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Statements

Subject Item
dbr:SM-65D_Atlas
rdf:type
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rdfs:label
Atlas D SM-65D Atlas SM-65D Atlas SM-65D Atlas
rdfs:comment
Atlas D – amerykańska jednostopniowa rakieta nośna, pierwotnie pocisk balistyczny. Był to pierwszy pocisk serii Atlas, który uzyskał status operacyjny (po locie 12D w 1959). Rakieta brała udział w pierwszym załogowym programie lotów kosmicznych, Mercury (pod nazwą Atlas LV-3B). W kategorii pocisków zastąpiona przez konstrukcje i , zaś w kategorii rakiet nośnych przez i . L'Atlas SM-65D, ou Atlas D, est la première version opérationnelle du missile SM-65 Atlas américain. L'Atlas D a d'abord été utilisé comme missile balistique intercontinental (ICBM) pour fournir une charge utile d'arme nucléaire sur une trajectoire suborbitale, avant d'être développé plus tard comme un véhicule de lancement pour transporter une charge utile en orbite terrestre basse par lui-même, puis plus tard en orbite géosynchrone, puis à la Lune, Vénus ou Mars avec les étages supérieurs Agena ou Centaur. L'Atlas D a été lancé depuis la base de lancement de Cap Canaveral en Floride. The SM-65D Atlas, or Atlas D, was the first operational version of the U.S. Atlas missile. Atlas D was first used as an intercontinental ballistic missile (ICBM) to deliver a nuclear weapon payload on a suborbital trajectory. It was later developed as a launch vehicle to carry a payload to low Earth orbit on its own, and later to geosynchronous orbit, to the Moon, Venus, or Mars with the Agena or Centaur upper stage. Atlas D was launched from Cape Canaveral Air Force Station, at Launch Complexes 11, 12, 13 and 14, and Vandenberg Air Force Base at Launch Complex 576.
foaf:name
Atlas D (SM-65D)
dbp:name
Atlas D
foaf:depiction
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dcterms:subject
dbc:Atlas_(rocket_family) dbc:Rockets_and_missiles
dbo:wikiPageID
20870057
dbo:wikiPageRevisionID
1108431121
dbo:wikiPageWikiLink
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dbp:sites
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dbo:thumbnail
n19:Atlas-icbm-erection-large.jpg?width=300
dbp:success
103
dbp:caption
0001-04-22
dbp:first
1959-04-14
dbp:last
1967-11-07
dbp:manufacturer
dbr:Convair
dbp:status
Retired
dbp:stages
1
dbo:abstract
The SM-65D Atlas, or Atlas D, was the first operational version of the U.S. Atlas missile. Atlas D was first used as an intercontinental ballistic missile (ICBM) to deliver a nuclear weapon payload on a suborbital trajectory. It was later developed as a launch vehicle to carry a payload to low Earth orbit on its own, and later to geosynchronous orbit, to the Moon, Venus, or Mars with the Agena or Centaur upper stage. Atlas D was launched from Cape Canaveral Air Force Station, at Launch Complexes 11, 12, 13 and 14, and Vandenberg Air Force Base at Launch Complex 576. The fully operational D-series Atlas was similar to the R&D model Atlas B and C, but incorporated a number of design changes implemented as a result of lessons learned during test flights. In addition, the D-series had the full-up Rocketdyne MA-2 propulsion system with 360,000 pounds-force (1,600 kN) of thrust versus the 250,000 pounds-force (1,100 kN) of thrust in the Atlas B/C's engines. Operational Atlas D missiles retained radio ground guidance aside from a few R&D launches which tested the inertial guidance system designed for the Atlas E/F, and the Atlas D would be the basis for most space launcher variants of Atlas. L'Atlas SM-65D, ou Atlas D, est la première version opérationnelle du missile SM-65 Atlas américain. L'Atlas D a d'abord été utilisé comme missile balistique intercontinental (ICBM) pour fournir une charge utile d'arme nucléaire sur une trajectoire suborbitale, avant d'être développé plus tard comme un véhicule de lancement pour transporter une charge utile en orbite terrestre basse par lui-même, puis plus tard en orbite géosynchrone, puis à la Lune, Vénus ou Mars avec les étages supérieurs Agena ou Centaur. L'Atlas D a été lancé depuis la base de lancement de Cap Canaveral en Floride. Atlas D – amerykańska jednostopniowa rakieta nośna, pierwotnie pocisk balistyczny. Był to pierwszy pocisk serii Atlas, który uzyskał status operacyjny (po locie 12D w 1959). Rakieta brała udział w pierwszym załogowym programie lotów kosmicznych, Mercury (pod nazwą Atlas LV-3B). W kategorii pocisków zastąpiona przez konstrukcje i , zaś w kategorii rakiet nośnych przez i .
dbp:countryOrigin
United States
dbp:fail
32
dbp:function
dbr:ICBM dbr:Expendable_launch_system
dbp:launches
135
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dbo:rocketFunction
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gold:hypernym
dbr:Version
dbo:finalFlight
1967-11-07
dbo:maidenFlight
1959-04-14
prov:wasDerivedFrom
wikipedia-en:SM-65D_Atlas?oldid=1108431121&ns=0
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3.048
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25149.048
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118843.2
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118843.2
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34877
dbo:diameter
3.048
dbo:failedLaunches
32
dbo:height
25.149048
dbo:mass
118843200.0
dbo:status
Retired
dbo:successfulLaunches
103
dbo:totalLaunches
135
dbo:rocketStages
1
dbo:manufacturer
dbr:Convair
foaf:isPrimaryTopicOf
wikipedia-en:SM-65D_Atlas