Adour Mk871  
Initial Operational Capability (IOC):
Total Production: ?
Unitary Cost: GBP£3.5 million   (USD$4.3 million)
Also Known As: Adour 871 and Adour Mk 821
Origin: France and United Kingdom
Corporations: Rolls-Royce and Snecma
Parent System: Adour
Initial Operational Capability (IOC):
Total Production: 2,600
Family Members: Adour Mk102, Adour Mk104, Adour Mk951 and F405-RR-401
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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.

Adour Mk871 Applications

Combat Aircraft Hawk

Adour Mk871 Specifications

Fan Diameter: 570 millimeter (22.4 inch)
Length: 1,960 millimeter (77 inch)
Dry Weight: 589 kilogram (1,299 pound)
Thrust: 6,000 pound (2.72 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)

Adour Mk871 News

There are 3 news between
13 May 2009 and 28 Jul 2010
Wednesday, July 28, 2010Rolls-Royce Awarded Contract for Adour Mk871 Engines to Power 57 Indian Hawk Trainers
Tuesday, June 16, 2009Adour MK 821 Engine Fits for Indian Air Force Jaguar Requirement
Wednesday, May 13, 2009Rolls-Royce to Support Malaysian Air Force Adour Engines

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