F402-RR-408  
Initial Operational Capability (IOC): 1990
Total Production: ?
Also Known As: F402-RR-408A, Pegasus and Pegasus Mk107
Origin: United Kingdom
Corporations: Rolls-Royce
Parent System: F402
Initial Operational Capability (IOC):
Total Production: 1,100
Family Members: F402-RR-406A
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Description: The F402 Pegasus engine was developed to meet the requirements of a Vertical or Short Take Off and Landing aircraft designated Harrier. Pegasus has swiveling nozzles to achieve Thrust Vector Control. Pegasus has powered all Harrier variants produced all over the world.

F402-RR-408 Applications


Combat Aircraft AV-8B Harrier II AV-8B Harrier II Plus Harrier Gr9

F402-RR-408 Specifications

Weight
Thrust: 23,800 pound (10.8 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)

F402-RR-408 News

There are 4 news between
23 Jan 2003 and 7 Feb 2011
Monday, February 7, 2011Spanish Navy Modernized Harrier Prototype Completes Test Flights
Wednesday, January 28, 2009UK MoD Awards Contract to Rolls-Royce for Pegasus Engine Support
Wednesday, June 11, 2008EADS to Upgrade Four Harrier AV-8B for the Spanish Navy
Thursday, January 23, 2003BAe Awarded Harrier Upgrade Contract

Operators & Related Equipment


OperatorsItems

Grand Total ?4
 
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