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  2. Rolls-Royce Olympus variants - Wikipedia

    en.wikipedia.org/wiki/Rolls-Royce_Olympus_variants

    The Rolls-Royce Olympus turbojet engine was developed extensively throughout its production run, the many variants can be described as belonging to four main groups. Initial non-afterburning variants were designed and produced by Bristol Aero Engines and Bristol Siddeley (BSEL) and powered the Avro Vulcan .

  3. Rolls-Royce Olympus - Wikipedia

    en.wikipedia.org/wiki/Rolls-Royce_Olympus

    The first reheat variant, the Bristol Siddeley Olympus Mk 320, powered the cancelled BAC TSR-2 supersonic strike aircraft. For Concorde, this was developed during the 1960s into the Rolls-Royce/Snecma Olympus 593, being further developed through several subsequent versions to eventually provide reliable airline service. The Olympus 593 is a ...

  4. Rolls-Royce/Snecma Olympus 593 - Wikipedia

    en.wikipedia.org/wiki/Rolls-Royce/Snecma_Olympus_593

    The Rolls-Royce/Snecma Olympus 593 was an Anglo-French turbojet with reheat, which powered the supersonic airliner Concorde. It was initially a joint project between Bristol Siddeley Engines Limited (BSEL) and Snecma , derived from the Bristol Siddeley Olympus 22R engine.

  5. Rolls-Royce Marine Olympus - Wikipedia

    en.wikipedia.org/wiki/Rolls-Royce_Marine_Olympus

    Data from Rolls-Royce Heritage Trust General characteristics Type: Gas generator Length: Diameter: Dry weight: Components Compressor: 5-stage LP, 7-stage HP Combustors: 8 chamber, cannular Turbine: Single-stage LP and HP Performance Maximum power output: 28,500 shp (21.4 MW) Specific fuel consumption: 0.47 lb/hp/hr (0.287 kg/KWh) See also Related development Rolls-Royce Olympus References ^ a ...

  6. Category:Rolls-Royce aircraft gas turbine engines - Wikipedia

    en.wikipedia.org/wiki/Category:Rolls-Royce...

    Pages in category "Rolls-Royce aircraft gas turbine engines" ... Rolls-Royce Olympus; Rolls-Royce Olympus variants; P. Rolls-Royce Pegasus; R. Rolls-Royce RB.108;

  7. Gordon Lewis (engineer) - Wikipedia

    en.wikipedia.org/wiki/Gordon_Lewis_(engineer)

    In 1946 he was entrusted with the design of the Olympus engine, which performed flawlessly on its very first test bed run, largely as a result of the discipline that Gordon Lewis brought to its design. [See Pegasus The Heart of the Harrier, by Andrew Dow.] The Olympus was later developed to power the Avro Vulcan, TSR-2 and Concorde.

  8. Rolls-Royce Conway - Wikipedia

    en.wikipedia.org/wiki/Rolls-Royce_Conway

    Rolls-Royce responded by designing an even larger model of the Conway, the 16,500 pounds-force (73,000 N) RCo.10 and offering the similar military-rated RCo.11 for the Victor. The new engine differed from the RCo.8 in having a new "zeroth stage" at the front of the low-pressure compressor, further increasing cold airflow around the engine.

  9. Category:Bristol Siddeley aircraft engines - Wikipedia

    en.wikipedia.org/wiki/Category:Bristol_Siddeley...

    Rolls-Royce Olympus; Rolls-Royce Olympus variants; Bristol Siddeley Orpheus; P. Rolls-Royce Pegasus; V. Armstrong Siddeley Viper

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