Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:developedBy |
gptkb:Apollo_program
|
| gptkbp:diameter |
21.7 feet
|
| gptkbp:enginesFirstStage |
8 × H-1
|
| gptkbp:enginesSecondStage |
1 × J-2
|
| gptkbp:family |
gptkb:Saturn_rocket_family
|
| gptkbp:firstFlight |
1966-02-26
|
| gptkbp:height |
68 feet
|
| gptkbp:launchSite |
gptkb:Kennedy_Space_Center
gptkb:Cape_Canaveral |
| gptkbp:manufacturer |
gptkb:NASA
|
| gptkbp:mass |
590,000 kg
|
| gptkbp:numberOfStages |
2
|
| gptkbp:propellantFirstStage |
RP-1/LOX
LH2/LOX |
| gptkbp:status |
retired
|
| gptkbp:testFlights |
gptkb:AS-201
gptkb:AS-202 gptkb:AS-203 |
| gptkbp:usedFor |
test flights
|
| gptkbp:bfsParent |
gptkb:F-1_engine
|
| gptkbp:bfsLayer |
7
|
| http://www.w3.org/2000/01/rdf-schema#label |
Saturn IB (test only)
|