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- RD-0210 abstract "The RD-0210 (GRAU Index: 8D411K) is also known as the RD-465. It and its twin, the RD-0211, are rocket engines burning N2O4 and UDMH in a oxidizer rich staged combustion cycle. They have single nozzle, possess TVC and are the latest evolution in the RD-0203/4 lineage. They are the engines used on the Proton second stage. The RD-0213 is a fixed nozzle variation that is used on the RD-0212 module of the Proton third stage.".
- RD-0210 wikiPageExternalLink liquid-rocket-engine.
- RD-0210 wikiPageExternalLink www.kbkha.ru.
- RD-0210 wikiPageExternalLink www.khrunichev.ru.
- RD-0210 wikiPageID "46972775".
- RD-0210 wikiPageLength "20153".
- RD-0210 wikiPageOutDegree "106".
- RD-0210 wikiPageRevisionID "699174698".
- RD-0210 wikiPageWikiLink Category:Rocket_engines.
- RD-0210 wikiPageWikiLink Category:Rocket_engines_of_Russia.
- RD-0210 wikiPageWikiLink Category:Rocket_engines_of_the_Soviet_Union.
- RD-0210 wikiPageWikiLink Category:Rocket_engines_using_hypergolic_propellant.
- RD-0210 wikiPageWikiLink Category:Spaceflight.
- RD-0210 wikiPageWikiLink Chemical_Automatics_Design_Bureau.
- RD-0210 wikiPageWikiLink Dinitrogen_tetroxide.
- RD-0210 wikiPageWikiLink Free_return_trajectory.
- RD-0210 wikiPageWikiLink GRAU.
- RD-0210 wikiPageWikiLink Heavy_ICBM.
- RD-0210 wikiPageWikiLink Intercontinental_ballistic_missile.
- RD-0210 wikiPageWikiLink International_Space_Station.
- RD-0210 wikiPageWikiLink Liquid-propellant_rocket.
- RD-0210 wikiPageWikiLink Mars.
- RD-0210 wikiPageWikiLink Mars_2.
- RD-0210 wikiPageWikiLink Mikhail_Vasilyevich_Melnikov.
- RD-0210 wikiPageWikiLink Moon.
- RD-0210 wikiPageWikiLink N1_(rocket).
- RD-0210 wikiPageWikiLink NPO_Mashinostroyeniya.
- RD-0210 wikiPageWikiLink Proton_(rocket_family).
- RD-0210 wikiPageWikiLink R-36_(missile).
- RD-0210 wikiPageWikiLink RD-0210.
- RD-0210 wikiPageWikiLink RD-0214.
- RD-0210 wikiPageWikiLink Rocket_engine.
- RD-0210 wikiPageWikiLink Russia.
- RD-0210 wikiPageWikiLink Russian_Orbital_Segment.
- RD-0210 wikiPageWikiLink S.P._Korolev_Rocket_and_Space_Corporation_Energia.
- RD-0210 wikiPageWikiLink S1.5400.
- RD-0210 wikiPageWikiLink Salyut_1.
- RD-0210 wikiPageWikiLink Semyon_Kosberg.
- RD-0210 wikiPageWikiLink Sergei_Korolev.
- RD-0210 wikiPageWikiLink Soviet_Union.
- RD-0210 wikiPageWikiLink Soviet_manned_lunar_programs.
- RD-0210 wikiPageWikiLink Staged_combustion_cycle.
- RD-0210 wikiPageWikiLink Thrust_vectoring.
- RD-0210 wikiPageWikiLink UR-200.
- RD-0210 wikiPageWikiLink Unsymmetrical_dimethylhydrazine.
- RD-0210 wikiPageWikiLink Venera_9.
- RD-0210 wikiPageWikiLink Venus.
- RD-0210 wikiPageWikiLink Vernier_thruster.
- RD-0210 wikiPageWikiLink Vladimir_Chelomey.
- RD-0210 wikiPageWikiLink Voronezh_Mechanical_Plant.
- RD-0210 wikiPageWikiLink Zarya.
- RD-0210 wikiPageWikiLink Zond_5.
- RD-0210 wikiPageWikiLink Zvezda_(ISS_module).
- RD-0210 wikiPageWikiLinkText "RD-0210".
- RD-0210 wikiPageWikiLinkText "RD-0210#Modules".
- RD-0210 associated Proton_(rocket_family).
- RD-0210 burnTime "220.0".
- RD-0210 combustionChamber "1".
- RD-0210 countryOfOrigin Russia.
- RD-0210 countryOfOrigin Soviet_Union.
- RD-0210 cycle Staged_combustion_cycle.
- RD-0210 designer "OKB-154, Yankel I. Guerchkovitch".
- RD-0210 firstDate "1967-03-10".
- RD-0210 fuel Unsymmetrical_dimethylhydrazine.
- RD-0210 manufacturer Voronezh_Mechanical_Plant.
- RD-0210 mixtureRatio "2.6".
- RD-0210 name "RD-0210".
- RD-0210 oxidiser Dinitrogen_tetroxide.
- RD-0210 predecessor RD-0210.
- RD-0210 purpose "Upper Stage".
- RD-0210 specificImpulseVacuum "326.5".
- RD-0210 status "In Production".
- RD-0210 type "liquid".
- RD-0210 usedIn "UR-200 and UR-500 and Proton second stage".
- RD-0210 wikiPageUsesTemplate Template:Convert.
- RD-0210 wikiPageUsesTemplate Template:Infobox_rocket_engine.
- RD-0210 wikiPageUsesTemplate Template:Reflist.
- RD-0210 wikiPageUsesTemplate Template:Rocket_Engines.
- RD-0210 subject Category:Rocket_engines.
- RD-0210 subject Category:Rocket_engines_of_Russia.
- RD-0210 subject Category:Rocket_engines_of_the_Soviet_Union.
- RD-0210 subject Category:Rocket_engines_using_hypergolic_propellant.
- RD-0210 subject Category:Spaceflight.
- RD-0210 comment "The RD-0210 (GRAU Index: 8D411K) is also known as the RD-465. It and its twin, the RD-0211, are rocket engines burning N2O4 and UDMH in a oxidizer rich staged combustion cycle. They have single nozzle, possess TVC and are the latest evolution in the RD-0203/4 lineage. They are the engines used on the Proton second stage. The RD-0213 is a fixed nozzle variation that is used on the RD-0212 module of the Proton third stage.".
- RD-0210 label "RD-0210".
- RD-0210 sameAs Q20203120.
- RD-0210 sameAs RD-0210.
- RD-0210 sameAs Q20203120.
- RD-0210 wasDerivedFrom RD-0210?oldid=699174698.
- RD-0210 isPrimaryTopicOf RD-0210.