Wednesday, December 03, 2008

Adour

Total Production: 2,600

Adour Mk951

IOC: 2005

Also Known As
Adour 951

Origin
France
United Kingdom

Contractor/s
Rolls-Royce
Snecma

Applications
Hawk

Family Members
Adour Mk102
Adour Mk104
Adour Mk871
F405-RR-401

Description: The Adour is a family of turbofan engines developed in conjunction between Rolls-Royce and Turbomeca. These engines are available with or without afterburner. They were selected to power Jaguar, Hawk, T-45 Goshawk, Mitsubishi F-1 and T-2 aircraft.

The Adour Mk951 engine has been developed to power the latest variants of Hawk 100/200 aircraft. Adour 951 delivers 6,500 pounds of thrust and features 4,000 hours Time Between Overhaul and dual Full Authority Digital Engine Control (FADEC).

Specifications
Dimensions: Diameter 580 mm, Length 1,960 mm

Weights: Max Weight 610 kg (1,345 lb)

Engine/s Performance: Thrust 6,500 lb (2,948 kg)

Operators

see operators map | see family operators map

Bahrain

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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