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Rolls-Royce/Turbomeca Adour

The Engine  Specifications (Mk 871)
The Rolls-Royce/Turbomeca Adour was designed to meet the requirements of ground attack and advanced training aircraft, with and without afterburning.

First flown in 1968, over 2,800 engines have been sold with more than 7 million flying hours accumulated (3/31/06).

The U.S. military designation for this engine is the F405-RR-401.

Two shaft
Bypass ratio: 0.8
Compressor: 2-stage LP, 5-stage HP
Turbine: 1-stage LP, 1-stage HP
Pressure ratio: 11
 Models  Used by
Adour Mk 151: 5,200 lb (23.1 kN) thrust 
British Aerospace Hawk
Mitsubishi F-1/T-2
 Related Pages
More about Rolls-Royce
More about Turbomeca

page updated 27 March 2006



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Kenneth W Shanaberger 2000 - 2010