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 |
1961
|
| gptkbp:lastFlight |
1975
|
| gptkbp:length |
24.8 m
|
| gptkbp:manufacturer |
gptkb:Chrysler_Corporation
|
| gptkbp:propulsion |
gptkb:RP-1
liquid oxygen |
| gptkbp:status |
retired
|
| gptkbp:thrust |
1,600,000 lbf
|
| gptkbp:usedOn |
gptkb:Saturn_I
gptkb:Saturn_IB |
| gptkbp:bfsParent |
gptkb:Pindad_SS2_rifle
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
SS2-V1
|