Monday, October 06, 2008

F101

IOC: 1970

Origin:United States of America

Contractor/s: General Electric

Description: The F101 engine was developed to power the B-1B Lancer Strategic Bomber. Jointly with its aerodynamics, the F101 are the keys of Lancer's supersonic low-level flight profile.

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

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

Family Members:
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Operators

United States of America

Image Gallery

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: Sunday, September 28, 2008

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