H-1
E701069
The H-1 was a liquid-fueled rocket engine developed in the United States and used on early Saturn launch vehicles during the Apollo era.
Statements (29)
| Predicate | Object |
|---|---|
| instanceOf |
liquid-fueled rocket engine
ⓘ
rocket engine ⓘ |
| combustionChamberCount | 1 ⓘ |
| countryOfOrigin |
United States of America
ⓘ
surface form:
United States
|
| developedFor |
Saturn I program
NERFINISHED
ⓘ
Saturn IB program NERFINISHED ⓘ |
| developedIn | United States NERFINISHED ⓘ |
| engineCycle | gas-generator cycle ⓘ |
| era | Apollo era ⓘ |
| fuel | RP-1 ⓘ |
| fuelType | kerosene ⓘ |
| generation | early Saturn rocket engine ⓘ |
| oxidizer | liquid oxygen ⓘ |
| propellantState | cryogenic oxidizer and room-temperature fuel ⓘ |
| propellantType | liquid propellant ⓘ |
| propulsionType | chemical rocket ⓘ |
| status | retired ⓘ |
| thrustPhase | liftoff ⓘ |
| usedByAgency | NASA NERFINISHED ⓘ |
| usedDuring | Apollo program NERFINISHED ⓘ |
| usedFor |
first stage propulsion
ⓘ
orbital launch ⓘ space launch ⓘ |
| usedInMissionType | Apollo test flights NERFINISHED ⓘ |
| usedOn |
Saturn I
NERFINISHED
ⓘ
Saturn IB NERFINISHED ⓘ |
| usedOnStage |
Saturn I first stage
NERFINISHED
ⓘ
Saturn IB first stage NERFINISHED ⓘ |
| usedOnVehicleFamily | Saturn launch vehicle NERFINISHED ⓘ |
Referenced by (1)
Full triples — surface form annotated when it differs from this entity's canonical label.