SM-65 Atlas

E52127

The SM-65 Atlas was the United States’ first operational intercontinental ballistic missile, later adapted as a pioneering space launch vehicle in the early space program.


Statements (48)
Predicate Object
instanceOf intercontinental ballistic missile
space launch vehicle
alsoKnownAs Atlas ICBM
configuration stage-and-a-half
countryOfOrigin United States
deploymentMode above-ground launchers
coffin-type shelters
silo-lift launchers
developedBy United States Air Force
developedUnderProgram Weapon System 107A-1
engineManufacturer Rocketdyne
engineType liquid-fuel rocket engine
enteredService 1959
firstFlightDate 1957-06-11
firstSuccessfulICBMFlightDate 1958-12-17
fuel RP-1 kerosene
guidanceSystem inertial guidance
radio-inertial guidance
launchedAstronaut John Glenn
launchedMission Mercury-Atlas 6
launchSitesUsed Cape Canaveral Air Force Station
Vandenberg Air Force Base
manufacturer Convair
maximumRange approximately 9000 miles
notableFeature balloon tank stainless-steel structure
thin-wall pressure-stabilized tanks
notableLaunch Friendship 7
oxidizer liquid oxygen
partOf United States nuclear deterrent
programStart early 1950s
propellantType liquid-fueled
retiredFromICBMService 1965
role orbital launch vehicle
strategic missile
status retired
successor Titan II ICBM
successorAsLaunchVehicle Atlas LV-3B
Atlas-Agena
Atlas-Centaur
usedAsLaunchVehicleFor Mercury program
Project Mercury crewed missions
early communications satellites
early weather satellites
scientific satellites
usedBy NASA
United States Air Force
usedIn Cold War
warheadType thermonuclear warhead

Referenced by (6)
Subject (surface form when different) Predicate
Atlas ("SM-65 Atlas ballistic missile")
Atlas-Centaur
developedFrom
United States rocket program ("Atlas rocket")
developed
Atlas-Centaur ("Atlas missile program")
heritage
Mercury program ("Atlas rocket")
launchVehicle
Convair ("SM-65 Atlas ICBM")
notableProduct

Please wait…