Statements (28)
| 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
|
| https://www.w3.org/2000/01/rdf-schema#label |
SM-65 Atlas
|
| gptkbp:launchMass |
120,000 kg
|
| gptkbp:length |
22.1 m
|
| gptkbp:manufacturer |
gptkb:Convair
|
| gptkbp:notableDerivative |
gptkb:Atlas-Agena
gptkb:Atlas-Centaur gptkb:Atlas_LV-3B |
| gptkbp:notableMission |
gptkb:Mercury-Atlas_6
|
| gptkbp:platform |
surface
silo |
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:range |
14,000 km
|
| gptkbp:retired |
1965
|
| gptkbp:status |
retired
|
| gptkbp:usedAs |
space launch vehicle
|
| gptkbp:usedBy |
gptkb:United_States_Air_Force
|
| gptkbp:warheadType |
gptkb:W49_thermonuclear_warhead
|
| gptkbp:warheadYield |
1.44 megatons
|
| gptkbp:bfsParent |
gptkb:USAF_Strategic_Air_Command
gptkb:Strategic_Air_Command |
| gptkbp:bfsLayer |
5
|