Statements (18)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
10.1 meters
|
| gptkbp:engine |
5 J-2 engines
|
| gptkbp:firstFlight |
1966
|
| gptkbp:height |
24.9 meters
|
| https://www.w3.org/2000/01/rdf-schema#label |
S-II
|
| gptkbp:manufacturer |
gptkb:North_American_Aviation
|
| gptkbp:mass |
480,000 kg (fully fueled)
|
| gptkbp:numberOfStages |
second stage
|
| gptkbp:propulsion |
liquid oxygen
liquid hydrogen |
| gptkbp:successor |
gptkb:S-IVB
|
| gptkbp:thrust |
5,000 kN
|
| gptkbp:usedFor |
gptkb:Apollo_missions
|
| gptkbp:usedIn |
gptkb:Saturn_V
|
| gptkbp:bfsParent |
gptkb:satellite
|
| gptkbp:bfsLayer |
4
|