About: Atlas H

An Entity of Type: rocket, from Named Graph: http://dbpedia.org, within Data Space: dbpedia.org:8891

The Atlas H was an American expendable launch system derived from the SM-65 Atlas missile. It was a member of the Atlas family of rockets, and was used to launch five clusters of NOSS satellites for the US National Reconnaissance Office. Two flights also carried LiPS satellites, as secondary payloads for the United States Naval Research Laboratory. Atlas H could put a payload of 3,630 kg (8,000 lb) into low Earth orbit, or a payload of 2,255 kg (4,971 lb) into a geostationary transfer orbit.

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dbo:abstract
  • The Atlas H was an American expendable launch system derived from the SM-65 Atlas missile. It was a member of the Atlas family of rockets, and was used to launch five clusters of NOSS satellites for the US National Reconnaissance Office. Two flights also carried LiPS satellites, as secondary payloads for the United States Naval Research Laboratory. The Atlas H was a stage and a half rocket, using the enhanced Atlas rocket designed for use as the first stage of the Atlas G rocket, which differed from the Atlas H in having a Centaur upper stage. This stage was later reused as the first stage of the Atlas I. In practice, an upper stage was flown on all five launches. Atlas H could put a payload of 3,630 kg (8,000 lb) into low Earth orbit, or a payload of 2,255 kg (4,971 lb) into a geostationary transfer orbit. (en)
  • O Atlas H, foi um veículo de lançamento descartável de origem Norte americana. Originalmente projetado e construido pela Divisão Convair da General Dynamics em San Diego, na Califórnia. Ele fazia parte da família Atlas de foguetes e foi criado a partir do míssil SM-65 Atlas. O Atlas H, foi usado para lançar cinco satélites militares de geolocalização para a Marinha dos Estados Unidos. (pt)
dbo:finalFlight
  • 1987-05-15 (xsd:date)
dbo:launchSite
dbo:maidenFlight
  • 1983-02-09 (xsd:date)
dbo:manufacturer
dbo:rocketFunction
dbo:status
  • Retired
dbo:successfulLaunches
  • 5 (xsd:nonNegativeInteger)
dbo:thumbnail
dbo:totalLaunches
  • 5 (xsd:nonNegativeInteger)
dbo:wikiPageID
  • 21343567 (xsd:integer)
dbo:wikiPageLength
  • 2085 (xsd:nonNegativeInteger)
dbo:wikiPageRevisionID
  • 1084018251 (xsd:integer)
dbo:wikiPageWikiLink
dbp:caption
  • Launch of the last Atlas H with NOSS-9. (en)
dbp:countryOrigin
  • United States (en)
dbp:first
  • 1983-02-09 (xsd:date)
dbp:function
dbp:last
  • 1987-05-15 (xsd:date)
dbp:launches
  • 5 (xsd:integer)
dbp:manufacturer
dbp:name
  • Atlas H (en)
dbp:sites
dbp:status
  • Retired (en)
dbp:success
  • 5 (xsd:integer)
dbp:wikiPageUsesTemplate
dcterms:subject
gold:hypernym
rdf:type
rdfs:comment
  • O Atlas H, foi um veículo de lançamento descartável de origem Norte americana. Originalmente projetado e construido pela Divisão Convair da General Dynamics em San Diego, na Califórnia. Ele fazia parte da família Atlas de foguetes e foi criado a partir do míssil SM-65 Atlas. O Atlas H, foi usado para lançar cinco satélites militares de geolocalização para a Marinha dos Estados Unidos. (pt)
  • The Atlas H was an American expendable launch system derived from the SM-65 Atlas missile. It was a member of the Atlas family of rockets, and was used to launch five clusters of NOSS satellites for the US National Reconnaissance Office. Two flights also carried LiPS satellites, as secondary payloads for the United States Naval Research Laboratory. Atlas H could put a payload of 3,630 kg (8,000 lb) into low Earth orbit, or a payload of 2,255 kg (4,971 lb) into a geostationary transfer orbit. (en)
rdfs:label
  • Atlas H (en)
  • Atlas H (pt)
owl:sameAs
prov:wasDerivedFrom
foaf:depiction
foaf:isPrimaryTopicOf
foaf:name
  • Atlas H (en)
is dbo:maidenFlightRocket of
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