Statements (34)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
10.1 meters
|
| gptkbp:engineType |
gptkb:J-2
|
| gptkbp:firstFlight |
1966
|
| gptkbp:followedBy |
gptkb:Saturn_V_S-IVB
|
| https://www.w3.org/2000/01/rdf-schema#label |
Saturn V S-II
|
| gptkbp:length |
24.9 meters
|
| gptkbp:manufacturer |
gptkb:North_American_Aviation
|
| gptkbp:massWhenEmpty |
36,600 kg
|
| gptkbp:massWhenFueled |
481,300 kg
|
| gptkbp:numberOfEngines |
5
|
| gptkbp:numberOfStages |
2
|
| gptkbp:precededBy |
gptkb:Saturn_V_S-IC
|
| gptkbp:propulsion |
liquid oxygen
liquid hydrogen |
| gptkbp:status |
retired
|
| gptkbp:thrust |
5,000 kN
|
| gptkbp:usedIn |
gptkb:Apollo_11
gptkb:Apollo_12 gptkb:Apollo_10 gptkb:Apollo_16 gptkb:Apollo_6 gptkb:Apollo_4 gptkb:Apollo_13 gptkb:Apollo_17 gptkb:Apollo_8 gptkb:Apollo_14 gptkb:Apollo_15 gptkb:Apollo_9 |
| gptkbp:usedOn |
gptkb:Saturn_V
|
| gptkbp:bfsParent |
gptkb:J-2_rocket_engine
gptkb:J-2_engine |
| gptkbp:bfsLayer |
7
|