Atlas D missile

URI: https://gptkb.org/entity/Atlas_D_missile

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	14 April 1959
gptkbp:guidanceSystem	radio-inertial
https://www.w3.org/2000/01/rdf-schema#label	Atlas D missile
gptkbp:launchSite	gptkb:Vandenberg_Air_Force_Base gptkb:Cape_Canaveral
gptkbp:launchWeight	109,000 kg
gptkbp:length	25.5 m
gptkbp:manufacturer	gptkb:Convair
gptkbp:numberBuilt	63
gptkbp:propulsion	gptkb:water
gptkbp:range	14,480 km
gptkbp:retired	1965
gptkbp:status	retired
gptkbp:successor	gptkb:Atlas_E_missile
gptkbp:usedAs	space launch vehicle
gptkbp:usedBy	gptkb:United_States_Air_Force
gptkbp:usedIn	gptkb:Project_Mercury gptkb:Mercury-Atlas_7 gptkb:Project_SCORE gptkb:Mercury-Atlas_9 gptkb:Mercury-Atlas_6 gptkb:Mercury-Atlas_8
gptkbp:warheadType	gptkb:W49_thermonuclear
gptkbp:warheadYield	1.44 megatons
gptkbp:bfsParent	gptkb:Rocketdyne_MA-2
gptkbp:bfsLayer	5