| dbo:MeanOfTransportation/diameter |
3.048 |
| dbo:MeanOfTransportation/height |
25149.048 |
| dbo:MeanOfTransportation/mass |
118843.2 |
| dbo:Rocket/mass |
118843.2 |
| 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. (en) 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. (fr) 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 . (pl) |
| dbo:diameter |
3.048000 (xsd:double) |
| dbo:failedLaunches |
32 (xsd:nonNegativeInteger) |
| dbo:finalFlight |
1967-11-07 (xsd:date) |
| dbo:height |
25.149048 (xsd:double) |
| dbo:launchSite |
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| dbo:maidenFlight |
1959-04-14 (xsd:date) |
| dbo:manufacturer |
dbr:Convair |
| dbo:mass |
118843200.000000 (xsd:double) |
| dbo:rocketFunction |
dbr:ICBM dbr:Expendable_launch_system |
| dbo:rocketStages |
1 (xsd:nonNegativeInteger) |
| dbo:status |
Retired |
| dbo:successfulLaunches |
103 (xsd:nonNegativeInteger) |
| dbo:thumbnail |
wiki-commons:Special:FilePath/Atlas-icbm-erection-large.jpg?width=300 |
| dbo:totalLaunches |
135 (xsd:nonNegativeInteger) |
| dbo:wikiPageID |
20870057 (xsd:integer) |
| dbo:wikiPageLength |
34877 (xsd:nonNegativeInteger) |
| dbo:wikiPageRevisionID |
1108431121 (xsd:integer) |
| dbo:wikiPageWikiLink |
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| dbp:caption |
0001-04-22 (xsd:gMonthDay) |
| dbp:countryOrigin |
United States (en) |
| dbp:fail |
32 (xsd:integer) |
| dbp:first |
1959-04-14 (xsd:date) |
| dbp:function |
dbr:ICBM dbr:Expendable_launch_system |
| dbp:last |
1967-11-07 (xsd:date) |
| dbp:launches |
135 (xsd:integer) |
| dbp:manufacturer |
dbr:Convair |
| dbp:name |
Atlas D (en) |
| dbp:sites |
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| dbp:stages |
1 (xsd:integer) |
| dbp:status |
Retired (en) |
| dbp:success |
103 (xsd:integer) |
| dbp:wikiPageUsesTemplate |
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| dcterms:subject |
dbc:Atlas_(rocket_family) dbc:Rockets_and_missiles |
| gold:hypernym |
dbr:Version |
| rdf:type |
owl:Thing dbo:MeanOfTransportation dbo:Work wikidata:Q41291 dbo:Rocket yago:WikicatRocketsAndMissiles yago:Artifact100021939 yago:Conveyance103100490 yago:Instrumentality103575240 yago:Object100002684 yago:PhysicalEntity100001930 yago:Rocket104099429 yago:Vehicle104524313 yago:Whole100003553 |
| rdfs:comment |
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. (fr) 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 . (pl) 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. (en) |
| rdfs:label |
SM-65D Atlas (en) SM-65D Atlas (fr) Atlas D (pl) SM-65D Atlas (pt) |
| owl:sameAs |
freebase:SM-65D Atlas yago-res:SM-65D Atlas wikidata:SM-65D Atlas dbpedia-fr:SM-65D Atlas dbpedia-gl:SM-65D Atlas dbpedia-he:SM-65D Atlas dbpedia-pl:SM-65D Atlas dbpedia-pt:SM-65D Atlas https://global.dbpedia.org/id/2gm5s |
| prov:wasDerivedFrom |
wikipedia-en:SM-65D_Atlas?oldid=1108431121&ns=0 |
| foaf:depiction |
wiki-commons:Special:FilePath/Atlas-icbm-erection-large.jpg |
| foaf:isPrimaryTopicOf |
wikipedia-en:SM-65D_Atlas |
| foaf:name |
Atlas D (SM-65D) (en) |
| is dbo:launchVehicle of |
dbr:Big_Joe_1 dbr:OV1-1 dbr:OV1-10 dbr:OV1-2 dbr:OV1-3 dbr:OV1-4 dbr:OV1-5 dbr:OV1-7 dbr:OV1-8 dbr:OV1-9 |
| is dbo:maidenFlightRocket of |
dbr:1959_in_spaceflight |
| is dbo:successor of |
dbr:Atlas_(rocket_family) |
| is dbo:wikiPageWikiLink of |
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| is dbp:launchRocket of |
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| is dbp:maidens of |
dbr:1959_in_spaceflight |
| is dbp:variantsWithTheirOwnArticles of |
dbr:Atlas_(rocket_family) |
| is foaf:primaryTopic of |
wikipedia-en:SM-65D_Atlas |
