Matches in DBpedia 2016-04 for { <http://wikidata.dbpedia.org/resource/Q3950832> ?p ?o }
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- Q3950832 subject Q7215293.
- Q3950832 subject Q8341344.
- Q3950832 subject Q8705391.
- Q3950832 abstract "The Saturn C-3 was the third rocket in the Saturn C series studied from 1959 to 1962. The design was for a three-stage launch vehicle that could launch 45,000 kg (100,000 lb) to low Earth orbit and send 18,000 kg (39,000 lb) to the Moon via Trans-Lunar Injection.President Kennedy's proposal on May 25, 1961 of an explicit manned lunar landing goal spurred NASA to concretize its launch vehicle requirements for a lunar landing. A week earlier, William Fleming (Office of Space Flight Programs, NASA Headquarters) chaired an ad hoc committee to conduct a six-weeks study of the requirements for a lunar landing. Judging the direct ascent approach to be the most feasible, they concentrated their attention accordingly, and proposed circumlunar flights in late 1965 using the Saturn C-3 launch vehicle.In early June 1961, Bruce Lundin, deputy director of the Lewis Research Center, led a week-long study of six different rendezvous possibilities. The alternatives included earth-orbital rendezvous, lunar-orbital rendezvous, earth and lunar rendezvous, and rendezvous on the lunar surface, employing Saturn C-1s, C-3s, and Nova designs. Lundin's committee concluded that rendezvous enjoyed distinct advantages over direct ascent and recommended an earth-orbital rendezvous using two or three Saturn C-3s.NASA announced on September 7, 1961 that the government-owned Michoud Ordnance Plant near New Orleans, LA, would be the site for fabrication and assembly of the Saturn C-3 first stage as well as larger vehicles in the Saturn program. Finalists were two government-owned plants in St. Louis and New Orleans. The height of the factory roof at Michoud meant that a launch vehicle with eight F-1 engines (Nova class, Saturn C-8) could not be built; four or five engines would have to be the maximum.This decision ended consideration of a Nova class launch vehicle for Direct Ascent to the Moon or as heavy-lift companion with the Saturn C-3 for Earth Orbit Rendezvous.".
- Q3950832 comparable Q1093627.
- Q3950832 comparable Q249492.
- Q3950832 countryOrigin Q30.
- Q3950832 diameter "8.128".
- Q3950832 height "81.9912".
- Q3950832 launchSite Q2175575.
- Q3950832 manufacturer Q519560.
- Q3950832 manufacturer Q651778.
- Q3950832 manufacturer Q66.
- Q3950832 mass "4.64336712E8".
- Q3950832 rocketFunction Q405.
- Q3950832 rocketFunction Q663611.
- Q3950832 rocketStages "3".
- Q3950832 status "Proposed (1961)".
- Q3950832 successor Q2615678.
- Q3950832 successor Q3054149.
- Q3950832 thumbnail Proposed_Saturn_C-3_Apollo_Configuration.jpg?width=300.
- Q3950832 wikiPageExternalLink satvint.pdf.
- Q3950832 wikiPageExternalLink 19740072519_1974072519.pdf..
- Q3950832 wikiPageExternalLink 19790076768_1979076768.pdf..
- Q3950832 wikiPageWikiLink Q1029937.
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- Q3950832 wikiPageWikiLink Q1093627.
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- Q3950832 wikiPageWikiLink Q2175575.
- Q3950832 wikiPageWikiLink Q249492.
- Q3950832 wikiPageWikiLink Q2615678.
- Q3950832 wikiPageWikiLink Q30.
- Q3950832 wikiPageWikiLink Q3054149.
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- Q3950832 wikiPageWikiLink Q405.
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- Q3950832 wikiPageWikiLink Q48821.
- Q3950832 wikiPageWikiLink Q49543.
- Q3950832 wikiPageWikiLink Q519560.
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- Q3950832 wikiPageWikiLink Q5313879.
- Q3950832 wikiPageWikiLink Q5319205.
- Q3950832 wikiPageWikiLink Q54363.
- Q3950832 wikiPageWikiLink Q618153.
- Q3950832 wikiPageWikiLink Q622779.
- Q3950832 wikiPageWikiLink Q64127.
- Q3950832 wikiPageWikiLink Q651778.
- Q3950832 wikiPageWikiLink Q66.
- Q3950832 wikiPageWikiLink Q663611.
- Q3950832 wikiPageWikiLink Q697175.
- Q3950832 wikiPageWikiLink Q719315.
- Q3950832 wikiPageWikiLink Q7215293.
- Q3950832 wikiPageWikiLink Q7337143.
- Q3950832 wikiPageWikiLink Q73658.
- Q3950832 wikiPageWikiLink Q737107.
- Q3950832 wikiPageWikiLink Q7426780.
- Q3950832 wikiPageWikiLink Q7426784.
- Q3950832 wikiPageWikiLink Q745457.
- Q3950832 wikiPageWikiLink Q8341344.
- Q3950832 wikiPageWikiLink Q858145.
- Q3950832 wikiPageWikiLink Q863248.
- Q3950832 wikiPageWikiLink Q8705391.
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- Q3950832 wikiPageWikiLink Q967369.
- Q3950832 wikiPageWikiLink Q967676.
- Q3950832 wikiPageWikiLink Q967724.
- Q3950832 comparable Q1093627.
- Q3950832 comparable Q249492.
- Q3950832 countryOrigin Q30.
- Q3950832 derivatives Q2615678.
- Q3950832 derivatives Q3054149.
- Q3950832 function "LEO and Lunar launch vehicle".
- Q3950832 manufacturer Q519560.
- Q3950832 manufacturer Q66.
- Q3950832 manufacturer "Douglas".
- Q3950832 name "Saturn C-3".
- Q3950832 sites "planned SLC 37, Kennedy Space Center".
- Q3950832 stages "3".
- Q3950832 status "Proposed".
- Q3950832 type MeanOfTransportation.
- Q3950832 type Rocket.
- Q3950832 type DesignedArtifact.
- Q3950832 type Thing.
- Q3950832 type Q41291.
- Q3950832 comment "The Saturn C-3 was the third rocket in the Saturn C series studied from 1959 to 1962. The design was for a three-stage launch vehicle that could launch 45,000 kg (100,000 lb) to low Earth orbit and send 18,000 kg (39,000 lb) to the Moon via Trans-Lunar Injection.President Kennedy's proposal on May 25, 1961 of an explicit manned lunar landing goal spurred NASA to concretize its launch vehicle requirements for a lunar landing.".
- Q3950832 label "Saturn C-3".
- Q3950832 depiction Proposed_Saturn_C-3_Apollo_Configuration.jpg.
- Q3950832 name "Saturn C-3".