Wednesday, December 03, 2008

deagel.com

Adour


Total Production: 2,600

Adour Mk871



Also Known As
Adour 871


Origin
France
United Kingdom


Contractor/s
Rolls-Royce
Snecma

Applications
Hawk

Family Members
Adour Mk102
Adour Mk104
Adour Mk951
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.

Adour Mk871 engine is one of the most outstanding derivatives of Adour turbofan engine family. It powers single-engine Hawk 100/200 aircraft. Originally, it was rated at 5,845 pounds of thrust but the latest 871 engines deliver up to 6,000-lb. Adour Mk871 engines are not provided with afterburner.

Specifications
Dimensions: Diameter 570 mm, Length 1,960 mm

Weights: Max Weight 589 kg (1,299 lb)

Engine/s Performance: Thrust 6,000 lb (2,722 kg)

Operators

see operators map | see family operators map

Australia
Brunei Darussalam
Canada
Finland
India
Indonesia
Kenya
Kuwait
Malaysia
Oman
Saudi Arabia
South Africa
South Korea
Switzerland
United Arab Emirates
United Kingdom
Zimbabwe

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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