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- RD-0233 abstract "The RD-0233 (GRAU Index 15D95) and RD-0234 (GRAU Index 15D96) are liquid rocket engines, burning N2O4 and UDMH in the oxidizer rich staged combustion cycle. The only difference between the RD-0233 and the RD-0234 is that the latter has a heat exchanger to heat the pressuring gasses for the tanks. Three RD-0233 and one RD-0234 are used on the first stage of the UR-100UTTKh ICBM. While the engine is out of production, the ICBM as well as Rokot and Strela remain operational as of 2015.".
- RD-0233 wikiPageExternalLink rd0233.htm.
- RD-0233 wikiPageExternalLink ?p=8&cat=10&prod=47.
- RD-0233 wikiPageID "47022645".
- RD-0233 wikiPageLength "4256".
- RD-0233 wikiPageOutDegree "34".
- RD-0233 wikiPageRevisionID "675949768".
- RD-0233 wikiPageWikiLink Category:Rocket_engines.
- RD-0233 wikiPageWikiLink Category:Rocket_engines_of_the_Soviet_Union.
- RD-0233 wikiPageWikiLink Category:Rocket_engines_using_hypergolic_propellant.
- RD-0233 wikiPageWikiLink Category:Spaceflight.
- RD-0233 wikiPageWikiLink Chemical_Automatics_Design_Bureau.
- RD-0233 wikiPageWikiLink Dinitrogen_tetroxide.
- RD-0233 wikiPageWikiLink GRAU.
- RD-0233 wikiPageWikiLink Intercontinental_ballistic_missile.
- RD-0233 wikiPageWikiLink Launch_vehicle.
- RD-0233 wikiPageWikiLink Liquid-propellant_rocket.
- RD-0233 wikiPageWikiLink Rocket_engine.
- RD-0233 wikiPageWikiLink Rokot.
- RD-0233 wikiPageWikiLink Soviet_Union.
- RD-0233 wikiPageWikiLink Staged_combustion_cycle.
- RD-0233 wikiPageWikiLink Strela_(rocket).
- RD-0233 wikiPageWikiLink UR-100N.
- RD-0233 wikiPageWikiLink Unsymmetrical_dimethylhydrazine.
- RD-0233 wikiPageWikiLinkText "RD-0233".
- RD-0233 associated "UR-100N, Rokot and Strela".
- RD-0233 burnTime "121.0".
- RD-0233 combustionChamber "1".
- RD-0233 countryOfOrigin Soviet_Union.
- RD-0233 cycle Staged_combustion_cycle.
- RD-0233 designer Chemical_Automatics_Design_Bureau.
- RD-0233 firstDate "1973-04-09".
- RD-0233 fuel Unsymmetrical_dimethylhydrazine.
- RD-0233 name "RD-0233".
- RD-0233 oxidiser Dinitrogen_tetroxide.
- RD-0233 status "Out of Production".
- RD-0233 type "liquid".
- RD-0233 usedIn "UR-100N core stage".
- RD-0233 wikiPageUsesTemplate Template:Convert.
- RD-0233 wikiPageUsesTemplate Template:Infobox_rocket_engine.
- RD-0233 wikiPageUsesTemplate Template:Portal.
- RD-0233 wikiPageUsesTemplate Template:Reflist.
- RD-0233 wikiPageUsesTemplate Template:Rocket-stub.
- RD-0233 wikiPageUsesTemplate Template:Rocket_Engines.
- RD-0233 subject Category:Rocket_engines.
- RD-0233 subject Category:Rocket_engines_of_the_Soviet_Union.
- RD-0233 subject Category:Rocket_engines_using_hypergolic_propellant.
- RD-0233 subject Category:Spaceflight.
- RD-0233 hypernym Engines.
- RD-0233 type Locomotive.
- RD-0233 comment "The RD-0233 (GRAU Index 15D95) and RD-0234 (GRAU Index 15D96) are liquid rocket engines, burning N2O4 and UDMH in the oxidizer rich staged combustion cycle. The only difference between the RD-0233 and the RD-0234 is that the latter has a heat exchanger to heat the pressuring gasses for the tanks. Three RD-0233 and one RD-0234 are used on the first stage of the UR-100UTTKh ICBM. While the engine is out of production, the ICBM as well as Rokot and Strela remain operational as of 2015.".
- RD-0233 label "RD-0233".
- RD-0233 sameAs Q20203123.
- RD-0233 sameAs RD-0233.
- RD-0233 sameAs m.013f7rsv.
- RD-0233 sameAs Q20203123.
- RD-0233 wasDerivedFrom RD-0233?oldid=675949768.
- RD-0233 homepage ?p=8&cat=10&prod=47.
- RD-0233 isPrimaryTopicOf RD-0233.