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n7http://commons.wikimedia.org/wiki/Special:FilePath/INT20C.
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Subject Item
dbpedia:Saturn_INT-20
rdfs:comment
The Saturn INT-20 was a proposed intermediate-payload follow-on from the Apollo Saturn V launch vehicle. A conical-form interstage would be fitted on top of the S-IC stage to support the S-IVB stage, so it could be considered either a retrofitted Saturn IB with a more powerful first stage, or a stubby, cut-down Saturn V without the S-II second stage.Three variants were studied, one with three F-1 engines in the first stage, one with four, and one with five.
foaf:name
Saturn INT-20
foaf:depiction
n7:svg
dbpedia-owl:countryOrigin
dbpedia:United_States
dbpedia-owl:diameter
10.0
dbpedia-owl:height
85.0
dbpedia-owl:launchSite
dbpedia:Kennedy_Space_Center_Launch_Complex_39
dbpedia-owl:lowerEarthOrbitPayload
6.05e+07
dbpedia-owl:manufacturer
dbpedia:Douglas_Aircraft_Company dbpedia:Boeing
dbpedia-owl:mass
2.304e+09
dbpedia-owl:rocketFunction
dbpedia:Low_Earth_orbit
dbpedia-owl:rocketStages
2
dbpedia-owl:status
Proposal
dbpedia-owl:thumbnail
n5:300