Statements (30)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:surface-to-air_missile
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:derivedFrom |
gptkb:Atlas-Agena
gptkb:Atlas_LV-3B |
| gptkbp:diameter |
3.05 m
|
| gptkbp:engineType |
gptkb:Rocketdyne_MA-2
|
| gptkbp:firstFlight |
1959
|
| gptkbp:guidanceSystem |
radio-inertial
|
| gptkbp:launchMass |
109,000 kg
|
| gptkbp:length |
25.5 m
|
| gptkbp:manufacturer |
gptkb:Convair
|
| gptkbp:notableMission |
Mercury-Atlas 6 (John Glenn orbital flight)
|
| gptkbp:numberBuilt |
63
|
| gptkbp:propulsion |
liquid oxygen and RP-1
|
| gptkbp:range |
14,000 km
|
| gptkbp:retired |
1965
|
| gptkbp:status |
retired
|
| gptkbp:usedAs |
gptkb:space_launch_vehicle
|
| gptkbp:usedBy |
gptkb:United_States_Air_Force
|
| gptkbp:usedIn |
gptkb:Project_Mercury
gptkb:Project_SCORE MIDAS satellite launches |
| gptkbp:warheadType |
gptkb:W49_thermonuclear
|
| gptkbp:warheadYield |
1.44 megatons
|
| gptkbp:bfsParent |
gptkb:SM-65_Atlas_missile_program
gptkb:Cape_Canaveral_LC-12 gptkb:Atlas_missile gptkb:LR89_rocket_engine |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Atlas D
|