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- RD-0124 abstract "The RD-0124 (GRAU Index 14D23) is a rocket engine burning liquid oxygen and kerosene in a staged combustion cycle. RD-0124 engines are used on the Soyuz-2.1b and Soyuz-2-1v. A slight variation of the engine, the RD-0124A, is used on the Angara rocket family URM-2 upper stage. RD-0124 is developed by Khimavtomatiki Design Bureau.".
- RD-0124 wikiPageID "20953139".
- RD-0124 wikiPageLength "7415".
- RD-0124 wikiPageOutDegree "42".
- RD-0124 wikiPageRevisionID "689114156".
- RD-0124 wikiPageWikiLink Angara_(rocket_family).
- RD-0124 wikiPageWikiLink Antares_(rocket).
- RD-0124 wikiPageWikiLink Attitude_control.
- RD-0124 wikiPageWikiLink Castor_(rocket_stage).
- RD-0124 wikiPageWikiLink Category:Rocket_engines.
- RD-0124 wikiPageWikiLink Category:Rocket_engines_of_Russia.
- RD-0124 wikiPageWikiLink Category:Rocket_engines_using_kerosene_propellant.
- RD-0124 wikiPageWikiLink Category:Spaceflight.
- RD-0124 wikiPageWikiLink Chemical_Automatics_Design_Bureau.
- RD-0124 wikiPageWikiLink Comparison_of_orbital_rocket_engines.
- RD-0124 wikiPageWikiLink GRAU.
- RD-0124 wikiPageWikiLink Gas_generator.
- RD-0124 wikiPageWikiLink Kerosene.
- RD-0124 wikiPageWikiLink Liquid_oxygen.
- RD-0124 wikiPageWikiLink Orbital_Sciences_Corporation.
- RD-0124 wikiPageWikiLink RD-0110.
- RD-0124 wikiPageWikiLink RP-1.
- RD-0124 wikiPageWikiLink Regenerative_cooling_(rocket).
- RD-0124 wikiPageWikiLink Rocket_engine.
- RD-0124 wikiPageWikiLink Russia.
- RD-0124 wikiPageWikiLink Soyuz-2-1v.
- RD-0124 wikiPageWikiLink Soyuz-2-3.
- RD-0124 wikiPageWikiLink Soyuz-2_(rocket).
- RD-0124 wikiPageWikiLink Staged_combustion_cycle.
- RD-0124 wikiPageWikiLink Viktor_Gorokhov.
- RD-0124 wikiPageWikiLink Voronezh_Mechanical_Plant.
- RD-0124 wikiPageWikiLinkText "RD-0124".
- RD-0124 wikiPageWikiLinkText "RD-0124A".
- RD-0124 associated Soyuz-2_(rocket).
- RD-0124 burnTime "300.0".
- RD-0124 combustionChamber "4".
- RD-0124 countryOfOrigin Russia.
- RD-0124 cycle Staged_combustion_cycle.
- RD-0124 date "1993".
- RD-0124 designer "KBKhA".
- RD-0124 firstDate "2006-12-27".
- RD-0124 fuel RP-1.
- RD-0124 manufacturer Voronezh_Mechanical_Plant.
- RD-0124 name "RD-0124".
- RD-0124 oxidiser Liquid_oxygen.
- RD-0124 predecessor RD-0110.
- RD-0124 purpose "Upper Stage".
- RD-0124 specificImpulseVacuum "359.0".
- RD-0124 status "In Production".
- RD-0124 thrustToWeight "52.5".
- RD-0124 type "liquid".
- RD-0124 usedIn "Soyuz-2-1b and Soyuz-2-1v Block-I".
- RD-0124 wikiPageUsesTemplate Template:Convert.
- RD-0124 wikiPageUsesTemplate Template:Infobox_rocket_engine.
- RD-0124 wikiPageUsesTemplate Template:Reflist.
- RD-0124 wikiPageUsesTemplate Template:Rocket-stub.
- RD-0124 wikiPageUsesTemplate Template:Rocket_Engines.
- RD-0124 wikiPageUsesTemplate Template:Russian_and_Soviet_military_designation_sequences.
- RD-0124 subject Category:Rocket_engines.
- RD-0124 subject Category:Rocket_engines_of_Russia.
- RD-0124 subject Category:Rocket_engines_using_kerosene_propellant.
- RD-0124 subject Category:Spaceflight.
- RD-0124 hypernym Oxygen.
- RD-0124 comment "The RD-0124 (GRAU Index 14D23) is a rocket engine burning liquid oxygen and kerosene in a staged combustion cycle. RD-0124 engines are used on the Soyuz-2.1b and Soyuz-2-1v. A slight variation of the engine, the RD-0124A, is used on the Angara rocket family URM-2 upper stage. RD-0124 is developed by Khimavtomatiki Design Bureau.".
- RD-0124 label "RD-0124".
- RD-0124 sameAs Q620359.
- RD-0124 sameAs RD-0124.
- RD-0124 sameAs RD-0124.
- RD-0124 sameAs RD-0124.
- RD-0124 sameAs RD-0124.
- RD-0124 sameAs RD-0124.
- RD-0124 sameAs RD-0124.
- RD-0124 sameAs m.05b63r1.
- RD-0124 sameAs РД-0124.
- RD-0124 sameAs Q620359.
- RD-0124 wasDerivedFrom RD-0124?oldid=689114156.
- RD-0124 isPrimaryTopicOf RD-0124.