Matches in DBpedia 2015-10 for { <http://dbpedia.org/resource/BMW_018> ?p ?o }
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- BMW_018 abstract "The BMW 018 (RLM designation BMW 109-018) was an early axial-flow turbojet engine project by BMW AG in Germany.The 018 design was begun in 1940. It was generally similar to the 003, but had a twelve-stage axial compressor and three-stage turbine, for an output of 3,500 kg (7,700 lb) thrust.No engines were completed before the end of the Second World War.".
- BMW_018 wikiPageID "42881658".
- BMW_018 wikiPageLength "2287".
- BMW_018 wikiPageOutDegree "11".
- BMW_018 wikiPageRevisionID "671975129".
- BMW_018 wikiPageWikiLink Axial-flow.
- BMW_018 wikiPageWikiLink Axial_compressor.
- BMW_018 wikiPageWikiLink BMW.
- BMW_018 wikiPageWikiLink BMW_003.
- BMW_018 wikiPageWikiLink Category:BMW_aircraft_engines.
- BMW_018 wikiPageWikiLink Category:Turbojet_engines_1940–1949.
- BMW_018 wikiPageWikiLink Germany.
- BMW_018 wikiPageWikiLink Ministry_of_Aviation_(Nazi_Germany).
- BMW_018 wikiPageWikiLink Turbojet.
- BMW_018 wikiPageWikiLink World_War_II.
- BMW_018 wikiPageWikiLinkText "BMW 018".
- BMW_018 combustion "annular".
- BMW_018 compressor "12".
- BMW_018 diameter "125.2".
- BMW_018 firstRun "August".
- BMW_018 hasPhotoCollection BMW_018.
- BMW_018 length "4.19 m".
- BMW_018 manufacturer BMW.
- BMW_018 numberBuilt "None".
- BMW_018 ref "Christopher, John. The Race for Hitler's X-Planes , p.74.".
- BMW_018 turbine "3".
- BMW_018 type Turbojet.
- BMW_018 type "axial flow turbine".
- BMW_018 weight "2295.0".
- BMW_018 wikiPageUsesTemplate Template:BMW_aeroengines.
- BMW_018 wikiPageUsesTemplate Template:Convert.
- BMW_018 wikiPageUsesTemplate Template:Infobox_aircraft_engine.
- BMW_018 wikiPageUsesTemplate Template:Jetspecs.
- BMW_018 wikiPageUsesTemplate Template:Refimprove.
- BMW_018 wikiPageUsesTemplate Template:Reflist.
- BMW_018 subject Category:BMW_aircraft_engines.
- BMW_018 subject Category:Turbojet_engines_1940–1949.
- BMW_018 hypernym Project.
- BMW_018 type Band.
- BMW_018 comment "The BMW 018 (RLM designation BMW 109-018) was an early axial-flow turbojet engine project by BMW AG in Germany.The 018 design was begun in 1940. It was generally similar to the 003, but had a twelve-stage axial compressor and three-stage turbine, for an output of 3,500 kg (7,700 lb) thrust.No engines were completed before the end of the Second World War.".
- BMW_018 label "BMW 018".
- BMW_018 sameAs BMW_018.
- BMW_018 sameAs m.010qcmq6.
- BMW_018 sameAs Q796365.
- BMW_018 sameAs Q796365.
- BMW_018 wasDerivedFrom BMW_018?oldid=671975129.
- BMW_018 isPrimaryTopicOf BMW_018.