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- RD-0110R abstract "The RD-0110R (GRAU Index 14D24) is a rocket engine burning liquid oxygen and kerosene in a gas generator combustion cycle. It has four nozzles that can gimbal up to 45 degrees in a single axis and is used as the vernier thruster on the Soyuz-2-1v first stage. It also has heat exchangers that heats oxygen and He to pressurize the LOX and RG-1 tanks of the Soyuz-2.1v first stage, respectively. The Oxygen is supplied from the same LOX tank in liquid form, while the He is supplied from separate high pressure bottles (known as the T tank).The engine's development started in 2010 and it is a heavily modified version of the RD-0110. The main areas of work were shortening the nozzles to optimized them for the atmospheric part of the flight (the RD-0110 is a vacuum optimized engine), propellant piping, heat exchangers and the gimballing system, which was developed by TsSKB Progress. The RD-0110R engines is produced on the Voronezh Mechanical Plant.".
- RD-0110R wikiPageExternalLink liquid-rocket-engine.
- RD-0110R wikiPageExternalLink en.samspace.ru.
- RD-0110R wikiPageExternalLink www.kbkha.ru.
- RD-0110R wikiPageID "46864355".
- RD-0110R wikiPageLength "4155".
- RD-0110R wikiPageOutDegree "29".
- RD-0110R wikiPageRevisionID "704349709".
- RD-0110R wikiPageWikiLink Category:Rocket_engines.
- RD-0110R wikiPageWikiLink Category:Rocket_engines_of_Russia.
- RD-0110R wikiPageWikiLink Category:Rocket_engines_of_the_Soviet_Union.
- RD-0110R wikiPageWikiLink Category:Rocket_engines_using_kerosene_propellant.
- RD-0110R wikiPageWikiLink Category:Spaceflight.
- RD-0110R wikiPageWikiLink Chemical_Automatics_Design_Bureau.
- RD-0110R wikiPageWikiLink GRAU.
- RD-0110R wikiPageWikiLink Gas-generator_cycle.
- RD-0110R wikiPageWikiLink Helium.
- RD-0110R wikiPageWikiLink Kerosene.
- RD-0110R wikiPageWikiLink Liquid_oxygen.
- RD-0110R wikiPageWikiLink Oxygen.
- RD-0110R wikiPageWikiLink Progress_State_Research_and_Production_Rocket_Space_Center.
- RD-0110R wikiPageWikiLink RD-0110.
- RD-0110R wikiPageWikiLink RP-1.
- RD-0110R wikiPageWikiLink Rocket_engine.
- RD-0110R wikiPageWikiLink Russia.
- RD-0110R wikiPageWikiLink Soyuz-2-1v.
- RD-0110R wikiPageWikiLink Vernier_thruster.
- RD-0110R wikiPageWikiLink Voronezh_Mechanical_Plant.
- RD-0110R wikiPageWikiLinkText "RD-0110R".
- RD-0110R associated Soyuz-2-1v.
- RD-0110R burnTime "210.0".
- RD-0110R combustionChamber "4".
- RD-0110R countryOfOrigin Russia.
- RD-0110R cycle Gas-generator_cycle.
- RD-0110R designer "KBKhA, Viktor Gorokhov".
- RD-0110R firstDate "2013-12-28".
- RD-0110R fuel RP-1.
- RD-0110R manufacturer Voronezh_Mechanical_Plant.
- RD-0110R name "RD-0110R".
- RD-0110R oxidiser Liquid_oxygen.
- RD-0110R predecessor RD-0110.
- RD-0110R purpose "1".
- RD-0110R specificImpulseSeaLevel "259.4".
- RD-0110R specificImpulseVacuum "298.4".
- RD-0110R status "In Production".
- RD-0110R type "liquid".
- RD-0110R usedIn "Soyuz-2-1v first stage.".
- RD-0110R wikiPageUsesTemplate Template:Convert.
- RD-0110R wikiPageUsesTemplate Template:Infobox_rocket_engine.
- RD-0110R wikiPageUsesTemplate Template:Reflist.
- RD-0110R wikiPageUsesTemplate Template:Rocket-stub.
- RD-0110R wikiPageUsesTemplate Template:Rocket_Engines.
- RD-0110R subject Category:Rocket_engines.
- RD-0110R subject Category:Rocket_engines_of_Russia.
- RD-0110R subject Category:Rocket_engines_of_the_Soviet_Union.
- RD-0110R subject Category:Rocket_engines_using_kerosene_propellant.
- RD-0110R subject Category:Spaceflight.
- RD-0110R hypernym Oxygen.
- RD-0110R comment "The RD-0110R (GRAU Index 14D24) is a rocket engine burning liquid oxygen and kerosene in a gas generator combustion cycle. It has four nozzles that can gimbal up to 45 degrees in a single axis and is used as the vernier thruster on the Soyuz-2-1v first stage. It also has heat exchangers that heats oxygen and He to pressurize the LOX and RG-1 tanks of the Soyuz-2.1v first stage, respectively.".
- RD-0110R label "RD-0110R".
- RD-0110R sameAs Q12146473.
- RD-0110R sameAs m.013b8cq6.
- RD-0110R sameAs РД-0110Р.
- RD-0110R sameAs РД-0110Р.
- RD-0110R sameAs Q12146473.
- RD-0110R wasDerivedFrom RD-0110R?oldid=704349709.
- RD-0110R isPrimaryTopicOf RD-0110R.