Rocketdyne H-1

E259960

The Rocketdyne H-1 was a kerosene/liquid-oxygen rocket engine developed in the United States and used on early Saturn launch vehicles during the Apollo era.

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All labels observed (1)

Label Occurrences
Rocketdyne H-1 canonical 1

Statements (47)

Predicate Object
instanceOf chemical rocket engine
liquid-fuel rocket engine
chamberPressure about 48 bar
combustionChambers 1
coolingMethod regenerative cooling
countryOfOrigin United States of America
surface form: United States
cycle gas-generator cycle
developedFor early Saturn launch vehicles
developmentPeriod late 1950s
engineType open-cycle gas-generator engine
era Apollo program era
firstFlightUse Saturn I test flights
fuel RP-1 kerosene
gimbalCapability gimballed for thrust vector control
heritage derived from earlier Navaho and Thor/Jupiter engine technology
ignitionSystem pyrotechnic ignition
manufacturer Pratt & Whitney Rocketdyne
surface form: Rocketdyne
mountingConfiguration clustered engine arrangement
nozzles 1
numberPerStage 8 on Saturn I first stage
8 on Saturn IB first stage
oxidizer liquid oxygen
propellantFeed turbopump-fed
propellantMixtureRatio approximately 2.25:1 O/F
propellantType bipropellant
reusability expendable engine
specificImpulseSeaLevel about 263 s
specificImpulseVacuum about 289 s
status retired
successor RS-27 rocket engine
throttleCapability non-throttleable (on-off operation)
thrustSeaLevel about 188,000 lbf
about 836 kN
thrustVacuum about 205,000 lbf
about 912 kN
usedByAgency NASA
Army Ballistic Missile Agency
surface form: United States Army (via early Saturn development)
usedFor crew-rated launch vehicles
orbital launch
usedInMissionType Apollo test missions
Earth-orbit missions
usedInProgram Apollo program
usedOn Saturn I
Saturn IB
usedOnLaunchVehicleFamily Saturn rocket family
surface form: Saturn family of launch vehicles
usedOnStage Saturn I
surface form: Saturn I first stage S-I

Saturn IB
surface form: Saturn IB first stage S-IB

Referenced by (1)

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

Saturn I firstStageEngineType Rocketdyne H-1