Wednesday, August 20, 2008

F402

Total Production: 1,100

F402-RR-408

IOC: 1990

Also Known As: F402-RR-408A, Pegasus, Pegasus Mk107

Origin:United Kingdom

Contractor/s: Rolls-Royce

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 23,800 lb (10,796 kg)

Family Members:
F402-RR-406A Related Equipment
Derived from: F402-RR-406A

Applications
AV-8B Harrier II, AV-8B Harrier II Plus, Harrier Gr9 News
EADS to Upgrade Four Harrier AV-8B for the Spanish Navy

BAe Awarded Harrier Upgrade Contract

Operators

see operators map | see family operators map

Italy

Spain

United Kingdom

United States of America

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: Monday, August 18, 2008

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