Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
5.49 m
|
| gptkbp:engineType |
gptkb:RL10
|
| gptkbp:firstFlight |
1963
|
| gptkbp:grossMass |
45,359 kg
|
| gptkbp:length |
12.19 m
|
| gptkbp:manufacturer |
gptkb:Douglas_Aircraft_Company
|
| gptkbp:mass |
10,000 kg
|
| gptkbp:numberOfEngines |
6
|
| gptkbp:propulsion |
liquid oxygen
liquid hydrogen |
| gptkbp:thrustVacuum |
400 kN
|
| gptkbp:usedIn |
gptkb:SA-5
gptkb:SA-10 gptkb:SA-6 gptkb:SA-7 gptkb:SA-8 gptkb:SA-9 |
| gptkbp:usedOn |
gptkb:Saturn_I
|
| gptkbp:bfsParent |
gptkb:RL10_engine
gptkb:RL10_(second_stage) |
| gptkbp:bfsLayer |
7
|
| http://www.w3.org/2000/01/rdf-schema#label |
Saturn I S-IV stage
|