Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:cycle |
gas-generator
|
| gptkbp:derivedFrom |
gptkb:Rocketdyne_S-3D
|
| gptkbp:diameter |
3.8 ft
|
| gptkbp:firstFlight |
1961
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rocketdyne H-1
|
| gptkbp:length |
12.7 ft
|
| gptkbp:manufacturer |
gptkb:Rocketdyne
|
| gptkbp:mass |
1,905 kg
|
| gptkbp:numberBuilt |
over 140
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:propulsion |
gptkb:RP-1
|
| gptkbp:specificImpulseVacuum |
263 s
289 s |
| gptkbp:status |
retired
|
| gptkbp:thrustSeaLevel |
188,000 lbf
|
| gptkbp:thrustVacuum |
188,000 lbf
|
| gptkbp:usedFor |
launch vehicle propulsion
|
| gptkbp:usedIn |
gptkb:Saturn_I
gptkb:Saturn_IB |
| gptkbp:usedOn |
first stage of Saturn I
first stage of Saturn IB |
| gptkbp:bfsParent |
gptkb:Rocketdyne_S-3D
|
| gptkbp:bfsLayer |
7
|