Statements (33)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:satellite
|
| gptkbp:book |
dummy stage
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
6.52 meters
|
| gptkbp:engineType |
gptkb:H-1
|
| gptkbp:firstFlight |
1961-10-27
|
| gptkbp:flightNumber |
4
|
| gptkbp:height |
55 meters
|
| https://www.w3.org/2000/01/rdf-schema#label |
Saturn I Block 1 rocket
|
| gptkbp:lastFlight |
1963-01-29
|
| gptkbp:launchSite |
gptkb:Cape_Canaveral_LC-34
|
| gptkbp:manufacturer |
gptkb:NASA
gptkb:Chrysler |
| gptkbp:mass |
524,000 kg
|
| gptkbp:notableMission |
gptkb:SA-1
SA-3 SA-2 SA-4 |
| gptkbp:numberOfEngines |
8
|
| gptkbp:numberOfStages |
gptkb:S-I
2 |
| gptkbp:payloadToLEO |
9,000 kg
|
| gptkbp:predecessor |
none
|
| gptkbp:program |
gptkb:Apollo_program
|
| gptkbp:propulsion |
gptkb:RP-1
liquid oxygen |
| gptkbp:purpose |
test vehicle
|
| gptkbp:status |
retired
|
| gptkbp:successor |
gptkb:Saturn_I_Block_2_rocket
|
| gptkbp:successRate |
100%
|
| gptkbp:usedBy |
gptkb:NASA
|
| gptkbp:bfsParent |
gptkb:Saturn_I_Block_2_rocket
|
| gptkbp:bfsLayer |
6
|