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EngineTurbojet with reheat

Rolls-Royce/Snecma Olympus 593

The Rolls-Royce/Snecma Olympus 593 was the turbojet powerplant of Concorde. Four engines powered each aircraft, combining normal jet operation with reheat for take-off and acceleration into supersonic flight. British…

Reviewed September 13, 20264 sources2 min readLast edited by aviation.wiki

The Rolls-Royce/Snecma Olympus 593 was the turbojet powerplant of Concorde. Four engines powered each aircraft, combining normal jet operation with reheat for take-off and acceleration into supersonic flight. British Airways gives approximately 38,000 lbf of thrust per engine with reheat, a rating that should not be confused with unaugmented cruise thrust.[1]Celebrating ConcordeBritish Airways · hotline.britishairways.com · Accessed 2026-09-13Open source details

Development programme

The powerplant was developed in close association with Concorde's supersonic flight programme. A 1971 technical paper by P. H. Calder describes the two prototype aircraft already flying regularly at Mach 2 over substantial distances. The work reviewed engine performance, intake controls, exhaust systems and compatibility between engine and intake, demonstrating that propulsion development extended beyond the engine core alone.[2]Olympus 593 Powerplant in ConcordeSAE International · saemobilus.sae.org · Accessed 2026-09-13Open source details

Ground and flight testing both contributed to that programme. Safran's historical account includes an Olympus 593 on a noise-test stand at Istres in 1968. That surviving record documents Snecma's involvement in evaluating the engine during development, before Concorde began carrying fare-paying passengers.[3]The Story of Safran Aircraft Engines – from 1945 to 2005Safran · safran-group.com · Accessed 2026-09-13Open source details

Reheat and aircraft performance

Reheat adds fuel downstream in the engine's exhaust system to obtain additional thrust. British Airways identifies take-off and the transition to supersonic flight as its uses on Concorde. The aircraft subsequently operated at roughly twice the speed of sound, making the propulsion installation's requirements markedly different from those of an ordinary subsonic airliner.[1]Celebrating ConcordeBritish Airways · hotline.britishairways.com · Accessed 2026-09-13Open source details

The engine, intake and exhaust controls were consequently important parts of the overall powerplant. Calder's contemporary paper treats their compatibility as a specific development subject, alongside bench and flight testing. This is why the Olympus 593 is best understood as part of Concorde's integrated propulsion installation rather than as an isolated thrust-producing component.[2]Olympus 593 Powerplant in ConcordeSAE International · saemobilus.sae.org · Accessed 2026-09-13Open source details

Service and preservation

British Airways began commercial Concorde service to Bahrain on 21 January 1976 and withdrew its scheduled Concorde operation on 24 October 2003. Its history therefore places the Olympus installation within a passenger-service career lasting more than a quarter of a century.[1]Celebrating ConcordeBritish Airways · hotline.britishairways.com · Accessed 2026-09-13Open source details

A preserved Olympus 593 Mark 3B at the Science Museum came from Concorde 002, the British prototype. The museum identifies it as serial number 59351, made around 1969. That provenance is important: a development engine from a prototype illustrates the programme's history, but should not automatically be assigned the specifications of a later production-aircraft engine.[4]Rolls-Royce Olympus 593 Mark 3B aero-engineScience Museum Group · collection.sciencemuseumgroup.org.uk · Accessed 2026-09-13Open source details

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Sources

4 cited
  1. Celebrating Concorde. British Airways. Accessed 9/13/2026Cited 3 times
  2. Olympus 593 Powerplant in Concorde. SAE International. Accessed 9/13/2026Cited 2 times
  3. The Story of Safran Aircraft Engines – from 1945 to 2005. Safran. Accessed 9/13/2026
  4. Rolls-Royce Olympus 593 Mark 3B aero-engine. Science Museum Group. Accessed 9/13/2026

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Last approved September 13, 2026 · Revision 0df82135 · View history