NK-33 engine

E443694

The NK-33 engine is a Soviet-era high-performance liquid-fuel rocket engine originally developed for the N1 lunar rocket program, known for its efficiency and thrust-to-weight ratio.

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Observed surface forms (1)

Surface form Occurrences
NK-33 0

Statements (48)

Predicate Object
instanceOf liquid-fuel rocket engine
rocket engine
application first-stage propulsion
chamberPressure_bar ~147
combustionMode oxygen-rich
coolingMethod regenerative cooling
countryOfOrigin Soviet Union
cycleType oxygen-rich staged combustion
derivative AJ26
designer Nikolai Kuznetsov NERFINISHED
developmentPeriod 1960s
engineType open-cycle staged combustion (oxygen-rich)
era Soviet era
exportVersion AJ26
firstFlightUse N1 test flights
fuel RP-1 kerosene
gimbalRange_deg about 5
heritageFrom N1 first-stage propulsion system
intendedForVehicle N1 lunar rocket NERFINISHED
manufacturer Kuznetsov Design Bureau NERFINISHED
mountingConfiguration clustered on N1 first stage
notableFeature high specific impulse for kerosene engine
high thrust-to-weight ratio
oxygen-rich staged combustion in kerosene engine
nozzleType bell nozzle
numberOfCombustionChambers 1
numberOfNozzles 1
oxidizer liquid oxygen
program N1-L3 lunar program NERFINISHED
propellantFeedSystem turbopump-fed
propellantType liquid oxygen / RP-1
restartCapability single-start
specificImpulseSeaLevel_s ~297
specificImpulseVacuum_s ~331
status heritage engine
in service
storageHistory long-term storage after N1 cancellation
successorInFamily NK-33A NERFINISHED
throttleCapability limited
thrustSeaLevel_kN ~1500
thrustToWeightRatio high
thrustVacuum_kN ~1715
usedBy Orbital Sciences Corporation NERFINISHED
Russian space program NERFINISHED
Soviet space program NERFINISHED
usedFor orbital launch vehicles
usedOnVehicle Antares 100 series NERFINISHED
Soyuz-2-1v NERFINISHED

Referenced by (1)

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

RP-1 usedInEngine NK-33 engine