Statements (29)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
2.44 m
|
| gptkbp:engineType |
Rocketdyne LR79-NA-9
|
| gptkbp:firstFlight |
1957-01-26
|
| https://www.w3.org/2000/01/rdf-schema#label |
Thor DM-19
|
| gptkbp:launchSite |
gptkb:Vandenberg_Air_Force_Base
gptkb:Cape_Canaveral |
| gptkbp:length |
19.8 m
|
| gptkbp:manufacturer |
gptkb:Douglas_Aircraft_Company
|
| gptkbp:mass |
49,900 kg
|
| gptkbp:numberOfStages |
1
|
| gptkbp:propulsion |
gptkb:RP-1
liquid oxygen |
| gptkbp:purpose |
space launch vehicle
intermediate-range ballistic missile |
| gptkbp:retired |
1963
|
| gptkbp:rocketFamily |
Thor family
|
| gptkbp:status |
retired
|
| gptkbp:successor |
gptkb:satellite
|
| gptkbp:thrust |
667 kN
|
| gptkbp:usedBy |
gptkb:United_States_Air_Force
|
| gptkbp:usedIn |
Explorer 6 mission
Pioneer 1 mission Pioneer 3 mission Pioneer 4 mission Transit 1B mission |
| gptkbp:bfsParent |
gptkb:Thor-Delta
|
| gptkbp:bfsLayer |
6
|