Statements (17)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
6.52 m
|
| gptkbp:engine |
8 H-1 engines
|
| gptkbp:firstFlight |
1964
|
| gptkbp:length |
25.5 m
|
| gptkbp:manufacturer |
gptkb:Chrysler_Corporation
|
| gptkbp:mass |
500,000 kg
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:predecessor |
S-I Block I
|
| gptkbp:propulsion |
gptkb:RP-1
|
| gptkbp:thrust |
1,500,000 lbf
|
| gptkbp:usedIn |
gptkb:Apollo_program
gptkb:Saturn_I |
| gptkbp:bfsParent |
gptkb:Saturn_I_SA-5
|
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
S-I Block II
|