Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
10.06 meters
|
| gptkbp:engine |
5 J-2 engines
|
| gptkbp:firstFlight |
April 4, 1968
|
| http://www.w3.org/2000/01/rdf-schema#label |
Saturn II
|
| gptkbp:lastFlight |
May 14, 1973
|
| gptkbp:length |
24.87 meters
|
| gptkbp:manufacturer |
gptkb:North_American_Aviation
|
| gptkbp:mass |
496,200 kg (fully fueled)
|
| gptkbp:nickname |
gptkb:S-II
|
| gptkbp:partOf |
gptkb:Saturn_rocket_family
|
| gptkbp:propulsion |
liquid oxygen
liquid hydrogen |
| gptkbp:status |
retired
|
| gptkbp:thrust |
1,000,000 lbf
|
| gptkbp:usedFor |
gptkb:Apollo_program
Skylab launch |
| gptkbp:usedIn |
gptkb:Saturn_V
Saturn INT-21 Saturn V-B Saturn V-D |
| gptkbp:bfsParent |
gptkb:Encélado
|
| gptkbp:bfsLayer |
9
|