Wednesday, December 03, 2008

F402

Total Production: 1,100

F402-RR-406A

Also Known As
Pegasus
Pegasus Mk105

Origin
United Kingdom

Contractor/s
Rolls-Royce

Applications
F402-RR-408
Sea Harrier F/A.2

Family Members
F402-RR-408

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.

Specifications
Engine/s Performance: Thrust 21,750 lb (9,866 kg)

Operators

United Kingdom

Notes
(*) lead contractor
IOC: Initial Operating Capability
FOC: Full Operating Capability
CEP: Circular Error Probable
Comm: Commissioning Date
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)

Last Updated: Saturday, November 22, 2008

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