Matches in DBpedia 2016-04 for { <http://wikidata.dbpedia.org/resource/Q7053759> ?p ?o }
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- Q7053759 subject Q13425903.
- Q7053759 subject Q7059182.
- Q7053759 subject Q8341344.
- Q7053759 subject Q8341356.
- Q7053759 subject Q8784597.
- Q7053759 abstract "The DC-3 was a proposed spaceplane designed by Maxime Faget at the Manned Spacecraft Center (MSC) in Houston. The design was nominally developed by North American Aviation (NAA), although it was a purely NASA-internal design.Unlike the eventual Space Shuttle design that emerged, the DC-3 was a fully reusable launch vehicle two-stage-to-orbit design with a smaller payload capacity of about 12,000 lbs and limited maneuverability. Its inherent strengths were good low-speed handling during landing, and a low-risk development that was relatively immune to changes in weight and balance.Work on the DC-3 program ended when the US Air Force joined the Shuttle program; they demanded a much greater "cross-range" maneuverability than the DC-3 could deliver, and expressed serious concerns about its stability during re-entry. NAA eventually won the Shuttle Orbiter contract, although it was based on a very different design from another team at MSC.".
- Q7053759 wikiPageExternalLink shuttle.htm.
- Q7053759 wikiPageExternalLink sld022.htm.
- Q7053759 wikiPageWikiLink Q1030042.
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- Q7053759 wikiPageWikiLink Q13425903.
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- Q7053759 wikiPageWikiLink Q8341344.
- Q7053759 wikiPageWikiLink Q8341356.
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- Q7053759 comment "The DC-3 was a proposed spaceplane designed by Maxime Faget at the Manned Spacecraft Center (MSC) in Houston. The design was nominally developed by North American Aviation (NAA), although it was a purely NASA-internal design.Unlike the eventual Space Shuttle design that emerged, the DC-3 was a fully reusable launch vehicle two-stage-to-orbit design with a smaller payload capacity of about 12,000 lbs and limited maneuverability.".
- Q7053759 label "North American DC-3".