F402-RR-406A  
Initial Operational Capability (IOC):
Total Production: 1,100
Also Known As: Pegasus and Pegasus Mk105
Origin: United Kingdom
Corporations: Rolls-Royce
Parent System: F402
Initial Operational Capability (IOC):
Total Production: 1,100
Family Members: F402-RR-408
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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-406A Applications


Combat Aircraft Sea Harrier F/A.2 Propulsion Systems F402-RR-408

F402-RR-406A Specifications

Weight
Thrust: 21,750 pound (9.87 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


OperatorsItems

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