F101-GE-102  
Initial Operational Capability (IOC):
Total Production: ?
Origin: United States of America
Corporations: General Electric
Parent System: F101
Initial Operational Capability (IOC): 1970
Total Production: ?
Family Members: F101
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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.

F101-GE-102 Applications


Combat Aircraft B-1B Lancer

F101-GE-102 Specifications

Dimensions
Fan Diameter: 1,400 millimeter (55 inch)
Length: 4.60 meter (181 inch)
Weight
Dry Weight: 1,996 kilogram (4,400 pound)
Thrust: 30,000 pound (13.6 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)

Operators & Related Equipment


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