There is 1 images added on 20 July 2008
F101  
Initial Operational Capability (IOC): 1970
Total Production: ?
Origin: United States of America
Corporations: General Electric
Parent System: F101
Initial Operational Capability (IOC): 1970
Total Production: ?
Family Members: F101-GE-102
Reviews
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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.

F101 Applications


Propulsion Systems CFM56-2 F110-GE-100 F110-GE-400 F118-GE-100 F118-GE-101

F101 Specifications

Dimensions
Fan Diameter: 1,400 millimeter (55 inch)
Length: 4.60 meter (181 inch)
Weight
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)

F101 News

There is 1 news
on 30 Apr 2008
Wednesday, April 30, 2008Synthetic Fuel Testing Begins on Fighter Engine

Operators & Related Equipment


OperatorsItems

Grand Total ?1
 
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