Matches in DBpedia 2015-10 for { <http://dbpedia.org/resource/Rolls-Royce/MAN_Turbo_RB153> ?p ?o }
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- MAN_Turbo_RB153 abstract "The Rolls-Royce/MAN Turbo RB.153 was a high-performance 6,850 pounds-force (3,110 kgf) dry thrust turbofan engine developed jointly by Rolls-Royce Limited and MAN Turbo. Developed for the German EWR VJ 101D interceptor with a German-developed thrust-deflector system. The engine was also proposed for a number of other military VTOL projects including the Hawker P.1157. A commercial-version of the engine was also considered for the Messerschmitt Me P.160 airliner. The VJ101D project was cancelled and the engine never flew, being retained as a test bed.".
- MAN_Turbo_RB153 wikiPageID "28582762".
- MAN_Turbo_RB153 wikiPageLength "3143".
- MAN_Turbo_RB153 wikiPageOutDegree "15".
- MAN_Turbo_RB153 wikiPageRevisionID "668369295".
- MAN_Turbo_RB153 wikiPageWikiLink Category:Rolls-Royce_aircraft_gas_turbine_engines.
- MAN_Turbo_RB153 wikiPageWikiLink Category:Turbofan_engines_1960–1969.
- MAN_Turbo_RB153 wikiPageWikiLink EWR_VJ_101.
- MAN_Turbo_RB153 wikiPageWikiLink Hawker_P.1157.
- MAN_Turbo_RB153 wikiPageWikiLink List_of_aircraft_engines.
- MAN_Turbo_RB153 wikiPageWikiLink MAN_Turbo.
- MAN_Turbo_RB153 wikiPageWikiLink MAN_Turbo_RB193.
- MAN_Turbo_RB153 wikiPageWikiLink Rolls-Royce_Limited.
- MAN_Turbo_RB153 wikiPageWikiLink Turbofan.
- MAN_Turbo_RB153 wikiPageWikiLink VTOL.
- MAN_Turbo_RB153 wikiPageWikiLinkText "RB153".
- MAN_Turbo_RB153 wikiPageWikiLinkText "Rolls-Royce RB.153".
- MAN_Turbo_RB153 wikiPageWikiLinkText "Rolls-Royce/MAN Turbo RB153".
- MAN_Turbo_RB153 diameter "29.5".
- MAN_Turbo_RB153 firstRun "January".
- MAN_Turbo_RB153 fuelcon "121".
- MAN_Turbo_RB153 hasPhotoCollection MAN_Turbo_RB153.
- MAN_Turbo_RB153 length "89".
- MAN_Turbo_RB153 lists "*List of aircraft engines".
- MAN_Turbo_RB153 majorApplications EWR_VJ_101.
- MAN_Turbo_RB153 manufacturer Rolls-Royce_Limited.
- MAN_Turbo_RB153 manufacturer "MAN Turbo".
- MAN_Turbo_RB153 seeAlso "*Rolls-Royce/MAN Turbo RB193".
- MAN_Turbo_RB153 thrust "6850".
- MAN_Turbo_RB153 type Turbofan.
- MAN_Turbo_RB153 type "Turbofan".
- MAN_Turbo_RB153 weight "1431.0".
- MAN_Turbo_RB153 wikiPageUsesTemplate Template:Aircontent.
- MAN_Turbo_RB153 wikiPageUsesTemplate Template:Convert.
- MAN_Turbo_RB153 wikiPageUsesTemplate Template:Infobox_Aircraft_Engine.
- MAN_Turbo_RB153 wikiPageUsesTemplate Template:Jetspecs.
- MAN_Turbo_RB153 wikiPageUsesTemplate Template:Joint_development_aeroengines.
- MAN_Turbo_RB153 wikiPageUsesTemplate Template:Refbegin.
- MAN_Turbo_RB153 wikiPageUsesTemplate Template:Refend.
- MAN_Turbo_RB153 wikiPageUsesTemplate Template:Reflist.
- MAN_Turbo_RB153 subject Category:Rolls-Royce_aircraft_gas_turbine_engines.
- MAN_Turbo_RB153 subject Category:Turbofan_engines_1960–1969.
- MAN_Turbo_RB153 hypernym Engine.
- MAN_Turbo_RB153 type Software.
- MAN_Turbo_RB153 comment "The Rolls-Royce/MAN Turbo RB.153 was a high-performance 6,850 pounds-force (3,110 kgf) dry thrust turbofan engine developed jointly by Rolls-Royce Limited and MAN Turbo. Developed for the German EWR VJ 101D interceptor with a German-developed thrust-deflector system. The engine was also proposed for a number of other military VTOL projects including the Hawker P.1157. A commercial-version of the engine was also considered for the Messerschmitt Me P.160 airliner.".
- MAN_Turbo_RB153 label "Rolls-Royce/MAN Turbo RB153".
- MAN_Turbo_RB153 sameAs m.0czd1hw.
- MAN_Turbo_RB153 sameAs Q7361311.
- MAN_Turbo_RB153 sameAs Q7361311.
- MAN_Turbo_RB153 wasDerivedFrom MAN_Turbo_RB153?oldid=668369295.
- MAN_Turbo_RB153 isPrimaryTopicOf MAN_Turbo_RB153.