Matches in DBpedia 2016-04 for { <http://dbpedia.org/resource/Saturn_II> ?p ?o }
- Saturn_II diameter "10.0584".
- Saturn_II height "50901.6".
- Saturn_II abstract "The Saturn II was a series of American expendable launch vehicles, studied by North American Aviation under NASA contract in 1966, derived from the Saturn V rocket used for the Apollo lunar program. The intent of the study was to eliminate production of the Saturn IB, and create a lower-cost heavy launch vehicle based on Saturn V hardware. North American studied three versions with the S-IC first stage removed: the INT-17, a two-stage vehicle with a low Earth orbit payload capability of 47,000 pounds (21,000 kg); the INT-18, which added Titan UA1204 or UA1207 strap-on solid rocket boosters, with payloads ranging from 47,000 pounds (21,000 kg) to 146,400 pounds (66,400 kg); and the INT-19, using solid boosters derived from the Minuteman missile first stage.For this study, the Boeing company also investigated configurations designated INT-20 and INT-21 which employed its S-IC first stage, and eliminated either North American's S-II second stage, or the Douglas S-IVB third stage. Budget constraints led to cancellation of the study and exclusive use of the Space Shuttle for orbital payloads.".
- Saturn_II countryOrigin United_States.
- Saturn_II diameter "10.0584".
- Saturn_II height "50.9016".
- Saturn_II launchSite Kennedy_Space_Center.
- Saturn_II manufacturer Douglas_Aircraft_Company.
- Saturn_II manufacturer North_American_Aviation.
- Saturn_II rocketFunction Launch_vehicle.
- Saturn_II rocketStages "2".
- Saturn_II status "Study 1966".
- Saturn_II thumbnail Saturn_II.svg?width=300.
- Saturn_II totalLaunches "0".
- Saturn_II wikiPageExternalLink satvint.pdf.
- Saturn_II wikiPageExternalLink satint18.htm.
- Saturn_II wikiPageExternalLink satint17.htm.
- Saturn_II wikiPageExternalLink satint19.htm.
- Saturn_II wikiPageExternalLink saturnii.htm.
- Saturn_II wikiPageID "6597242".
- Saturn_II wikiPageLength "15216".
- Saturn_II wikiPageOutDegree "70".
- Saturn_II wikiPageRevisionID "707242186".
- Saturn_II wikiPageWikiLink Ammonium_perchlorate_composite_propellant.
- Saturn_II wikiPageWikiLink Apollo_Applications_Program.
- Saturn_II wikiPageWikiLink Apollo_program.
- Saturn_II wikiPageWikiLink Atlas_(rocket_family).
- Saturn_II wikiPageWikiLink Boeing.
- Saturn_II wikiPageWikiLink Category:Saturn_(rocket_family).
- Saturn_II wikiPageWikiLink Chrysler.
- Saturn_II wikiPageWikiLink Douglas_Aircraft_Company.
- Saturn_II wikiPageWikiLink Expansion_ratio.
- Saturn_II wikiPageWikiLink Expendable_launch_system.
- Saturn_II wikiPageWikiLink HG-3_(rocket_engine).
- Saturn_II wikiPageWikiLink Impulse_(physics).
- Saturn_II wikiPageWikiLink Kennedy_Space_Center.
- Saturn_II wikiPageWikiLink Kennedy_Space_Center_Launch_Complex_39.
- Saturn_II wikiPageWikiLink LGM-30_Minuteman.
- Saturn_II wikiPageWikiLink Launch_vehicle.
- Saturn_II wikiPageWikiLink Liquid_hydrogen.
- Saturn_II wikiPageWikiLink Liquid_oxygen.
- Saturn_II wikiPageWikiLink Low_Earth_orbit.
- Saturn_II wikiPageWikiLink Marshall_Space_Flight_Center.
- Saturn_II wikiPageWikiLink NASA.
- Saturn_II wikiPageWikiLink North_American_Aviation.
- Saturn_II wikiPageWikiLink Rocketdyne_J-2.
- Saturn_II wikiPageWikiLink S-IB.
- Saturn_II wikiPageWikiLink S-IC.
- Saturn_II wikiPageWikiLink S-II.
- Saturn_II wikiPageWikiLink S-IVB.
- Saturn_II wikiPageWikiLink Saturn_(rocket_family).
- Saturn_II wikiPageWikiLink Saturn_IB.
- Saturn_II wikiPageWikiLink Saturn_INT-20.
- Saturn_II wikiPageWikiLink Saturn_INT-21.
- Saturn_II wikiPageWikiLink Saturn_V.
- Saturn_II wikiPageWikiLink Solid_rocket_booster.
- Saturn_II wikiPageWikiLink Space_Shuttle.
- Saturn_II wikiPageWikiLink Titan_(rocket_family).
- Saturn_II wikiPageWikiLink UA120.
- Saturn_II wikiPageWikiLink United_States.
- Saturn_II wikiPageWikiLinkText "Saturn II".
- Saturn_II wikiPageWikiLinkText "Saturn INT-17".
- Saturn_II caption "Saturn II proposals: INT-17, INT-18, INT-19.".
- Saturn_II countryOrigin United_States.
- Saturn_II family Saturn_(rocket_family).
- Saturn_II function "Orbital launch vehicle".
- Saturn_II launches "0".
- Saturn_II manufacturer North_American_Aviation.
- Saturn_II manufacturer "Douglas".
- Saturn_II name "Saturn II".
- Saturn_II sites Kennedy_Space_Center.
- Saturn_II sites Kennedy_Space_Center_Launch_Complex_39.
- Saturn_II stages "2".
- Saturn_II status "Study 1966".
- Saturn_II wikiPageUsesTemplate Template:About.
- Saturn_II wikiPageUsesTemplate Template:Convert.
- Saturn_II wikiPageUsesTemplate Template:Infobox_rocket.
- Saturn_II wikiPageUsesTemplate Payload.
- Saturn_II wikiPageUsesTemplate Stage.
- Saturn_II wikiPageUsesTemplate stage.
- Saturn_II wikiPageUsesTemplate Template:Reflist.
- Saturn_II wikiPageUsesTemplate Template:Saturns.
- Saturn_II wikiPageUsesTemplate Template:Ubl.
- Saturn_II subject Category:Saturn_(rocket_family).
- Saturn_II hypernym Series.
- Saturn_II type MeanOfTransportation.
- Saturn_II type Rocket.
- Saturn_II type TelevisionShow.
- Saturn_II type Vehicle.
- Saturn_II type DesignedArtifact.
- Saturn_II type Thing.
- Saturn_II type Q41291.
- Saturn_II comment "The Saturn II was a series of American expendable launch vehicles, studied by North American Aviation under NASA contract in 1966, derived from the Saturn V rocket used for the Apollo lunar program. The intent of the study was to eliminate production of the Saturn IB, and create a lower-cost heavy launch vehicle based on Saturn V hardware.".
- Saturn_II label "Saturn II".
- Saturn_II sameAs Q7426795.
- Saturn_II sameAs m.0gd4gt.
- Saturn_II sameAs Q7426795.
- Saturn_II wasDerivedFrom Saturn_II?oldid=707242186.
- Saturn_II depiction Saturn_II.svg.
- Saturn_II isPrimaryTopicOf Saturn_II.