Initial Operational Capability (IOC):
Also Known As: F100U
Origin: United States of America
Pratt & Whitney
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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-220U is a derivative of the F-100-PW-220E engine capable of providing up to 16,000 pounds of thrust while operating in a maritime environment, including carrier deck operations. The -220U engine has been designed for integration onto the X-47B unmanned combat air vehicle (UCAV). Its first flight is scheduled in 2009, with at-sea carrier trials planned to begin in late 2011.
Thrust: 16,000 pound (7.26 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
14 Jul 2008 and 7 Jan 2009
Operators & Related Equipment
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