Statements (30)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:combustionChambers |
1
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:cycle |
gas-generator
|
| gptkbp:diameter |
1.14 m
|
| gptkbp:firstFlight |
1956
|
| gptkbp:fuelType |
gptkb:RP-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rocketdyne S-3D
|
| gptkbp:length |
2.92 m
|
| gptkbp:manufacturer |
gptkb:Rocketdyne
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:specificImpulseVacuum |
247 s
265 s |
| gptkbp:status |
retired
|
| gptkbp:successor |
gptkb:Rocketdyne_H-1
|
| gptkbp:thrustSeaLevel |
608 kN
|
| gptkbp:thrustVacuum |
667 kN
|
| gptkbp:usedFor |
missile propulsion
launch vehicle propulsion |
| gptkbp:usedIn |
gptkb:Juno_II
gptkb:Jupiter-C gptkb:SM-65_Atlas gptkb:Juno_I gptkb:Redstone_missile gptkb:PGM-17_Thor |
| gptkbp:weight |
725 kg
|
| gptkbp:bfsParent |
gptkb:Jupiter_IRBM
gptkb:Jupiter_missile |
| gptkbp:bfsLayer |
6
|