Matches in DBpedia 2016-04 for { <http://wikidata.dbpedia.org/resource/Q7426795> ?p ?o }
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- Q7426795 subject Q8705391.
- Q7426795 abstract "The Saturn II was a series of American expendable launch vehicles, studied by North American Aviation under NASA contract in 1966, derived from the Saturn V rocket used for the Apollo lunar program. The intent of the study was to eliminate production of the Saturn IB, and create a lower-cost heavy launch vehicle based on Saturn V hardware. North American studied three versions with the S-IC first stage removed: the INT-17, a two-stage vehicle with a low Earth orbit payload capability of 47,000 pounds (21,000 kg); the INT-18, which added Titan UA1204 or UA1207 strap-on solid rocket boosters, with payloads ranging from 47,000 pounds (21,000 kg) to 146,400 pounds (66,400 kg); and the INT-19, using solid boosters derived from the Minuteman missile first stage.For this study, the Boeing company also investigated configurations designated INT-20 and INT-21 which employed its S-IC first stage, and eliminated either North American's S-II second stage, or the Douglas S-IVB third stage. Budget constraints led to cancellation of the study and exclusive use of the Space Shuttle for orbital payloads.".
- Q7426795 countryOrigin Q30.
- Q7426795 diameter "10.0584".
- Q7426795 height "50.9016".
- Q7426795 manufacturer Q519560.
- Q7426795 manufacturer Q651778.
- Q7426795 rocketFunction Q697175.
- Q7426795 rocketStages "2".
- Q7426795 status "Study 1966".
- Q7426795 thumbnail Saturn_II.svg?width=300.
- Q7426795 totalLaunches "0".
- Q7426795 wikiPageExternalLink satvint.pdf.
- Q7426795 wikiPageExternalLink satint18.htm.
- Q7426795 wikiPageExternalLink satint17.htm.
- Q7426795 wikiPageExternalLink satint19.htm.
- Q7426795 wikiPageExternalLink saturnii.htm.
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- Q7426795 wikiPageWikiLink Q30.
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- Q7426795 wikiPageWikiLink Q519560.
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- Q7426795 wikiPageWikiLink Q618933.
- Q7426795 wikiPageWikiLink Q622779.
- Q7426795 wikiPageWikiLink Q651778.
- Q7426795 wikiPageWikiLink Q66.
- Q7426795 wikiPageWikiLink Q663611.
- Q7426795 wikiPageWikiLink Q697175.
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- Q7426795 wikiPageWikiLink Q837940.
- Q7426795 wikiPageWikiLink Q845774.
- Q7426795 wikiPageWikiLink Q861662.
- Q7426795 wikiPageWikiLink Q8705391.
- Q7426795 wikiPageWikiLink Q967676.
- Q7426795 countryOrigin Q30.
- Q7426795 function "Orbital launch vehicle".
- Q7426795 launches "0".
- Q7426795 manufacturer Q519560.
- Q7426795 manufacturer "Douglas".
- Q7426795 name "Saturn II".
- Q7426795 sites Q48821.
- Q7426795 sites Q845774.
- Q7426795 stages "2".
- Q7426795 status "Study 1966".
- Q7426795 type MeanOfTransportation.
- Q7426795 type Rocket.
- Q7426795 type DesignedArtifact.
- Q7426795 type Thing.
- Q7426795 type Q41291.
- Q7426795 comment "The Saturn II was a series of American expendable launch vehicles, studied by North American Aviation under NASA contract in 1966, derived from the Saturn V rocket used for the Apollo lunar program. The intent of the study was to eliminate production of the Saturn IB, and create a lower-cost heavy launch vehicle based on Saturn V hardware.".
- Q7426795 label "Saturn II".
- Q7426795 depiction Saturn_II.svg.
- Q7426795 name "Saturn II".