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- Rolls-Royce_Olympus abstract "The Rolls-Royce Olympus (originally the Bristol B.E.10 Olympus) was the world's first two-spool axial-flow turbojet aircraft engine, originally developed and produced by Bristol Aero Engines. First running in 1950, its initial use was as the powerplant of the Avro Vulcan V bomber. The design was further developed for supersonic performance as part of the BAC TSR-2 programme. Later it saw production as the Rolls-Royce/Snecma Olympus 593, the powerplant for Concorde SST. Versions of the engine were licenced to Curtiss-Wright in the USA as the TJ-32 or J67 (military designation) and the TJ-38 'Zephyr'. The Olympus was also developed with success as a marine and industrial gas turbine.Bristol Aero Engines (formerly Bristol Engine Company) merged with Armstrong Siddeley Motors in 1959 to form Bristol Siddeley Engines Limited (BSEL) which in turn was taken over by Rolls-Royce in 1966.As of 2012, the Olympus remains in service as both a marine and industrial gas turbine. It also powers the restored Avro Vulcan XH558.".
- Rolls-Royce_Olympus wikiPageExternalLink www.bristolaero.com.
- Rolls-Royce_Olympus wikiPageExternalLink Bristol%20Olympus%20301.JPG.
- Rolls-Royce_Olympus wikiPageExternalLink bristol-olympus-mk12a-cutaway.jpg.
- Rolls-Royce_Olympus wikiPageExternalLink 1958%20-%200289.html?tracked=1.
- Rolls-Royce_Olympus wikiPageExternalLink 1961%20-%200233.html.
- Rolls-Royce_Olympus wikiPageExternalLink www.gatwick-aviation-museum.co.uk.
- Rolls-Royce_Olympus wikiPageExternalLink heritagetrust.
- Rolls-Royce_Olympus wikiPageExternalLink www.turbine-support.com.
- Rolls-Royce_Olympus wikiPageExternalLink www.yorkshireairmuseum.org.
- Rolls-Royce_Olympus wikiPageID "574580".
- Rolls-Royce_Olympus wikiPageRevisionID "594316741".
- Rolls-Royce_Olympus combustion "Cannular 10 flame tubes".
- Rolls-Royce_Olympus compressor "Axial 6 LP pressure stages, 8 HP stages".
- Rolls-Royce_Olympus developedInto Snecma_Olympus_593.
- Rolls-Royce_Olympus firstRun "1950".
- Rolls-Royce_Olympus fueltype "AVTUR or AVTAG".
- Rolls-Royce_Olympus hasPhotoCollection Rolls-Royce_Olympus.
- Rolls-Royce_Olympus lists "* List of aircraft engines".
- Rolls-Royce_Olympus majorApplications Avro_Vulcan.
- Rolls-Royce_Olympus majorApplications Concorde.
- Rolls-Royce_Olympus manufacturer Bristol_Aeroplane_Company.
- Rolls-Royce_Olympus manufacturer Bristol_Siddeley.
- Rolls-Royce_Olympus manufacturer Rolls-Royce_Limited.
- Rolls-Royce_Olympus nationalOrigin United_Kingdom.
- Rolls-Royce_Olympus weight "3.04".
- Rolls-Royce_Olympus ref "The Operational Olympus Flight and Lecture Notes, Vulcan Bristol Aero Engine School".
- Rolls-Royce_Olympus related "* Bristol Siddeley BS100".
- Rolls-Royce_Olympus similarEngines "* Pratt & Whitney J75".
- Rolls-Royce_Olympus state "collapsed".
- Rolls-Royce_Olympus title "Articles and topics related to Rolls-Royce Olympus".
- Rolls-Royce_Olympus turbine "HP single stage, LP single stage".
- Rolls-Royce_Olympus type Turbojet.
- Rolls-Royce_Olympus type "Axial flow two-spool turbojet".
- Rolls-Royce_Olympus subject Category:Bristol_Siddeley_aircraft_engines.
- Rolls-Royce_Olympus subject Category:Rolls-Royce_aircraft_gas_turbine_engines.
- Rolls-Royce_Olympus subject Category:Turbojet_engines_1950–1959.
- Rolls-Royce_Olympus type AircraftEngine102687423.
- Rolls-Royce_Olympus type Artifact100021939.
- Rolls-Royce_Olympus type BristolSiddeleyAircraftEngines.
- Rolls-Royce_Olympus type Device103183080.
- Rolls-Royce_Olympus type Engine103287733.
- Rolls-Royce_Olympus type Instrumentality103575240.
- Rolls-Royce_Olympus type Machine103699975.
- Rolls-Royce_Olympus type Motor103789946.
- Rolls-Royce_Olympus type Object100002684.
- Rolls-Royce_Olympus type PhysicalEntity100001930.
- Rolls-Royce_Olympus type Rolls-RoyceAircraftGasTurbineEngines.
- Rolls-Royce_Olympus type Whole100003553.
- Rolls-Royce_Olympus comment "The Rolls-Royce Olympus (originally the Bristol B.E.10 Olympus) was the world's first two-spool axial-flow turbojet aircraft engine, originally developed and produced by Bristol Aero Engines. First running in 1950, its initial use was as the powerplant of the Avro Vulcan V bomber. The design was further developed for supersonic performance as part of the BAC TSR-2 programme. Later it saw production as the Rolls-Royce/Snecma Olympus 593, the powerplant for Concorde SST.".
- Rolls-Royce_Olympus label "Rolls-Royce Olympus".
- Rolls-Royce_Olympus label "Rolls-Royce Olympus".
- Rolls-Royce_Olympus label "Rolls-Royce Olympus".
- Rolls-Royce_Olympus label "Rolls-Royce Olympus".
- Rolls-Royce_Olympus label "Rolls-Royce Olympus".
- Rolls-Royce_Olympus label "ロールス・ロイス オリンパス".
- Rolls-Royce_Olympus sameAs Rolls-Royce_Olympus.
- Rolls-Royce_Olympus sameAs Rolls-Royce_Olympus.
- Rolls-Royce_Olympus sameAs Rolls-Royce_Olympus.
- Rolls-Royce_Olympus sameAs Rolls-Royce_Olympus.
- Rolls-Royce_Olympus sameAs ロールス・ロイス_オリンパス.
- Rolls-Royce_Olympus sameAs m.02rkp1.
- Rolls-Royce_Olympus sameAs Q1784919.
- Rolls-Royce_Olympus sameAs Q1784919.
- Rolls-Royce_Olympus sameAs Rolls-Royce_Olympus.
- Rolls-Royce_Olympus wasDerivedFrom Rolls-Royce_Olympus?oldid=594316741.
- Rolls-Royce_Olympus isPrimaryTopicOf Rolls-Royce_Olympus.