Saturn IB second stage (S-IVB)
GPTKB entity
Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
6.6 m
|
| gptkbp:engineType |
gptkb:J-2
|
| gptkbp:firstFlight |
February 26, 1966
|
| https://www.w3.org/2000/01/rdf-schema#label |
Saturn IB second stage (S-IVB)
|
| 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:propulsion |
liquid oxygen
liquid hydrogen |
| gptkbp:status |
retired
|
| gptkbp:thrust |
1,033 kN
|
| gptkbp:usedIn |
gptkb:Apollo_7
gptkb:Apollo–Soyuz_Test_Project gptkb:Skylab |
| gptkbp:usedOn |
gptkb:Saturn_IB
gptkb:Saturn_V |
| gptkbp:bfsParent |
gptkb:J-2
|
| gptkbp:bfsLayer |
5
|