Matches in DBpedia 2015-10 for { <http://dbpedia.org/resource/Saturn_INT-20> ?p ?o }
- Saturn_INT-20 diameter "10.0".
- Saturn_INT-20 height "85000.0".
- Saturn_INT-20 mass "2304000.0".
- Saturn_INT-20 lowerEarthOrbitPayload "60500.0".
- Saturn_INT-20 mass "2304000.0".
- Saturn_INT-20 abstract "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.".
- Saturn_INT-20 countryOrigin United_States.
- Saturn_INT-20 diameter "10.0".
- Saturn_INT-20 height "85.0".
- Saturn_INT-20 launchSite Kennedy_Space_Center.
- Saturn_INT-20 launchSite Kennedy_Space_Center_Launch_Complex_39.
- Saturn_INT-20 lowerEarthOrbitPayload "6.05E7".
- Saturn_INT-20 manufacturer Boeing.
- Saturn_INT-20 manufacturer Douglas_Aircraft_Company.
- Saturn_INT-20 mass "2.304E9".
- Saturn_INT-20 rocketFunction Low_Earth_orbit.
- Saturn_INT-20 rocketStages "2".
- Saturn_INT-20 status "Proposal".
- Saturn_INT-20 thumbnail INT20C.svg?width=300.
- Saturn_INT-20 wikiPageExternalLink satvint.pdf.
- Saturn_INT-20 wikiPageExternalLink satint20.htm.
- Saturn_INT-20 wikiPageID "5882940".
- Saturn_INT-20 wikiPageLength "3858".
- Saturn_INT-20 wikiPageOutDegree "37".
- Saturn_INT-20 wikiPageRevisionID "649180563".
- Saturn_INT-20 wikiPageWikiLink Apollo_program.
- Saturn_INT-20 wikiPageWikiLink Boeing.
- Saturn_INT-20 wikiPageWikiLink Category:Apollo_program.
- Saturn_INT-20 wikiPageWikiLink Category:Cancelled_space_launch_vehicles.
- Saturn_INT-20 wikiPageWikiLink Category:Saturn_(rocket_family).
- Saturn_INT-20 wikiPageWikiLink Douglas_Aircraft_Company.
- Saturn_INT-20 wikiPageWikiLink F-1_(rocket_engine).
- Saturn_INT-20 wikiPageWikiLink Foot_(unit).
- Saturn_INT-20 wikiPageWikiLink Foot_(unit_of_length).
- Saturn_INT-20 wikiPageWikiLink J-2_(rocket_engine).
- Saturn_INT-20 wikiPageWikiLink Kennedy_Space_Center.
- Saturn_INT-20 wikiPageWikiLink Kennedy_Space_Center_Launch_Complex_39.
- Saturn_INT-20 wikiPageWikiLink Kilogram.
- Saturn_INT-20 wikiPageWikiLink LH2.
- Saturn_INT-20 wikiPageWikiLink LOX.
- Saturn_INT-20 wikiPageWikiLink Launch_vehicle.
- Saturn_INT-20 wikiPageWikiLink Liquid_hydrogen.
- Saturn_INT-20 wikiPageWikiLink Liquid_oxygen.
- Saturn_INT-20 wikiPageWikiLink Low_Earth_orbit.
- Saturn_INT-20 wikiPageWikiLink Nautical_mile.
- Saturn_INT-20 wikiPageWikiLink Newton_(unit).
- Saturn_INT-20 wikiPageWikiLink Pound-force.
- Saturn_INT-20 wikiPageWikiLink Pound_(force).
- Saturn_INT-20 wikiPageWikiLink Pound_(mass).
- Saturn_INT-20 wikiPageWikiLink Project_Apollo.
- Saturn_INT-20 wikiPageWikiLink RP-1.
- Saturn_INT-20 wikiPageWikiLink Rocketdyne.
- Saturn_INT-20 wikiPageWikiLink Rocketdyne_F-1.
- Saturn_INT-20 wikiPageWikiLink Rocketdyne_J-2.
- Saturn_INT-20 wikiPageWikiLink S-IC.
- Saturn_INT-20 wikiPageWikiLink S-II.
- Saturn_INT-20 wikiPageWikiLink S-IVB.
- Saturn_INT-20 wikiPageWikiLink Saturn_C-3.
- Saturn_INT-20 wikiPageWikiLink Saturn_IB.
- Saturn_INT-20 wikiPageWikiLink Saturn_V.
- Saturn_INT-20 wikiPageWikiLink Space_Launch_System.
- Saturn_INT-20 wikiPageWikiLink United_States.
- Saturn_INT-20 wikiPageWikiLinkText "Saturn INT-20".
- Saturn_INT-20 altDiameter "33.0".
- Saturn_INT-20 altHeight "281.0".
- Saturn_INT-20 altMass "5070000.0".
- Saturn_INT-20 altStage1thrust "max 7,648,000 lbf".
- Saturn_INT-20 altStage2thrust "225000".
- Saturn_INT-20 caption "INT-20 configuration".
- Saturn_INT-20 countryOrigin United_States.
- Saturn_INT-20 diameter "10 m".
- Saturn_INT-20 function "Manned LEO launch vehicle".
- Saturn_INT-20 hasPhotoCollection Saturn_INT-20.
- Saturn_INT-20 height "85 m".
- Saturn_INT-20 leoPayload "max 60,500 kg".
- Saturn_INT-20 manufacturer Boeing.
- Saturn_INT-20 manufacturer "Douglas".
- Saturn_INT-20 mass "2304000.0".
- Saturn_INT-20 name "Saturn INT-20".
- Saturn_INT-20 sites Kennedy_Space_Center.
- Saturn_INT-20 sites Kennedy_Space_Center_Launch_Complex_39.
- Saturn_INT-20 stage1engines "3".
- Saturn_INT-20 stage1fuel LOX.
- Saturn_INT-20 stage1fuel Liquid_oxygen.
- Saturn_INT-20 stage1fuel RP-1.
- Saturn_INT-20 stage1name S-IC.
- Saturn_INT-20 stage1thrust "max 34.02 MN".
- Saturn_INT-20 stage1time "212.0".
- Saturn_INT-20 stage2engines "1".
- Saturn_INT-20 stage2fuel LH2.
- Saturn_INT-20 stage2fuel LOX.
- Saturn_INT-20 stage2fuel Liquid_hydrogen.
- Saturn_INT-20 stage2fuel Liquid_oxygen.
- Saturn_INT-20 stage2name S-IVB.
- Saturn_INT-20 stage2thrust "1.0".
- Saturn_INT-20 stage2time "475.0".
- Saturn_INT-20 stages "2".
- Saturn_INT-20 status "Proposal".
- Saturn_INT-20 wikiPageUsesTemplate Template:Infobox_rocket.
- Saturn_INT-20 wikiPageUsesTemplate Template:Saturns.