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Aeroplane engine, used British & French prototypes of Concorde

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Postcard of Aeroplane engine, used British & French prototypes of Concorde.
000-190-004-360-C
© National Museums Scotland

Aeroplane engine, used British & French prototypes of Concorde

This turbojet aero engine, the Olympus 593, was made in 1969 by the Bristol Siddeley Engine Division of Rolls-Royce Ltd. It was used in both the British and French prototypes of Concorde between 1969 and 1973.

The engine is an axial flow gas turbine: the air drawn through the compression stages into the combustion chamber flows along the engine's longitudinal axis. (Axial flow engines are generally more complex and have more moving parts but a greater power output.) The engine's nameplate is marked 'BRISTOL OLYMPUS 593 ENGINE-MOTEUR, MARK 593B, SERIAL 59367, MIN'.

The Olympus engine was originally designed for the subsonic Avro Vulcan as the Olympus 101 in 1956 but was chosen for extensive development for a low altitude supersonic role for the British Aircraft Corporation TSR.2. The modified powerplant proved troublesome and not all the faults were cured before cancellation of TSR.2 in 1965. Further development resulted in the Olympus 593, the world's first fully certified engine for commercial supersonic operation.


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Online ID: 000-190-004-360-C
Image Rights Holder: National Museums Scotland
Project: 0098: National Museums Scotland
Project description | View all records in project
Ref: National Museums Scotland  T.1976.56
Date: 1969
Material: Inscription: BRISTOL OLYMPUS 593 ENGINE-MOTEUR, MARK 593B, SERIAL 59367, MIN
Dimensions: 156.00" x 52.00" D
What: Jet aero-engine / turbojet engine
Subject: 1. AERONAUTICS, Jet engines and turboprops (Departmental Classification)
Who: Concorde (Used in prototypes)
Rolls-Royce, Bristol (Maker)
Where: England, Gloucestershire, Bristol
Event:
Description: Axial flow turbot jet engine, the Olympus, by Rolls-Royce (Bristol), which was used in both the British and French prototypes of Concorde during 1969 - 1973
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