SM-65 Atlas

URI: https://gptkb.org/entity/SM-65_Atlas

GPTKB entity

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
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	gptkb:surface silo
gptkbp:propulsion	gptkb:water
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:warheadType	gptkb:W49_thermonuclear_warhead
gptkbp:warheadYield	1.44 megatons
gptkbp:bfsParent	gptkb:Space_Launch_Complex_576G gptkb:Space_Launch_Complex_576R gptkb:Strategic_Air_Command
gptkbp:bfsLayer	6
https://www.w3.org/2000/01/rdf-schema#label	SM-65 Atlas