Initial Operational Capability (IOC):
Total Production: ?
Origin: United States of America
Corporations: General Electric Aviation
Parent System: F118
Initial Operational Capability (IOC):
Total Production: ?
Family Members: F118-GE-100
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Description: The F118 was developed utilizing the same core design of the F101 engine. The F118 has different fan and afterburner packages to tailor engine performance compared with the F101.

The F118-GE-101 has been designed to re-engine the U-2R high-altitude reconnaissance aircraft, U-2R with -101 engines are designated U-2S. The -101 engine increases U-2's ceiling, range, safety and ease of flight.

F118-GE-101 Applications

Support Aircraft U-2S Dragon Lady

F118-GE-101 Specifications

Fan Diameter: 1,190 millimeter (47 inch)
Length: 2.79 meter (110 inch)
Dry Weight: 1,429 kilogram (3,150 pound)
Thrust: 17,000 pound (7.71 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)
Shaft-Horse-Power (shp)

F118-GE-101 News

There is 1 news
on 22 Jan 2008
Tuesday, January 22, 2008Kelly Aviation Center to Continue with U-2 Dragon Lady Support

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