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- RD-0124 abstract "The RD-0124 is a rocket engine burning liquid oxygen and kerosene in a staged combustion cycle. RD-0124 engines are used on the Soyuz-2.1b. A modification of the engine will also be used on the second stage of some rockets in the planned Angara rocket family. RD-0124 is developed by Khimavtomatiki Design Bureau.".
- RD-0124 wikiPageID "20953139".
- RD-0124 wikiPageRevisionID "604982010".
- RD-0124 chamberPressure "162.0".
- RD-0124 countryOfOrigin Russia.
- RD-0124 cycle Staged_combustion_cycle.
- RD-0124 date "2001".
- RD-0124 designer Chemical_Automatics_Design_Bureau.
- RD-0124 diameter "2.4 m".
- RD-0124 dryWeight "480.0".
- RD-0124 fuel RP-1.
- RD-0124 hasPhotoCollection RD-0124.
- RD-0124 length "1.58 m".
- RD-0124 manufacturer Progress_State_Research_and_Production_Rocket_Space_Center.
- RD-0124 name "RD-0124".
- RD-0124 oxidiser Liquid_oxygen.
- RD-0124 predecessor RD-0110.
- RD-0124 purpose "Upper stage booster".
- RD-0124 specificImpulseSeaLevel "331.0".
- RD-0124 specificImpulseVacuum "359.0".
- RD-0124 status "In use".
- RD-0124 thrust(vac)_ "294.3 kN".
- RD-0124 type "liquid".
- RD-0124 subject Category:Kerosene_rocket_engines.
- RD-0124 subject Category:Rocket_engines.
- RD-0124 subject Category:Rocket_engines_of_the_Soviet_Union.
- RD-0124 comment "The RD-0124 is a rocket engine burning liquid oxygen and kerosene in a staged combustion cycle. RD-0124 engines are used on the Soyuz-2.1b. A modification of the engine will also be used on the second stage of some rockets in the planned Angara rocket family. RD-0124 is developed by Khimavtomatiki Design Bureau.".
- RD-0124 label "RD-0124".
- RD-0124 label "RD-0124".
- RD-0124 label "RD-0124".
- RD-0124 label "РД-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 Q620359.
- RD-0124 sameAs Q620359.
- RD-0124 wasDerivedFrom RD-0124?oldid=604982010.
- RD-0124 isPrimaryTopicOf RD-0124.