Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:alsoKnownAs |
gptkb:S-IVB
|
| gptkbp:diameter |
6.6 m
|
| gptkbp:emptyWeight |
10,000 kg
|
| gptkbp:engineType |
gptkb:J-2
|
| gptkbp:firstFlight |
1966
|
| https://www.w3.org/2000/01/rdf-schema#label |
Saturn V upper stage
|
| gptkbp:length |
17.8 m
|
| gptkbp:manufacturer |
gptkb:Douglas_Aircraft_Company
|
| gptkbp:massLoaded |
119,000 kg
|
| gptkbp:numberOfEngines |
1
|
| gptkbp:partOf |
gptkb:Saturn_V
|
| gptkbp:propulsion |
liquid oxygen
liquid hydrogen |
| gptkbp:retired |
1973
|
| gptkbp:thrust |
1,033 kN
|
| gptkbp:usedFor |
trans-lunar injection
Earth orbit insertion |
| gptkbp:usedOn |
gptkb:Apollo–Soyuz_Test_Project
gptkb:Apollo_missions Skylab launch |
| gptkbp:bfsParent |
gptkb:NERVA_nuclear_rocket_program
|
| gptkbp:bfsLayer |
7
|