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SM-65_Atlas height "23114.0".
SM-65_Atlas abstract "Main article: Atlas (rocket family)The SM-65 Atlas was the first intercontinental ballistic missile (ICBM) developed and deployed by the United States. It was built for the U.S. Air Force by Convair Division of General Dynamics at the Kearny Mesa assembly plant north of San Diego, California. Atlas became operational as an ICBM in October 1959 and was used as a first stage for satellite launch vehicles for half a century. The Atlas missile's warhead was over 100 times more powerful than the bomb dropped over Nagasaki in 1945.An initial development contract was given to Consolidated Vultee Aircraft (Convair) on 16 January 1951 for what was then called MX-1593, but at a relatively low priority. The 1953 testing of the first dry fuel H-bomb in the Soviet Union led to the project being dramatically accelerated. The initial design completed by Convair in 1953 was larger than the missile that eventually entered service. Estimated warhead weight was lowered from 8,000 lb (3,630 kg) to 3,000 lb (1,360 kg) based on highly favorable U.S. nuclear warhead tests in early 1954, and on 14 May 1954 the Atlas program was formally given the highest national priority. A major development and test contract was awarded to Convair on 14 January 1955 for a 10-foot (3 m) diameter missile to weigh about 250,000 lb (113,400 kg). Atlas development was tightly controlled by the Air Force's Western Development Division, WDD, later part of the Air Force Ballistic Missile Division. Contracts for warhead, guidance and propulsion were handled separately by WDD. The first successful flight of a highly instrumented Atlas missile to full range occurred 28 November 1958. Atlas ICBMs were deployed operationally from 31 October 1959 to 12 April 1965.On 18 December 1958, the launch of Atlas 10B sent the missile into orbit around the Earth (without use of an upper stage) carrying the "SCORE" (Signal Communications by Orbiting Relay Equipment) communications payload. Atlas 10B/SCORE, at 8,750 lb (3,970 kg) was the heaviest man-made object then in orbit, the first voice relay satellite, and the first man-made object in space easily visible to the naked eye due to the large, mirror-polished stainless steel tank. This was the first flight in what would be a long career for the Atlas as a satellite launcher. Many retired Atlas ICBMs would be used as launch vehicles, most with an added spin-stabilized solid rocket motor upper stage for polar orbit military payloads. Even before its military use ended in 1965, Atlas had placed four Project Mercury astronauts in orbit and was becoming the foundation for a family of successful space launch vehicles, most notably Atlas Agena and Atlas Centaur.Mergers led to the acquisition of the Atlas Centaur line by Lockheed Martin which in turn became part of the United Launch Alliance. Today Lockheed Martin and ULA support a new Atlas rocket family based on the larger "Atlas V" which still uses the unique and highly efficient Centaur upper stage. Atlas V stage one is powered by a Russian RD-180 oxygen/kerosene engine and uses conventional aluminum isogrid tankage rather than the thin-wall, pressure-stabilized stainless steel tanks of the original Convair Atlas. Payload weights have increased along with launch vehicle weights over the years so the current Atlas V family serves many of the same type commercial, DoD, and planetary missions as earlier Atlas Centaurs.".
SM-65_Atlas countryOrigin United_States.
SM-65_Atlas failedLaunches "11".
SM-65_Atlas finalFlight "1959-08-24".
SM-65_Atlas height "23.114".
SM-65_Atlas maidenFlight "1957-06-06".
SM-65_Atlas manufacturer Convair.
SM-65_Atlas rocketFunction Intercontinental_ballistic_missile.
SM-65_Atlas rocketStages "1".
SM-65_Atlas status "Retired April 1965".
SM-65_Atlas successfulLaunches "13".
SM-65_Atlas thumbnail Atlas_missile_launch.jpg?width=300.
SM-65_Atlas totalLaunches "24".
SM-65_Atlas wikiPageExternalLink atlas.
SM-65_Atlas wikiPageExternalLink combat_sq_of_the_af_wwii.pdf.
SM-65_Atlas wikiPageExternalLink bossart.htm.
SM-65_Atlas wikiPageExternalLink atlasd.htm.
SM-65_Atlas wikiPageExternalLink www.atlasbases.homestead.com.
SM-65_Atlas wikiPageExternalLink m-16.html.
SM-65_Atlas wikiPageExternalLink Atlas-ICBM-Launched.htm.
SM-65_Atlas wikiPageExternalLink Karel%20Jan%20Bossart.
SM-65_Atlas wikiPageExternalLink index.php.
SM-65_Atlas wikiPageExternalLink atlas.htm.
SM-65_Atlas wikiPageExternalLink watch?v=Dg9PdW9yb3c.
SM-65_Atlas wikiPageID "101396".
SM-65_Atlas wikiPageRevisionID "626963488".
SM-65_Atlas align "center".
SM-65_Atlas caption "--02-20".
SM-65_Atlas caption "Atlas C missile sitting on its launch pad, 1957/58".
SM-65_Atlas caption "Atlas-B with Score payload, 1958".
SM-65_Atlas caption "Convair X-11 being launched".
SM-65_Atlas caption "Convair X-12 being launched".
SM-65_Atlas caption "Launch of an SM-65A Atlas from LC-12,".
SM-65_Atlas caption "Launch of an SM-65E Atlas".
SM-65_Atlas caption "Launch of an SM-65F Atlas".
SM-65_Atlas ceilingAlt "60.0".
SM-65_Atlas ceilingMain "40.0".
SM-65_Atlas comparableAircraftHeader "Comparable missiles".
SM-65_Atlas countryOrigin United_States.
SM-65_Atlas crew "Unmanned".
SM-65_Atlas description ""Atlas In Orbit. Radios Ike's Message Of Peace To World, 1958/12/22 "".
SM-65_Atlas designDate "1953".
SM-65_Atlas emptyWeightAlt "5670.0".
SM-65_Atlas emptyWeightMain "12500.0".
SM-65_Atlas fail "11".
SM-65_Atlas family Atlas_(rocket_family).
SM-65_Atlas first "1957-06-06".
SM-65_Atlas ft "10".
SM-65_Atlas ft "16".
SM-65_Atlas ft "75".
SM-65_Atlas ft "82".
SM-65_Atlas function Intercontinental_ballistic_missile.
SM-65_Atlas hasPhotoCollection SM-65_Atlas.
SM-65_Atlas height "2311.4".
SM-65_Atlas height "in ICBM configuration".
SM-65_Atlas id "1958-12-22".
SM-65_Atlas image "Atlas C.jpg".
SM-65_Atlas image "Atlas-B with Score payload.jpg".
SM-65_Atlas image "Atlas-E.jpg".
SM-65_Atlas image "Atlas-F.jpg".
SM-65_Atlas image "Convair X-11 launch.jpg".
SM-65_Atlas image "Convair X-12 launch.JPG".
SM-65_Atlas in "0".
SM-65_Atlas in "1".
SM-65_Atlas in "6".
SM-65_Atlas jetOrProp%3F_ "jet".
SM-65_Atlas last "1959-08-24".
SM-65_Atlas launches "24".
SM-65_Atlas lengthAlt "29.3 m".
SM-65_Atlas lengthMain "96.0".
SM-65_Atlas lists "* List of military aircraft of the United States * List of missiles".
SM-65_Atlas loadedWeightAlt "36300.0".
SM-65_Atlas loadedWeightMain "80000.0".
SM-65_Atlas manufacturer Convair.
SM-65_Atlas maxSpeedMain "Mach 10+".
SM-65_Atlas name "B-65/SM-65/CGM-16/HGM-16 Atlas".
SM-65_Atlas number ".".
SM-65_Atlas number "350".
SM-65_Atlas number "Peak deployment level of 129".
SM-65_Atlas numberOfJets "1".
SM-65_Atlas planeOrCopter%3F_ "plane".
SM-65_Atlas productionDate "1959".
SM-65_Atlas rangeAlt "690".
SM-65_Atlas rangeMain "600.0".
SM-65_Atlas seeAlso "*Strategic Air Command *WD-40".
SM-65_Atlas service "1959".
SM-65_Atlas similarAircraft "* SM-68 Titan I * SM-68 Titan II".
SM-65_Atlas spanAlt "3.66 m".
SM-65_Atlas spanMain "12.0".
SM-65_Atlas stages "1".
SM-65_Atlas status "Retired April 1965".
SM-65_Atlas success "13".
SM-65_Atlas typeOfJet Rocket_engine.
SM-65_Atlas variants "Atlas A, B/C, D, E/F".
SM-65_Atlas variants "SLV-3/3A/3C".
SM-65_Atlas width "112".
SM-65_Atlas width "113".
SM-65_Atlas width "125".
SM-65_Atlas width "130".