RD-120

E766013

The RD-120 is a Soviet-designed liquid-fueled rocket engine used on medium-lift launch vehicles, notable for its high performance and role in powering upper stages of space launch systems.

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Statements (46)

Predicate Object
instanceOf liquid-fueled rocket engine
applicationDomain space launch
chamberPressure_bar ~147
combustionMode single-shaft turbopump
coolingMethod regenerative cooling
countryOfOrigin Soviet Union
designedFor Zenit family of launch vehicles NERFINISHED
designer NPO Energomash NERFINISHED
developedIn 1980s
engineCycle staged combustion cycle
engineType liquid rocket engine
firstFlightVehicle Zenit-2 NERFINISHED
fuel kerosene
gimbalCapability yes
guidanceRole provides thrust vector control via gimbaling
launchVehicleFamily Zenit NERFINISHED
manufacturer NPO Energomash NERFINISHED
nozzleExpansionRatio optimized for upper-stage operation
numberOfCombustionChambers 1
originLanguageName РД-120 NERFINISHED
oxidizer liquid oxygen
oxidizerRich true
performanceCharacteristic high specific impulse for kerosene/LOX class
propellantCombination LOX/RP-1
propellantType kerosene (RP-1)
liquid oxygen (LOX)
relatedEngine RD-170 NERFINISHED
RD-171 NERFINISHED
reusability expendable
specificImpulseSeaLevel_s ~309
specificImpulseVacuum_s ~350
stageApplication second stage
status operational
successor RD-120K NERFINISHED
throttleCapability limited
thrustSeaLevel_kN ~740
thrustVacuum_kN ~833
usedBy Russian space program
Soviet space program NERFINISHED
Ukrainian launch vehicles
usedFor medium-lift launch vehicles
orbital launch
upper stages of space launch systems
usedIn Zenit-2 launch vehicle NERFINISHED
Zenit-3SL launch vehicle
Zenit-3SLB launch vehicle NERFINISHED

Referenced by (1)

Full triples — surface form annotated when it differs from this entity's canonical label.