Matches in DBpedia 2016-04 for { <http://dbpedia.org/resource/RD-120> ?p ?o }
- RD-120 abstract "The RD-120 (GRAU Index 11D123) is a liquid upper stage rocket engine burning RG-1 and LOX in an oxidizer rich staged combustion cycle with an O/F ratio of 2.6. It is used in the second stage of the Zenit family of launch vehicles. It has a single, fixed combustion chamber and thus on the Zenit it is paired with the RD-8 vernier engine. The engine has been developed from 1976 to 1985 by NPO Energomash with V.P. Radovskogo leading the development. It is manufactured by Yuzhmash in Ukraine along most of the rocket.It should not be confused with the RD-0120, which is a discontinued LOX/hydrogen rocket engine that was used in the Soviet Energia launch system.".
- RD-120 wikiPageExternalLink rd120.
- RD-120 wikiPageExternalLink rengines?id=25.
- RD-120 wikiPageID "29129815".
- RD-120 wikiPageLength "20013".
- RD-120 wikiPageOutDegree "80".
- RD-120 wikiPageRevisionID "686851741".
- RD-120 wikiPageWikiLink Boeing_747.
- RD-120 wikiPageWikiLink Buran_programme.
- RD-120 wikiPageWikiLink Category:Rocket_engines.
- RD-120 wikiPageWikiLink Category:Rocket_engines_of_Russia.
- RD-120 wikiPageWikiLink Category:Rocket_engines_of_the_Soviet_Union.
- RD-120 wikiPageWikiLink Category:Rocket_engines_using_kerosene_propellant.
- RD-120 wikiPageWikiLink Category:Spaceflight.
- RD-120 wikiPageWikiLink Chemical_Automatics_Design_Bureau.
- RD-120 wikiPageWikiLink EchoStar_X.
- RD-120 wikiPageWikiLink Energia.
- RD-120 wikiPageWikiLink GRAU.
- RD-120 wikiPageWikiLink Gimbaled_thrust.
- RD-120 wikiPageWikiLink Liquefied_natural_gas.
- RD-120 wikiPageWikiLink Liquid-propellant_rocket.
- RD-120 wikiPageWikiLink Liquid_oxygen.
- RD-120 wikiPageWikiLink Makeyev_Rocket_Design_Bureau.
- RD-120 wikiPageWikiLink Methane.
- RD-120 wikiPageWikiLink Multistage_rocket.
- RD-120 wikiPageWikiLink NPO_Energomash.
- RD-120 wikiPageWikiLink Orbital_Sciences_Corporation.
- RD-120 wikiPageWikiLink Orbital_Sciences_X-34.
- RD-120 wikiPageWikiLink Pratt_&_Whitney.
- RD-120 wikiPageWikiLink Proton_(rocket_family).
- RD-120 wikiPageWikiLink RD-0120.
- RD-120 wikiPageWikiLink RD-170.
- RD-120 wikiPageWikiLink RD-263.
- RD-120 wikiPageWikiLink RD-8.
- RD-120 wikiPageWikiLink RP-1.
- RD-120 wikiPageWikiLink RS-27.
- RD-120 wikiPageWikiLink Rocket_engine.
- RD-120 wikiPageWikiLink Rocket_propellant.
- RD-120 wikiPageWikiLink Rockwell_International.
- RD-120 wikiPageWikiLink Russia.
- RD-120 wikiPageWikiLink SCE-200.
- RD-120 wikiPageWikiLink Sea_Launch.
- RD-120 wikiPageWikiLink Soviet_Union.
- RD-120 wikiPageWikiLink Soyuz_(rocket).
- RD-120 wikiPageWikiLink Space_Shuttle_main_engine.
- RD-120 wikiPageWikiLink Staged_combustion_cycle.
- RD-120 wikiPageWikiLink Thrust_vectoring.
- RD-120 wikiPageWikiLink Ukraine.
- RD-120 wikiPageWikiLink United_States.
- RD-120 wikiPageWikiLink Vernier_thruster.
- RD-120 wikiPageWikiLink WikiLeaks.
- RD-120 wikiPageWikiLink YF-100.
- RD-120 wikiPageWikiLink YF-115.
- RD-120 wikiPageWikiLink Yuzhmash.
- RD-120 wikiPageWikiLink Yuzhnoye_Design_Office.
- RD-120 wikiPageWikiLink Zenit-2.
- RD-120 wikiPageWikiLink Zenit-3SL.
- RD-120 wikiPageWikiLink Zenit_(rocket_family).
- RD-120 wikiPageWikiLinkText "RD-120".
- RD-120 wikiPageWikiLinkText "RD-120M".
- RD-120 burnTime "315.0".
- RD-120 chamberPressure "Standard:".
- RD-120 chamberPressure "Uprated:".
- RD-120 countryOfOrigin Russia.
- RD-120 countryOfOrigin Soviet_Union.
- RD-120 cycle Staged_combustion_cycle.
- RD-120 designer "NPO Energomash, V.K.Chvanov, V.P. Radovsky".
- RD-120 fuel RP-1.
- RD-120 manufacturer Yuzhmash.
- RD-120 name "RD-120".
- RD-120 oxidiser Liquid_oxygen.
- RD-120 purpose "Upper stage".
- RD-120 specificImpulseVacuum "350.0".
- RD-120 status "Operational".
- RD-120 thrust(vac)_ "Standard:".
- RD-120 thrust(vac)_ "Uprated:".
- RD-120 thrustToWeight "Standard:".
- RD-120 thrustToWeight "Uprated:".
- RD-120 type "liquid".
- RD-120 usedIn Zenit-2.
- RD-120 usedIn Zenit-3SL.
- RD-120 wikiPageUsesTemplate Template:Convert.
- RD-120 wikiPageUsesTemplate Template:Infobox_rocket_engine.
- RD-120 wikiPageUsesTemplate Template:Nts.
- RD-120 wikiPageUsesTemplate Template:Reflist.
- RD-120 wikiPageUsesTemplate Template:Rocket_Engines.
- RD-120 wikiPageUsesTemplate Template:Russian_and_Soviet_military_designation_sequences.
- RD-120 subject Category:Rocket_engines.
- RD-120 subject Category:Rocket_engines_of_Russia.
- RD-120 subject Category:Rocket_engines_of_the_Soviet_Union.
- RD-120 subject Category:Rocket_engines_using_kerosene_propellant.
- RD-120 subject Category:Spaceflight.
- RD-120 comment "The RD-120 (GRAU Index 11D123) is a liquid upper stage rocket engine burning RG-1 and LOX in an oxidizer rich staged combustion cycle with an O/F ratio of 2.6. It is used in the second stage of the Zenit family of launch vehicles. It has a single, fixed combustion chamber and thus on the Zenit it is paired with the RD-8 vernier engine. The engine has been developed from 1976 to 1985 by NPO Energomash with V.P. Radovskogo leading the development.".
- RD-120 label "RD-120".
- RD-120 sameAs Q574440.
- RD-120 sameAs RD-120.
- RD-120 sameAs RD-120.
- RD-120 sameAs RD-120.
- RD-120 sameAs RD-120.
- RD-120 sameAs m.0fpgq37.