Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:derivedFrom |
gptkb:S-3D_engine
|
| gptkbp:engineCycle |
gas-generator
|
| gptkbp:fuelType |
gptkb:RP-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
H-1 rocket engine
|
| gptkbp:manufacturer |
gptkb:Rocketdyne
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:status |
retired
|
| gptkbp:thrustSeaLevel |
165,000 lbf
|
| gptkbp:thrustVacuum |
188,000 lbf
|
| gptkbp:usedIn |
gptkb:Saturn_I
gptkb:Saturn_IB |
| gptkbp:usedInFirstFlight |
1961
|
| gptkbp:usedInLastFlight |
1975
|
| gptkbp:usedInStage |
first stage
|
| gptkbp:vehicleType |
gptkb:Apollo_program
|
| gptkbp:bfsParent |
gptkb:RS-27
gptkb:Rocketdyne |
| gptkbp:bfsLayer |
6
|