|
gptkbp:instanceOf
|
gptkb:surface-to-air_missile
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:diameter
|
3.05 m
|
|
gptkbp:engineType
|
Rocketdyne LR105
Rocketdyne LR89
|
|
gptkbp:enteredService
|
1959
|
|
gptkbp:firstFlight
|
1957-06-11
|
|
gptkbp:guidanceSystem
|
inertial guidance
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Convair SM-65 Atlas
|
|
gptkbp:launchMass
|
120,000 kg
|
|
gptkbp:length
|
22.1 m
|
|
gptkbp:manufacturer
|
gptkb:Convair
|
|
gptkbp:nickname
|
gptkb:Titan
|
|
gptkbp:notableMission
|
gptkb:Mercury-Atlas_7
gptkb:Mercury-Atlas_9
gptkb:Mercury-Atlas_6
|
|
gptkbp:propulsion
|
gptkb:RP-1_kerosene
liquid oxygen
|
|
gptkbp:range
|
14,000 km
|
|
gptkbp:retired
|
1965
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
gptkb:LGM-30_Minuteman
|
|
gptkbp:usedAs
|
space launch vehicle
|
|
gptkbp:usedBy
|
gptkb:United_States_Air_Force
|
|
gptkbp:usedIn
|
gptkb:Project_Mercury
gptkb:Project_Gemini_(as_Atlas-Agena)
|
|
gptkbp:variant
|
gptkb:Atlas_D
gptkb:Atlas_E
gptkb:Atlas_F
|
|
gptkbp:warheadType
|
gptkb:W49_thermonuclear_warhead
|
|
gptkbp:warheadYield
|
1.44 megatons
|
|
gptkbp:bfsParent
|
gptkb:Strategic_Air_Command_&_Aerospace_Museum
|
|
gptkbp:bfsLayer
|
6
|