Matches in DBpedia 2016-04 for { <http://dbpedia.org/resource/KVD-1> ?p ?o }
Showing triples 1 to 67 of
67
with 100 triples per page.
- KVD-1 abstract "KVD-1 was an upper stage LOX/LH2 cryogenic engine developed by Isayev Design Bureau (now KB KhIMMASH) of Russia in early 1960s. It is a modified version of RD-56 which was developed with an intention to manufacture cryogenic engine for upper stage of Lunar N-1 launch vehicle. It was to be used in USSR moon missions.Template:Unreliable source? KVD-1 can produce engine thrust of 7.5 tonnes.".
- KVD-1 wikiPageExternalLink rd56.htm.
- KVD-1 wikiPageID "41571990".
- KVD-1 wikiPageLength "7538".
- KVD-1 wikiPageOutDegree "22".
- KVD-1 wikiPageRevisionID "705945601".
- KVD-1 wikiPageWikiLink A.M._Isayev_Chemical_Engineering_Design_Bureau.
- KVD-1 wikiPageWikiLink Angara_(rocket_family).
- KVD-1 wikiPageWikiLink Category:Articles_created_via_the_Article_Wizard.
- KVD-1 wikiPageWikiLink Category:Rocket_engines.
- KVD-1 wikiPageWikiLink Category:Rocket_engines_of_the_Soviet_Union.
- KVD-1 wikiPageWikiLink Category:Rocket_engines_using_hydrogen_propellant.
- KVD-1 wikiPageWikiLink GSAT-1.
- KVD-1 wikiPageWikiLink GSAT-5P.
- KVD-1 wikiPageWikiLink Geosynchronous_Satellite_Launch_Vehicle.
- KVD-1 wikiPageWikiLink Glavcosmos.
- KVD-1 wikiPageWikiLink INSAT-4CR.
- KVD-1 wikiPageWikiLink Indian_Space_Research_Organisation.
- KVD-1 wikiPageWikiLink KVTK_(rocket_stage).
- KVD-1 wikiPageWikiLink Liquid_hydrogen.
- KVD-1 wikiPageWikiLink Liquid_oxygen.
- KVD-1 wikiPageWikiLink Missile_Technology_Control_Regime.
- KVD-1 wikiPageWikiLink Proton-M.
- KVD-1 wikiPageWikiLink Russia.
- KVD-1 wikiPageWikiLink Soviet_Union.
- KVD-1 wikiPageWikiLink Staged_combustion.
- KVD-1 wikiPageWikiLinkText "KVD-1".
- KVD-1 associated Geosynchronous_Satellite_Launch_Vehicle.
- KVD-1 burnTime "800.0".
- KVD-1 combustionChamber "1".
- KVD-1 countryOfOrigin Russia.
- KVD-1 countryOfOrigin Soviet_Union.
- KVD-1 cycle Staged_combustion.
- KVD-1 date "March 2015".
- KVD-1 designer A.M._Isayev_Chemical_Engineering_Design_Bureau.
- KVD-1 firstDate "2001-04-20".
- KVD-1 fuel Liquid_hydrogen.
- KVD-1 gimbal "None; uses 2 vernier engines for attitude control".
- KVD-1 lastDate "2010-12-25".
- KVD-1 mixtureRatio "6".
- KVD-1 name "KVD-1".
- KVD-1 oxidiser Liquid_oxygen.
- KVD-1 purpose "Upper stage engine".
- KVD-1 reason "not doubting the engine was designed for lunar rocket, but this is an opinion piece and makes a lot of unverifiable claims.".
- KVD-1 specificImpulseVacuum "462.0".
- KVD-1 status "Retired".
- KVD-1 type "liquid".
- KVD-1 wikiPageUsesTemplate Template:Convert.
- KVD-1 wikiPageUsesTemplate Template:Infobox_rocket_engine.
- KVD-1 wikiPageUsesTemplate Template:Reflist.
- KVD-1 wikiPageUsesTemplate Template:Rocket_Engines.
- KVD-1 wikiPageUsesTemplate Template:Unreliable_source%3F.
- KVD-1 wikiPageUsesTemplate Template:Upper_stages.
- KVD-1 subject Category:Articles_created_via_the_Article_Wizard.
- KVD-1 subject Category:Rocket_engines.
- KVD-1 subject Category:Rocket_engines_of_the_Soviet_Union.
- KVD-1 subject Category:Rocket_engines_using_hydrogen_propellant.
- KVD-1 hypernym LH.
- KVD-1 comment "KVD-1 was an upper stage LOX/LH2 cryogenic engine developed by Isayev Design Bureau (now KB KhIMMASH) of Russia in early 1960s. It is a modified version of RD-56 which was developed with an intention to manufacture cryogenic engine for upper stage of Lunar N-1 launch vehicle. It was to be used in USSR moon missions.Template:Unreliable source? KVD-1 can produce engine thrust of 7.5 tonnes.".
- KVD-1 label "KVD-1".
- KVD-1 sameAs Q17007267.
- KVD-1 sameAs KVD-1.
- KVD-1 sameAs m.0_gywrg.
- KVD-1 sameAs Q17007267.
- KVD-1 sameAs RD-56.
- KVD-1 wasDerivedFrom KVD-1?oldid=705945601.
- KVD-1 isPrimaryTopicOf KVD-1.