Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:surface-to-air_missile
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:deployment |
gptkb:Italy
gptkb:Turkey gptkb:United_Kingdom |
| gptkbp:derivedFrom |
gptkb:Delta_rocket_family
|
| gptkbp:diameter |
2.44 m
|
| gptkbp:engine |
gptkb:Rocketdyne_LR79
|
| gptkbp:enteredService |
1959
|
| gptkbp:firstFlight |
1957
|
| gptkbp:guidanceSystem |
inertial
|
| https://www.w3.org/2000/01/rdf-schema#label |
Thor IRBM
|
| gptkbp:launchWeight |
49,900 kg
|
| gptkbp:length |
19.8 m
|
| gptkbp:manufacturer |
gptkb:Douglas_Aircraft_Company
|
| gptkbp:NATOReportingName |
gptkb:Thor
|
| gptkbp:notableFor |
first operational IRBM of the US
|
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:range |
2,400 km
|
| gptkbp:retired |
1963
|
| gptkbp:type |
intermediate-range ballistic missile
|
| gptkbp:usedBy |
gptkb:Royal_Air_Force
gptkb:United_States_Air_Force |
| gptkbp:warheadType |
gptkb:W49_thermonuclear
|
| gptkbp:warheadYield |
1.44 megatons
|
| gptkbp:bfsParent |
gptkb:Strategic_Air_Command_&_Aerospace_Museum
|
| gptkbp:bfsLayer |
6
|