Matches in DBpedia 2014 for { <http://dbpedia.org/resource/S-IV> ?p ?o. }
Showing items 1 to 44 of
44
with 100 items per page.
- 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 wikiPageRevisionID "592967893".
- 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 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 subject Category:Apollo_program.
- S-IV subject Category:Rocket_stages.
- S-IV type Abstraction100002137.
- S-IV type FundamentalQuantity113575869.
- S-IV type Measure100033615.
- S-IV type Phase115290337.
- S-IV type RocketStages.
- S-IV type TimePeriod115113229.
- 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 (estágio de foguete)".
- S-IV label "S-IV".
- S-IV label "S-IV".
- S-IV label "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 sameAs S-IV.
- S-IV wasDerivedFrom S-IV?oldid=592967893.
- S-IV depiction S-IV_rocket_stage.jpg.
- S-IV isPrimaryTopicOf S-IV.