (191 inch)
Dry Weight: 1,860 kilogram (4,101 pound)
Thrust: 32,500 pound (14.7 ton)
CEP: Circular Error Probable
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)
There are 2 news between
19 Jun 2007 and 4 Apr 2018
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