Statements (30)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:burnTime |
up to 475 seconds
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
6.6 meters
|
| gptkbp:emptyWeight |
10,000 kg
|
| gptkbp:engine |
gptkb:J-2
|
| gptkbp:firstFlight |
February 26, 1966
|
| gptkbp:length |
17.81 meters
|
| gptkbp:manufacturer |
gptkb:Douglas_Aircraft_Company
|
| gptkbp:mass |
119,000 kg
|
| gptkbp:notableMission |
gptkb:Apollo_11
gptkb:Skylab_1 gptkb:Apollo_13 gptkb:Apollo_8 |
| gptkbp:numberBuilt |
17
|
| gptkbp:propulsion |
liquid oxygen
liquid hydrogen |
| gptkbp:restartedInOrbit |
yes
|
| gptkbp:status |
retired
|
| gptkbp:thrust |
1,033 kN
|
| gptkbp:usedAs |
second stage of Saturn IB
third stage of Saturn V |
| gptkbp:usedFor |
gptkb:Trans-lunar_injection
gptkb:Apollo_missions Skylab launch |
| gptkbp:usedIn |
gptkb:Saturn_IB
gptkb:Saturn_V |
| gptkbp:bfsParent |
gptkb:Saturn_IB
|
| gptkbp:bfsLayer |
6
|
| https://www.w3.org/2000/01/rdf-schema#label |
S-IVB
|