Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:surface-to-air_missile
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
3.05 m
|
| gptkbp:engineType |
Rocketdyne LR89 and LR105
|
| gptkbp:enteredService |
1959
|
| gptkbp:firstFlight |
1957
|
| gptkbp:guidanceSystem |
inertial guidance
|
| gptkbp:launchWeight |
120,000 lb
|
| gptkbp:length |
25.5 m
|
| gptkbp:manufacturer |
gptkb:Convair
|
| gptkbp:nickname |
gptkb:Titan
|
| gptkbp:notableMission |
gptkb:Mercury-Atlas_9
gptkb:Mercury-Atlas_6 |
| gptkbp:platform |
silo
surface pad |
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:range |
14,000 km
|
| gptkbp:retired |
1965
|
| gptkbp:status |
retired
|
| gptkbp:successor |
gptkb:LGM-30_Minuteman
|
| gptkbp:usedAs |
gptkb:space_launch_vehicle
|
| gptkbp:usedBy |
gptkb:United_States_Air_Force
|
| gptkbp:warheadType |
gptkb:W49_thermonuclear_warhead
|
| gptkbp:warheadYield |
1.44 megatons
|
| gptkbp:bfsParent |
gptkb:Atlas_LV-3
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
SM-65 Atlas ICBM
|