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- Bristol_Theseus abstract "The Theseus was the Bristol Aeroplane Company's first attempt at a gas-turbine engine design, a turboprop that delivered just over 2,000 hp (1,500 kW). A novel feature was the use of a heat exchanger to transfer waste heat from the exhaust to the compressor exit.The engine was soon superseded by the Proteus design with more power, and the only extended use of the engine was in two Handley Page Hermes 5 development aircraft.Following 156 hours of ground runs and the receipt of a test certificate from the Ministry of Supply on 28 January 1947, two Theseus engines were fitted in the outer positions of a four-engined Avro Lincoln for air tests. After ground and taxying test the Lincoln first flew on 17 February 1947.The Theseus was the first propeller turbine (turboprop) engine in the world to pass a type test, doing so in January 1947.".
- Bristol_Theseus wikiPageExternalLink 1945%20-%202384.html.
- Bristol_Theseus wikiPageExternalLink 1950%20-%202036.html.
- Bristol_Theseus wikiPageID "323850".
- Bristol_Theseus wikiPageLength "4416".
- Bristol_Theseus wikiPageOutDegree "16".
- Bristol_Theseus wikiPageRevisionID "681454944".
- Bristol_Theseus wikiPageWikiLink Avro_Lincoln.
- Bristol_Theseus wikiPageWikiLink Avro_Theseus_Lincoln.
- Bristol_Theseus wikiPageWikiLink Bristol_Aeroplane_Company.
- Bristol_Theseus wikiPageWikiLink Bristol_Proteus.
- Bristol_Theseus wikiPageWikiLink Bristol_Siddeley.
- Bristol_Theseus wikiPageWikiLink Category:Bristol_aircraft_engines.
- Bristol_Theseus wikiPageWikiLink Category:Turboprop_engines_1940–1949.
- Bristol_Theseus wikiPageWikiLink Handley_Page_Hermes.
- Bristol_Theseus wikiPageWikiLink List_of_aircraft_engines.
- Bristol_Theseus wikiPageWikiLink Turbine.
- Bristol_Theseus wikiPageWikiLink Turboprop.
- Bristol_Theseus wikiPageWikiLink Type_certificate.
- Bristol_Theseus wikiPageWikiLinkText "Bristol Theseus 502".
- Bristol_Theseus wikiPageWikiLinkText "Bristol Theseus".
- Bristol_Theseus wikiPageWikiLinkText "Theseus engine".
- Bristol_Theseus wikiPageWikiLinkText "Theseus".
- Bristol_Theseus combustion "8".
- Bristol_Theseus compression "3".
- Bristol_Theseus compressor "8".
- Bristol_Theseus firstRun "1945-07-18".
- Bristol_Theseus fuelcon "/hr".
- Bristol_Theseus fueltype "Kerosene".
- Bristol_Theseus hasPhotoCollection Bristol_Theseus.
- Bristol_Theseus majorApplications Handley_Page_Hermes.
- Bristol_Theseus manufacturer Bristol_Siddeley.
- Bristol_Theseus oilsystem "pressure feed to bearings, dry sump, 40 S.U. secs grade oil".
- Bristol_Theseus power "equivalent at 8,200 rpm at sea level".
- Bristol_Theseus weight "1.02".
- Bristol_Theseus specfuelcon "0.5".
- Bristol_Theseus weight "*Maximum flight rating: equivalent at 8,200 rpm at".
- Bristol_Theseus turbine "2".
- Bristol_Theseus type Turboprop.
- Bristol_Theseus type "Mixed compressor turboprop with heat exchanger".
- Bristol_Theseus wikiPageUsesTemplate Template:BristolAeroengines.
- Bristol_Theseus wikiPageUsesTemplate Template:Commons_category.
- Bristol_Theseus wikiPageUsesTemplate Template:Infobox_Aircraft_Engine.
- Bristol_Theseus wikiPageUsesTemplate Template:Jetspecs.
- Bristol_Theseus wikiPageUsesTemplate Template:Refbegin.
- Bristol_Theseus wikiPageUsesTemplate Template:Refend.
- Bristol_Theseus wikiPageUsesTemplate Template:Reflist.
- Bristol_Theseus subject Category:Bristol_aircraft_engines.
- Bristol_Theseus subject Category:Turboprop_engines_1940–1949.
- Bristol_Theseus hypernym Company.
- Bristol_Theseus type Company.
- Bristol_Theseus comment "The Theseus was the Bristol Aeroplane Company's first attempt at a gas-turbine engine design, a turboprop that delivered just over 2,000 hp (1,500 kW).".
- Bristol_Theseus label "Bristol Theseus".
- Bristol_Theseus sameAs Bristol_Theseus.
- Bristol_Theseus sameAs m.01vwzq.
- Bristol_Theseus sameAs Q4969038.
- Bristol_Theseus sameAs Q4969038.
- Bristol_Theseus wasDerivedFrom Bristol_Theseus?oldid=681454944.
- Bristol_Theseus isPrimaryTopicOf Bristol_Theseus.