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- RD-119 abstract "The RD-119 (GRAU Index 8D710) was a liquid rocket engine, burning liquid oxygen and UDMH in the Gas Generator cycle. It has a huge expansion ratio on the nozzle and uses a unique propellant combination to achieve an extremely high isp of 352s for a semi-cryogenic gas generator engine. It also has a unique steering mechanism. The engine main nozzle is fixed and the output of the gas generator is fed into four nozzles on the side of the engine. Instead of using gimbaled verniers to supply vector control, the combustion gases are distributed by an electrically driven system that can control the thrust among the nozzles.".
- RD-119 thumbnail RD-119_rocket_engine.jpg?width=300.
- RD-119 wikiPageExternalLink cosmos2.html.
- RD-119 wikiPageExternalLink www.npoenergomash.ru.
- RD-119 wikiPageID "47084620".
- RD-119 wikiPageLength "7014".
- RD-119 wikiPageOutDegree "40".
- RD-119 wikiPageRevisionID "699245712".
- RD-119 wikiPageWikiLink Category:Rocket_engines.
- RD-119 wikiPageWikiLink Category:Rocket_engines_of_the_Soviet_Union.
- RD-119 wikiPageWikiLink Category:Spaceflight.
- RD-119 wikiPageWikiLink GRAU.
- RD-119 wikiPageWikiLink Gas-generator_cycle.
- RD-119 wikiPageWikiLink Gimbaled_thrust.
- RD-119 wikiPageWikiLink Kosmos-2I.
- RD-119 wikiPageWikiLink Launch_vehicle.
- RD-119 wikiPageWikiLink Liquid-propellant_rocket.
- RD-119 wikiPageWikiLink Liquid_oxygen.
- RD-119 wikiPageWikiLink Mikhail_Yangel.
- RD-119 wikiPageWikiLink NPO_Energomash.
- RD-119 wikiPageWikiLink R-7_Semyorka.
- RD-119 wikiPageWikiLink Rocket_engine.
- RD-119 wikiPageWikiLink SS-4_Sandal.
- RD-119 wikiPageWikiLink Sergei_Korolev.
- RD-119 wikiPageWikiLink Soviet_Union.
- RD-119 wikiPageWikiLink Specific_impulse.
- RD-119 wikiPageWikiLink Theatre_ballistic_missile.
- RD-119 wikiPageWikiLink Thrust_vectoring.
- RD-119 wikiPageWikiLink Unsymmetrical_dimethylhydrazine.
- RD-119 wikiPageWikiLink Valentin_Glushko.
- RD-119 wikiPageWikiLink Vernier_thruster.
- RD-119 wikiPageWikiLink Yuzhnoye_Design_Office.
- RD-119 wikiPageWikiLinkText "RD-119".
- RD-119 associated Kosmos-2I.
- RD-119 burnTime "260.0".
- RD-119 caption "Museum of Space and Missile Technology . RD-119 rocket engine for Сosmos LV second stage.".
- RD-119 combustionChamber "1".
- RD-119 countryOfOrigin Soviet_Union.
- RD-119 cycle Gas-generator_cycle.
- RD-119 date "1960".
- RD-119 designer NPO_Energomash.
- RD-119 designer Valentin_Glushko.
- RD-119 fuel Unsymmetrical_dimethylhydrazine.
- RD-119 gimbal "Fixed with four fixed steering nozzles.".
- RD-119 imageSize "220".
- RD-119 mixtureRatio "1.5".
- RD-119 name "RD-119".
- RD-119 nozzleRatio "1350".
- RD-119 oxidiser Liquid_oxygen.
- RD-119 status "Out of Production".
- RD-119 type "liquid".
- RD-119 usedIn Kosmos-2I.
- RD-119 wikiPageUsesTemplate Template:Convert.
- RD-119 wikiPageUsesTemplate Template:Infobox_rocket_engine.
- RD-119 wikiPageUsesTemplate Template:Portal.
- RD-119 wikiPageUsesTemplate Template:Reflist.
- RD-119 wikiPageUsesTemplate Template:Rocket-stub.
- RD-119 wikiPageUsesTemplate Template:Rocket_Engines.
- RD-119 subject Category:Rocket_engines.
- RD-119 subject Category:Rocket_engines_of_the_Soviet_Union.
- RD-119 subject Category:Spaceflight.
- RD-119 hypernym Engine.
- RD-119 type Software.
- RD-119 comment "The RD-119 (GRAU Index 8D710) was a liquid rocket engine, burning liquid oxygen and UDMH in the Gas Generator cycle. It has a huge expansion ratio on the nozzle and uses a unique propellant combination to achieve an extremely high isp of 352s for a semi-cryogenic gas generator engine. It also has a unique steering mechanism. The engine main nozzle is fixed and the output of the gas generator is fed into four nozzles on the side of the engine.".
- RD-119 label "RD-119".
- RD-119 sameAs Q163790.
- RD-119 sameAs RD-119.
- RD-119 sameAs RD-119.
- RD-119 sameAs RD-119.
- RD-119 sameAs Q163790.
- RD-119 wasDerivedFrom RD-119?oldid=699245712.
- RD-119 depiction RD-119_rocket_engine.jpg.
- RD-119 homepage www.npoenergomash.ru.
- RD-119 isPrimaryTopicOf RD-119.