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Statements

Subject Item
dbr:Saturn_C-2
dbo:wikiPageWikiLink
dbr:S-III
Subject Item
dbr:S-III
rdf:type
dbo:Person yago:TimePeriod115113229 yago:WikicatRocketStages yago:Measure100033615 yago:Abstraction100002137 yago:Phase115290337 yago:FundamentalQuantity113575869
rdfs:label
S-III
rdfs:comment
The S-III (pronounced "S 3") was a proposed third stage of the early Saturn C designs for a five-stage Saturn launch vehicle. The Saturn C configurations were based on a "building block" approach, in which the upper stages would be test-flown before the intermediate stages. The S-III was to have been fueled with liquid oxygen and liquid hydrogen and powered by two J-2 engines. The original Saturn C-2 design would have been a three- or four-stage launch vehicle using the S-I plus S-III plus S-IV stages plus, for some missions, S-V.
dbp:name
S-III
dcterms:subject
dbc:Rocket_stages
dbo:wikiPageID
38732782
dbo:wikiPageRevisionID
1039266935
dbo:wikiPageWikiLink
dbr:J-2_(rocket_engine) dbr:S-IV dbr:LH2 dbr:S-I dbr:Saturn_(rocket_family) dbr:Liquid_hydrogen dbr:LOX dbr:Liquid_oxygen dbc:Rocket_stages dbr:NASA dbr:S-V dbr:Saturn_C-2 dbr:Saturn_C-3
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dbp:country
United States
dbo:abstract
The S-III (pronounced "S 3") was a proposed third stage of the early Saturn C designs for a five-stage Saturn launch vehicle. The Saturn C configurations were based on a "building block" approach, in which the upper stages would be test-flown before the intermediate stages. The S-III was to have been fueled with liquid oxygen and liquid hydrogen and powered by two J-2 engines. The original Saturn C-2 design would have been a three- or four-stage launch vehicle using the S-I plus S-III plus S-IV stages plus, for some missions, S-V.
dbp:rockets
dbr:Saturn_C-2 dbr:Saturn_C-3
gold:hypernym
dbr:Stage
prov:wasDerivedFrom
wikipedia-en:S-III?oldid=1039266935&ns=0
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1760
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wikipedia-en:S-III
Subject Item
dbr:Modular_rocket
dbo:wikiPageWikiLink
dbr:S-III
Subject Item
wikipedia-en:S-III
foaf:primaryTopic
dbr:S-III