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- RD-263 abstract "The RD-263 (GRAU Index 15D117) is a liquid rocket engine, burning N2O4 and UDMH in the oxidizer rich staged combustion cycle. Four RD-263 form a propulsion module RD-264 (GRAU Index 15D119). For the R-36M KB Yuzhnoye only ordered the first stage propulsion to Energomash, instead of both stages, arguing that they were overworked with the RD-270 development. By April 1970 Yuzhnoye was getting the engine documentation. By the end of 1972 Energomash started to test fire the engines in its own test stand. And by September 1973 the engine was certified for flight. While the engine is out of production, the ICBM as well as the Dnepr-1 remain operational as of 2015.".
- RD-263 wikiPageExternalLink rd0233.htm.
- RD-263 wikiPageExternalLink ?p=8&cat=10&prod=47.
- RD-263 wikiPageID "47034076".
- RD-263 wikiPageLength "9632".
- RD-263 wikiPageOutDegree "55".
- RD-263 wikiPageRevisionID "695639378".
- RD-263 wikiPageWikiLink Category:Rocket_engines.
- RD-263 wikiPageWikiLink Category:Rocket_engines_of_the_Soviet_Union.
- RD-263 wikiPageWikiLink Category:Rocket_engines_using_hypergolic_propellant.
- RD-263 wikiPageWikiLink Category:Spaceflight.
- RD-263 wikiPageWikiLink Dinitrogen_tetroxide.
- RD-263 wikiPageWikiLink Dnepr-1.
- RD-263 wikiPageWikiLink GRAU.
- RD-263 wikiPageWikiLink Intercontinental_ballistic_missile.
- RD-263 wikiPageWikiLink Launch_vehicle.
- RD-263 wikiPageWikiLink Liquid-propellant_rocket.
- RD-263 wikiPageWikiLink NPO_Energomash.
- RD-263 wikiPageWikiLink R-36_(missile).
- RD-263 wikiPageWikiLink RD-270.
- RD-263 wikiPageWikiLink Rocket_engine.
- RD-263 wikiPageWikiLink SS-17_Spanker.
- RD-263 wikiPageWikiLink Soviet_Union.
- RD-263 wikiPageWikiLink Staged_combustion_cycle.
- RD-263 wikiPageWikiLink Unsymmetrical_dimethylhydrazine.
- RD-263 wikiPageWikiLink Valentin_Glushko.
- RD-263 wikiPageWikiLink Yuzhmash.
- RD-263 wikiPageWikiLink Yuzhnoye_Design_Office.
- RD-263 wikiPageWikiLinkText "RD-263".
- RD-263 wikiPageWikiLinkText "RD-268".
- RD-263 associated "R-36M and Dnepr".
- RD-263 combustionChamber "1".
- RD-263 countryOfOrigin Soviet_Union.
- RD-263 cycle Staged_combustion_cycle.
- RD-263 date "1969".
- RD-263 designer NPO_Energomash.
- RD-263 designer Valentin_Glushko.
- RD-263 fuel Unsymmetrical_dimethylhydrazine.
- RD-263 gimbal "7".
- RD-263 manufacturer Yuzhmash.
- RD-263 mixtureRatio "2.67".
- RD-263 name "RD-263".
- RD-263 oxidiser Dinitrogen_tetroxide.
- RD-263 status "Out of Production".
- RD-263 type "liquid".
- RD-263 usedIn "R-36M and R-36MUTTKh core stage".
- RD-263 wikiPageUsesTemplate Template:Convert.
- RD-263 wikiPageUsesTemplate Template:Infobox_rocket_engine.
- RD-263 wikiPageUsesTemplate Template:Portal.
- RD-263 wikiPageUsesTemplate Template:Reflist.
- RD-263 wikiPageUsesTemplate Template:Rocket_Engines.
- RD-263 subject Category:Rocket_engines.
- RD-263 subject Category:Rocket_engines_of_the_Soviet_Union.
- RD-263 subject Category:Rocket_engines_using_hypergolic_propellant.
- RD-263 subject Category:Spaceflight.
- RD-263 hypernym Engine.
- RD-263 type Software.
- RD-263 comment "The RD-263 (GRAU Index 15D117) is a liquid rocket engine, burning N2O4 and UDMH in the oxidizer rich staged combustion cycle. Four RD-263 form a propulsion module RD-264 (GRAU Index 15D119). For the R-36M KB Yuzhnoye only ordered the first stage propulsion to Energomash, instead of both stages, arguing that they were overworked with the RD-270 development. By April 1970 Yuzhnoye was getting the engine documentation.".
- RD-263 label "RD-263".
- RD-263 sameAs Q20203126.
- RD-263 sameAs RD-263.
- RD-263 sameAs Q20203126.
- RD-263 wasDerivedFrom RD-263?oldid=695639378.
- RD-263 homepage ?p=8&cat=10&prod=47.
- RD-263 isPrimaryTopicOf RD-263.