DBpedia 2015-10

Matches in DBpedia 2015-10 for { <http://dbpedia.org/resource/S-IV> ?p ?o }

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S-IV abstract "The S-IV was the second stage of the Saturn I, a rocket-powered launch vehicle used by NASA for early flights in the Apollo program. The S-IV was manufactured by the Douglas Aircraft Company and later modified by them to the S-IVB, a similar but distinct stage used on the Saturn IB and Saturn V rockets.The S-IV stage was a large LOX/LH2-fueled rocket stage used for the early test flights of the Saturn I rocket. It formed the second stage of the Saturn I and was powered by a cluster of six RL-10A-3 engines. Each one of the engines supplied 66.7 kilonewtons (15,000 lbf) of thrust for a total of about 400 kilonewtons (90,000 lbf). The cryogenic LH2 (liquid hydrogen) and LOX (liquid oxygen) tanks were separated by a common bulkhead. The forward bulkhead of the LOX tank formed the aft bulkhead of the LH2 tank. This saved about ten tons of structural weight.".
S-IV thumbnail S-IV_rocket_stage.jpg?width=300.
S-IV wikiPageExternalLink APSR-JSC-09423.pdf.
S-IV wikiPageID "654880".
S-IV wikiPageLength "2265".
S-IV wikiPageOutDegree "21".
S-IV wikiPageRevisionID "667821213".
S-IV wikiPageWikiLink Apollo_program.
S-IV wikiPageWikiLink Category:Apollo_program.
S-IV wikiPageWikiLink Category:Rocket_stages.
S-IV wikiPageWikiLink Douglas_Aircraft_Company.
S-IV wikiPageWikiLink LH2.
S-IV wikiPageWikiLink LOX.
S-IV wikiPageWikiLink Launch_vehicle.
S-IV wikiPageWikiLink Liquid_hydrogen.
S-IV wikiPageWikiLink Liquid_oxygen.
S-IV wikiPageWikiLink Multistage_rocket.
S-IV wikiPageWikiLink NASA.
S-IV wikiPageWikiLink Project_Apollo.
S-IV wikiPageWikiLink RL-10_(rocket_engine).
S-IV wikiPageWikiLink RL10.
S-IV wikiPageWikiLink Rocket.
S-IV wikiPageWikiLink S-IVB.
S-IV wikiPageWikiLink Saturn_I.
S-IV wikiPageWikiLink Saturn_IB.
S-IV wikiPageWikiLink Saturn_V.
S-IV wikiPageWikiLinkText "S-IV".
S-IV wikiPageWikiLinkText "Saturn S-IV stage".
S-IV altDiameter "18.0".
S-IV altHeight "40.0".
S-IV altThrust "90000".
S-IV caption "Schematics of the S-IV".
S-IV country "United States".
S-IV diameter "5.49 m".
S-IV engines "6".
S-IV fuel LH2.
S-IV fuel LOX.
S-IV fuel Liquid_hydrogen.
S-IV fuel Liquid_oxygen.
S-IV hasPhotoCollection S-IV.
S-IV height "12.19 m".
S-IV manufacturer Douglas_Aircraft_Company.
S-IV name "S-IV".
S-IV rockets Saturn_I.
S-IV thrust "400 kN".
S-IV time "410.0".
S-IV wikiPageUsesTemplate Template:Cite_book.
S-IV wikiPageUsesTemplate Template:Cite_web.
S-IV wikiPageUsesTemplate Template:Convert.
S-IV wikiPageUsesTemplate Template:Infobox_rocket_stage.
S-IV wikiPageUsesTemplate Template:Refbegin.
S-IV wikiPageUsesTemplate Template:Refend.
S-IV wikiPageUsesTemplate Template:Reflist.
S-IV subject Category:Apollo_program.
S-IV subject Category:Rocket_stages.
S-IV hypernym Stage.
S-IV type Person.
S-IV type Mission.
S-IV type Program.
S-IV type Programme.
S-IV type Stage.
S-IV comment "The S-IV was the second stage of the Saturn I, a rocket-powered launch vehicle used by NASA for early flights in the Apollo program. The S-IV was manufactured by the Douglas Aircraft Company and later modified by them to the S-IVB, a similar but distinct stage used on the Saturn IB and Saturn V rockets.The S-IV stage was a large LOX/LH2-fueled rocket stage used for the early test flights of the Saturn I rocket.".
S-IV label "S-IV".
S-IV sameAs S-IV.
S-IV sameAs S-IV.
S-IV sameAs S-IV.
S-IV sameAs S-IV.
S-IV sameAs S-IV_(estágio_de_foguete).
S-IV sameAs m.02p2rz4.
S-IV sameAs Q1030212.
S-IV sameAs Q1030212.
S-IV wasDerivedFrom S-IV?oldid=667821213.
S-IV depiction S-IV_rocket_stage.jpg.
S-IV isPrimaryTopicOf S-IV.