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- RD-0216 abstract "The RD-0216 and RD-0217 are liquid rocket engines, burning N2O4 and UDMH in the oxidizer rich staged combustion cycle. The only difference between the RD-0216 and the RD-0217 is that the latter has a heat exchanger to heat the pressuring gasses for the tanks. Three RD-0216 and one RD-0217 were used on the first stage of the UR-100 ICBM. The engines were manufactured until 1974 and stayed in operational use until 1991. More than 1100 engines were produced.For the UR-100N project, while first stage propulsion was based on the more powerful RD-0233 engine. The second stage used a variation of the RD-0217 called the RD-0235 (GRAU Index 15D113). It used a vacuum optimized nozzle extension, and thus had an extra 10s of isp and 21 kilonewtons (4,700 lbf) of more thrust. It has a fixed nozzle and relies on the RD-0236 vernier engine for thrust vectoring. While the engine has been out of production for a while, the UR-100NU and the Rokot and Strela use it as of 2015.".
- RD-0216 wikiPageExternalLink ?p=8&cat=10&prod=47.
- RD-0216 wikiPageExternalLink ?p=8&cat=10&prod=45.
- RD-0216 wikiPageID "47021696".
- RD-0216 wikiPageLength "6849".
- RD-0216 wikiPageOutDegree "47".
- RD-0216 wikiPageRevisionID "682519373".
- RD-0216 wikiPageWikiLink Category:Rocket_engines.
- RD-0216 wikiPageWikiLink Category:Rocket_engines_of_the_Soviet_Union.
- RD-0216 wikiPageWikiLink Category:Rocket_engines_using_hypergolic_propellant.
- RD-0216 wikiPageWikiLink Category:Spaceflight.
- RD-0216 wikiPageWikiLink Chemical_Automatics_Design_Bureau.
- RD-0216 wikiPageWikiLink Dinitrogen_tetroxide.
- RD-0216 wikiPageWikiLink GRAU.
- RD-0216 wikiPageWikiLink Intercontinental_ballistic_missile.
- RD-0216 wikiPageWikiLink Krasny_Oktyabr_Closed_Joint-Stock_Company.
- RD-0216 wikiPageWikiLink Liquid-propellant_rocket.
- RD-0216 wikiPageWikiLink Proton-PM.
- RD-0216 wikiPageWikiLink RD-0216.
- RD-0216 wikiPageWikiLink RD-0233.
- RD-0216 wikiPageWikiLink RD-0236.
- RD-0216 wikiPageWikiLink Rocket_engine.
- RD-0216 wikiPageWikiLink Rokot.
- RD-0216 wikiPageWikiLink Soviet_Union.
- RD-0216 wikiPageWikiLink Specific_impulse.
- RD-0216 wikiPageWikiLink Staged_combustion_cycle.
- RD-0216 wikiPageWikiLink Strela_(rocket).
- RD-0216 wikiPageWikiLink Thrust_vectoring.
- RD-0216 wikiPageWikiLink UR-100.
- RD-0216 wikiPageWikiLink UR-100N.
- RD-0216 wikiPageWikiLink Unsymmetrical_dimethylhydrazine.
- RD-0216 wikiPageWikiLink Vernier_thruster.
- RD-0216 wikiPageWikiLinkText "RD-0216".
- RD-0216 associated UR-100.
- RD-0216 associated "UR-100N, Rokot and Strela".
- RD-0216 combustionChamber "1".
- RD-0216 countryOfOrigin Soviet_Union.
- RD-0216 cycle Staged_combustion_cycle.
- RD-0216 designer Chemical_Automatics_Design_Bureau.
- RD-0216 firstDate "1965-04-19".
- RD-0216 firstDate "1973-04-09".
- RD-0216 fuel Unsymmetrical_dimethylhydrazine.
- RD-0216 manufacturer Krasny_Oktyabr_Closed_Joint-Stock_Company.
- RD-0216 manufacturer Proton-PM.
- RD-0216 name "RD-0216".
- RD-0216 name "RD-0235".
- RD-0216 oxidiser Dinitrogen_tetroxide.
- RD-0216 purpose "ICBM propulsion".
- RD-0216 status "Out of Production".
- RD-0216 status "Retired".
- RD-0216 successor RD-0216.
- RD-0216 type "liquid".
- RD-0216 usedIn "UR-100 Core Stage".
- RD-0216 usedIn "UR-100N Second Stage".
- RD-0216 wikiPageUsesTemplate Template:Convert.
- RD-0216 wikiPageUsesTemplate Template:Infobox_rocket_engine.
- RD-0216 wikiPageUsesTemplate Template:Portal.
- RD-0216 wikiPageUsesTemplate Template:Reflist.
- RD-0216 wikiPageUsesTemplate Template:Rocket-stub.
- RD-0216 wikiPageUsesTemplate Template:Rocket_Engines.
- RD-0216 subject Category:Rocket_engines.
- RD-0216 subject Category:Rocket_engines_of_the_Soviet_Union.
- RD-0216 subject Category:Rocket_engines_using_hypergolic_propellant.
- RD-0216 subject Category:Spaceflight.
- RD-0216 hypernym Engines.
- RD-0216 type Locomotive.
- RD-0216 comment "The RD-0216 and RD-0217 are liquid rocket engines, burning N2O4 and UDMH in the oxidizer rich staged combustion cycle. The only difference between the RD-0216 and the RD-0217 is that the latter has a heat exchanger to heat the pressuring gasses for the tanks. Three RD-0216 and one RD-0217 were used on the first stage of the UR-100 ICBM. The engines were manufactured until 1974 and stayed in operational use until 1991.".
- RD-0216 label "RD-0216".
- RD-0216 sameAs Q20203122.
- RD-0216 sameAs RD-0216.
- RD-0216 sameAs m.013f83kx.
- RD-0216 sameAs Q20203122.
- RD-0216 wasDerivedFrom RD-0216?oldid=682519373.
- RD-0216 homepage ?p=8&cat=10&prod=45.
- RD-0216 isPrimaryTopicOf RD-0216.