Statements (23)
| 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 |
1960
|
| gptkbp:guidanceSystem |
radio-inertial
|
| gptkbp:launchWeight |
117,900 kg
|
| gptkbp:length |
25.5 m
|
| gptkbp:manufacturer |
gptkb:Convair
|
| gptkbp:platform |
surface launch pad
|
| gptkbp:precededBy |
gptkb:Atlas_D_missile
|
| gptkbp:propulsion |
liquid oxygen and RP-1
|
| gptkbp:range |
14,480 km
|
| gptkbp:retired |
1965
|
| gptkbp:status |
retired
|
| gptkbp:successor |
Atlas F missile
|
| gptkbp:usedAs |
space launch vehicle (Atlas E space launch vehicle)
|
| gptkbp:usedBy |
gptkb:United_States_Air_Force
|
| gptkbp:warheadType |
W-49 thermonuclear
|
| gptkbp:warheadYield |
1.44 megatons
|
| gptkbp:bfsParent |
gptkb:Atlas_D_missile
|
| gptkbp:bfsLayer |
8
|
| http://www.w3.org/2000/01/rdf-schema#label |
Atlas E missile
|