Wednesday, December 03, 2008

F101

IOC: 1970

F101-GE-102

Origin
United States of America

Contractor/s
General Electric

Applications
B-1B Lancer

Family Members
F101

Description: The F101 engine was developed to power the B-1B Lancer Strategic Bomber. F101-GE-102 provides outstanding thrust performance, low fuel consumption in a robust, compact design.

Specifications
Dimensions: Diameter 1,400 mm, Length 4.6 m

Weights: Max Weight 1,996 kg (4,400 lb)

Engine/s Performance: Thrust 30,000 lb (13,608 kg)

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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