There is 1 images added on 16 September 2019
F130  
Initial Operational Capability (IOC): 2022
Total Production: ?
Origin: United Kingdom
Corporations: Rolls-Royce
Parent System: BR700
Initial Operational Capability (IOC): 1997
Total Production: 2,400
Family Members: BR710, BR715 and BR725
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Description: The F130 engine is a derivative of the BR725 commercial turbofan engine developed to power the US Air Force B-52 bomber fleet under the Commercial Engine Replacement Program. The F130 engine is rated at 17,000 pound and each bomber would get eight such engines. The new engine was completing testing in late 2019 and is expected to be ready for integration and deployment powering the B-52 aircraft in the early 2020s.

F130 Specifications

Weight
Max Takeoff Thrust: 17,000 pound (7,711 kilogram)
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)

F130 News

There is 1 news
on 16 Sep 2019
Monday, September 16, 2019B-52 Bomber F130 Engine Completes Early Testing

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