Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:alsoKnownAs |
gptkb:S-IVB
|
| gptkbp:diameter |
6.6 m
|
| gptkbp:engineType |
gptkb:J-2
|
| gptkbp:firstFlight |
February 26, 1966
|
| gptkbp:launchMass |
119,000 kg
|
| gptkbp:length |
17.8 m
|
| gptkbp:manufacturer |
gptkb:Douglas_Aircraft_Company
|
| gptkbp:mass |
10,000 kg
|
| gptkbp:numberOfEngines |
1
|
| gptkbp:partOf |
gptkb:Saturn_IB
|
| gptkbp:propulsion |
liquid oxygen
liquid hydrogen |
| gptkbp:status |
retired
|
| gptkbp:thrust |
1,033 kN
|
| gptkbp:usedFor |
gptkb:Apollo_program
gptkb:Skylab_program |
| gptkbp:usedOn |
gptkb:Saturn_IB
gptkb:Saturn_V |
| gptkbp:bfsParent |
gptkb:RL10_rocket_engine
|
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
Saturn IB upper stage
|