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- RD-0243 abstract "The RD-0243 is a propulsion module composed of an RD-0244 main engine and a RD-0245 vernier engine. Both are liquid rocket engine, burning N2O4 and UDMH. The RD-0244 main engine operates in the oxidizer rich staged combustion cycle, while the vernier RD-0245 uses the simpler gas generator cycle. Since volume is at a premium on submarine launches, this module is submerged on the propellant tank. Its development period was from 1977 to 1985, having had its first launch on December 27, 1981. Originally developed for the RSM-54, it was used later for the Shtil'.".
- RD-0243 wikiPageExternalLink rd0243.htm.
- RD-0243 wikiPageExternalLink ?p=8&cat=10&prod=50.
- RD-0243 wikiPageID "47016009".
- RD-0243 wikiPageLength "5451".
- RD-0243 wikiPageOutDegree "31".
- RD-0243 wikiPageRevisionID "675949795".
- RD-0243 wikiPageWikiLink Category:Rocket_engines.
- RD-0243 wikiPageWikiLink Category:Rocket_engines_of_the_Soviet_Union.
- RD-0243 wikiPageWikiLink Category:Rocket_engines_using_hypergolic_propellant.
- RD-0243 wikiPageWikiLink Category:Sea_launch_to_orbit.
- RD-0243 wikiPageWikiLink Category:Spaceflight.
- RD-0243 wikiPageWikiLink Chemical_Automatics_Design_Bureau.
- RD-0243 wikiPageWikiLink Dinitrogen_tetroxide.
- RD-0243 wikiPageWikiLink Gas-generator_cycle.
- RD-0243 wikiPageWikiLink Liquid-propellant_rocket.
- RD-0243 wikiPageWikiLink R-29RM_Shtil.
- RD-0243 wikiPageWikiLink Rocket_engine.
- RD-0243 wikiPageWikiLink Shtil.
- RD-0243 wikiPageWikiLink Soviet_Union.
- RD-0243 wikiPageWikiLink Staged_combustion_cycle.
- RD-0243 wikiPageWikiLink Unsymmetrical_dimethylhydrazine.
- RD-0243 wikiPageWikiLink Vernier_thruster.
- RD-0243 wikiPageWikiLinkText "RD-0243".
- RD-0243 associated R-29RM_Shtil.
- RD-0243 associated Shtil.
- RD-0243 burnTime "74.0".
- RD-0243 burnTime "79.0".
- RD-0243 combustionChamber "1".
- RD-0243 combustionChamber "4".
- RD-0243 countryOfOrigin Soviet_Union.
- RD-0243 cycle Gas-generator_cycle.
- RD-0243 cycle Staged_combustion_cycle.
- RD-0243 designer Chemical_Automatics_Design_Bureau.
- RD-0243 firstDate "1981-12-27".
- RD-0243 fuel Unsymmetrical_dimethylhydrazine.
- RD-0243 mixtureRatio "2.6".
- RD-0243 name "RD-0244".
- RD-0243 name "RD-0245".
- RD-0243 nozzleRatio "14".
- RD-0243 oxidiser Dinitrogen_tetroxide.
- RD-0243 status "Retired".
- RD-0243 type "liquid".
- RD-0243 usedIn "RD-0243 Propulsion Module".
- RD-0243 wikiPageUsesTemplate Template:Convert.
- RD-0243 wikiPageUsesTemplate Template:Infobox_rocket_engine.
- RD-0243 wikiPageUsesTemplate Template:Portal.
- RD-0243 wikiPageUsesTemplate Template:Reflist.
- RD-0243 wikiPageUsesTemplate Template:Rocket-stub.
- RD-0243 wikiPageUsesTemplate Template:Rocket_Engines.
- RD-0243 subject Category:Rocket_engines.
- RD-0243 subject Category:Rocket_engines_of_the_Soviet_Union.
- RD-0243 subject Category:Rocket_engines_using_hypergolic_propellant.
- RD-0243 subject Category:Sea_launch_to_orbit.
- RD-0243 subject Category:Spaceflight.
- RD-0243 hypernym Module.
- RD-0243 type Software.
- RD-0243 comment "The RD-0243 is a propulsion module composed of an RD-0244 main engine and a RD-0245 vernier engine. Both are liquid rocket engine, burning N2O4 and UDMH. The RD-0244 main engine operates in the oxidizer rich staged combustion cycle, while the vernier RD-0245 uses the simpler gas generator cycle. Since volume is at a premium on submarine launches, this module is submerged on the propellant tank. Its development period was from 1977 to 1985, having had its first launch on December 27, 1981.".
- RD-0243 label "RD-0243".
- RD-0243 sameAs Q20203125.
- RD-0243 sameAs RD-0243.
- RD-0243 sameAs m.013f7c6c.
- RD-0243 sameAs Q20203125.
- RD-0243 wasDerivedFrom RD-0243?oldid=675949795.
- RD-0243 homepage ?p=8&cat=10&prod=50.
- RD-0243 isPrimaryTopicOf RD-0243.