Statements (24)
| 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:firstFlight |
19 July 1958
|
| gptkbp:guidanceSystem |
radio-inertial guidance
|
| https://www.w3.org/2000/01/rdf-schema#label |
Atlas B missile
|
| gptkbp:launchMass |
109,000 kg
|
| gptkbp:length |
22.1 m
|
| gptkbp:manufacturer |
gptkb:Convair
|
| gptkbp:numberBuilt |
10
|
| gptkbp:partOf |
gptkb:SM-65_Atlas_program
|
| gptkbp:predecessor |
gptkb:Atlas_A_missile
|
| gptkbp:propulsion |
liquid oxygen and RP-1
|
| gptkbp:range |
10,360 km
|
| gptkbp:status |
retired
|
| gptkbp:successor |
gptkb:Atlas_D_missile
|
| gptkbp:usedBy |
gptkb:United_States_Air_Force
|
| gptkbp:usedFor |
test and development
|
| gptkbp:warheadType |
gptkb:W49_thermonuclear_warhead
|
| gptkbp:warheadYield |
1.44 megatons
|
| gptkbp:website |
gptkb:Cape_Canaveral
|
| gptkbp:bfsParent |
gptkb:Project_SCORE
|
| gptkbp:bfsLayer |
6
|