Matches in DBpedia 2015-10 for { <http://dbpedia.org/resource/Rolls-Royce/Snecma_Olympus_593> ?p ?o }
- Snecma_Olympus_593 abstract "The Rolls-Royce/Snecma Olympus 593 was an afterburning (reheated) turbojet which powered the supersonic airliner Concorde. It was initially a joint project between Bristol Siddeley Engines Limited (BSEL) and Snecma. It was based on the Bristol Siddeley Olympus 22R engine. Rolls-Royce Limited acquired BSEL in 1966 during development of the engine making BSEL the Bristol Engine Division of Rolls-Royce.Until regular commercial flights by Concorde ceased, the Olympus turbojet was unique in aviation as the only afterburning turbojet powering a commercial aircraft.The overall thermal efficiency of the engine in cruising flight was about 43%, which at the time was the highest figure recorded for any normal thermodynamic machine.".
- Snecma_Olympus_593 thumbnail Concorde_216_(G-BOAF)_last_flight.jpg?width=300.
- Snecma_Olympus_593 wikiPageExternalLink 1965%20-%201043.html.
- Snecma_Olympus_593 wikiPageExternalLink 1966%20-%200080.html.
- Snecma_Olympus_593 wikiPageExternalLink 1969%20-%200422.html.
- Snecma_Olympus_593 wikiPageExternalLink 1971%20-%202820.html.
- Snecma_Olympus_593 wikiPageExternalLink 1972%20-%200438.html.
- Snecma_Olympus_593 wikiPageID "17061942".
- Snecma_Olympus_593 wikiPageLength "20584".
- Snecma_Olympus_593 wikiPageOutDegree "69".
- Snecma_Olympus_593 wikiPageRevisionID "681690851".
- Snecma_Olympus_593 wikiPageWikiLink Afterburner.
- Snecma_Olympus_593 wikiPageWikiLink Afterburner_(engine).
- Snecma_Olympus_593 wikiPageWikiLink André_Edouard_Turcat.
- Snecma_Olympus_593 wikiPageWikiLink André_Turcat.
- Snecma_Olympus_593 wikiPageWikiLink Austin_Executive_Airport.
- Snecma_Olympus_593 wikiPageWikiLink Aviation_museum.
- Snecma_Olympus_593 wikiPageWikiLink Avro_Vulcan.
- Snecma_Olympus_593 wikiPageWikiLink BAC_TSR-2.
- Snecma_Olympus_593 wikiPageWikiLink Bristol.
- Snecma_Olympus_593 wikiPageWikiLink Bristol_Siddeley.
- Snecma_Olympus_593 wikiPageWikiLink British_Aircraft_Corporation.
- Snecma_Olympus_593 wikiPageWikiLink Brooklands_Museum.
- Snecma_Olympus_593 wikiPageWikiLink Category:France–United_Kingdom_relations.
- Snecma_Olympus_593 wikiPageWikiLink Category:Turbojet_engines_1960–1969.
- Snecma_Olympus_593 wikiPageWikiLink Concorde.
- Snecma_Olympus_593 wikiPageWikiLink Fleet_Air_Arm_Museum.
- Snecma_Olympus_593 wikiPageWikiLink France.
- Snecma_Olympus_593 wikiPageWikiLink Horsepower.
- Snecma_Olympus_593 wikiPageWikiLink Imperial_War_Museum_Duxford.
- Snecma_Olympus_593 wikiPageWikiLink Intrepid_Sea,_Air_&_Space_Museum.
- Snecma_Olympus_593 wikiPageWikiLink Kolesov_RD-36-51.
- Snecma_Olympus_593 wikiPageWikiLink Kuznetsov_NK-144.
- Snecma_Olympus_593 wikiPageWikiLink List_of_aircraft_engines.
- Snecma_Olympus_593 wikiPageWikiLink Mach_(speed).
- Snecma_Olympus_593 wikiPageWikiLink Mach_number.
- Snecma_Olympus_593 wikiPageWikiLink Melun_Villaroche_Aerodrome.
- Snecma_Olympus_593 wikiPageWikiLink Museo_del_Concorde.
- Snecma_Olympus_593 wikiPageWikiLink National_Gas_Turbine_Establishment.
- Snecma_Olympus_593 wikiPageWikiLink Nimonic.
- Snecma_Olympus_593 wikiPageWikiLink Overall_pressure_ratio.
- Snecma_Olympus_593 wikiPageWikiLink Patchway.
- Snecma_Olympus_593 wikiPageWikiLink Pratt_&_Whitney_J58.
- Snecma_Olympus_593 wikiPageWikiLink Propelling_nozzle.
- Snecma_Olympus_593 wikiPageWikiLink SNECMA_M45H.
- Snecma_Olympus_593 wikiPageWikiLink Rolls-Royce_Limited.
- Snecma_Olympus_593 wikiPageWikiLink Rolls-Royce_Olympus.
- Snecma_Olympus_593 wikiPageWikiLink Royal_Air_Force_Museum_Cosford.
- Snecma_Olympus_593 wikiPageWikiLink Saclay.
- Snecma_Olympus_593 wikiPageWikiLink Science_Museum,_London.
- Snecma_Olympus_593 wikiPageWikiLink Science_Museum_(London).
- Snecma_Olympus_593 wikiPageWikiLink Sinsheim_Auto_&_Technik_Museum.
- Snecma_Olympus_593 wikiPageWikiLink Snecma.
- Snecma_Olympus_593 wikiPageWikiLink Supercruise.
- Snecma_Olympus_593 wikiPageWikiLink Tu-144.
- Snecma_Olympus_593 wikiPageWikiLink Tupolev_Tu-144.
- Snecma_Olympus_593 wikiPageWikiLink Turbofan.
- Snecma_Olympus_593 wikiPageWikiLink Turbojet.
- Snecma_Olympus_593 wikiPageWikiLink United_Kingdom.
- Snecma_Olympus_593 wikiPageWikiLink University_of_Illinois_at_Urbana-Champaign.
- Snecma_Olympus_593 wikiPageWikiLink University_of_Illinois_at_Urbana–Champaign.
- Snecma_Olympus_593 wikiPageWikiLink Yorkshire_Air_Museum.
- Snecma_Olympus_593 wikiPageWikiLink Île-de-France.
- Snecma_Olympus_593 wikiPageWikiLink File:2001concordewingduxfordJM.jpg.
- Snecma_Olympus_593 wikiPageWikiLink File:Concorde_216_(G-BOAF)_last_flight.jpg.
- Snecma_Olympus_593 wikiPageWikiLink File:Concorde_Ramp.jpg.
- Snecma_Olympus_593 wikiPageWikiLink File:Concordeintake.gif.
- Snecma_Olympus_593 wikiPageWikiLink File:Olympus_593_FAAM_Turbine.JPG.
- Snecma_Olympus_593 wikiPageWikiLinkText "Olympus 593 Mk610".
- Snecma_Olympus_593 wikiPageWikiLinkText "Olympus 593".
- Snecma_Olympus_593 wikiPageWikiLinkText "Olympus".
- Snecma_Olympus_593 wikiPageWikiLinkText "Rolls-Royce/SNECMA Olympus 593".
- Snecma_Olympus_593 wikiPageWikiLinkText "Rolls-Royce/Snecma Olympus 593".
- Snecma_Olympus_593 aircon "186".
- Snecma_Olympus_593 combustion "Nickel alloy construction annular chamber, 16 vapourising burners, each with twin outlets".
- Snecma_Olympus_593 compression "15.5".
- Snecma_Olympus_593 compressor "Axial flow, 7-stage low pressure, 7-stage high pressure".
- Snecma_Olympus_593 developedFrom Rolls-Royce_Olympus.
- Snecma_Olympus_593 diameter "1.212 m".
- Snecma_Olympus_593 firstRun "June".
- Snecma_Olympus_593 fueltype "Jet A1".
- Snecma_Olympus_593 hasPhotoCollection Snecma_Olympus_593.
- Snecma_Olympus_593 length "4.039 m".
- Snecma_Olympus_593 lists "*List of aircraft engines".
- Snecma_Olympus_593 majorApplications Concorde.
- Snecma_Olympus_593 manufacturer Rolls-Royce_Limited.
- Snecma_Olympus_593 manufacturer Snecma.
- Snecma_Olympus_593 nationalOrigin France.
- Snecma_Olympus_593 nationalOrigin United_Kingdom.
- Snecma_Olympus_593 numberBuilt "67".
- Snecma_Olympus_593 ref "Jane's.".
- Snecma_Olympus_593 related "* Rolls-Royce Olympus".
- Snecma_Olympus_593 similarEngines "*Kolesov RD-36-51 *Kuznetsov NK-144 *Pratt & Whitney J58".
- Snecma_Olympus_593 specfuelcon "cruise / sl".
- Snecma_Olympus_593 thrust "wet: 169.2 kN dry: 139.4 kN".
- Snecma_Olympus_593 weight "5.4".
- Snecma_Olympus_593 turbine "High pressure single stage, low pressure single stage".
- Snecma_Olympus_593 type Turbojet.
- Snecma_Olympus_593 weight "3175.0".
- Snecma_Olympus_593 wikiPageUsesTemplate Template:Aircontent.