Matches in DBpedia 2016-04 for { <http://dbpedia.org/resource/Saturn_C-2> ?p ?o }
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- Saturn_C-2 diameter "6.52272".
- Saturn_C-2 height "68458.08".
- Saturn_C-2 mass "620071.2".
- Saturn_C-2 mass "620071.2".
- Saturn_C-2 abstract "The Saturn C-2 was the second rocket in the Saturn C series studied from 1959 to 1962. The design was for a four-stage launch vehicle that could launch 21,500 kg (47,300 lb) to low Earth orbit and send 6,800 kg (14,900 lb) to the Moon via Trans-Lunar Injection.The C-2 design concept was for a proposed manned circumlunar flight and the Earth orbit rendezvous (EOR) missions. It was initially considered for the Apollo lunar landing at the earliest possible date (1967).".
- Saturn_C-2 countryOrigin United_States.
- Saturn_C-2 diameter "6.52272".
- Saturn_C-2 height "68.45808".
- Saturn_C-2 launchSite Kennedy_Space_Center.
- Saturn_C-2 mass "6.200712E8".
- Saturn_C-2 rocketFunction Apollo_program.
- Saturn_C-2 rocketFunction Launch_vehicle.
- Saturn_C-2 status "Study, not developed".
- Saturn_C-2 wikiPageExternalLink saturnc2.htm.
- Saturn_C-2 wikiPageExternalLink free-return.htm.
- Saturn_C-2 wikiPageID "8431592".
- Saturn_C-2 wikiPageLength "9323".
- Saturn_C-2 wikiPageOutDegree "54".
- Saturn_C-2 wikiPageRevisionID "704657230".
- Saturn_C-2 wikiPageWikiLink Advanced_Cryogenic_Evolved_Stage.
- Saturn_C-2 wikiPageWikiLink Apollo_program.
- Saturn_C-2 wikiPageWikiLink Atlas_(rocket_family).
- Saturn_C-2 wikiPageWikiLink Atlas_V.
- Saturn_C-2 wikiPageWikiLink Category:Cancelled_space_launch_vehicles.
- Saturn_C-2 wikiPageWikiLink Category:Saturn_(rocket_family).
- Saturn_C-2 wikiPageWikiLink Centaur_(rocket_stage).
- Saturn_C-2 wikiPageWikiLink Circumlunar_trajectory.
- Saturn_C-2 wikiPageWikiLink Delta_Cryogenic_Second_Stage.
- Saturn_C-2 wikiPageWikiLink Delta_IV.
- Saturn_C-2 wikiPageWikiLink Douglas_Aircraft_Company.
- Saturn_C-2 wikiPageWikiLink Earth_orbit_rendezvous.
- Saturn_C-2 wikiPageWikiLink Kennedy_Space_Center.
- Saturn_C-2 wikiPageWikiLink Launch_vehicle.
- Saturn_C-2 wikiPageWikiLink Liquid_hydrogen.
- Saturn_C-2 wikiPageWikiLink Liquid_oxygen.
- Saturn_C-2 wikiPageWikiLink Low_Earth_orbit.
- Saturn_C-2 wikiPageWikiLink Moon.
- Saturn_C-2 wikiPageWikiLink Project_Horizon.
- Saturn_C-2 wikiPageWikiLink RL10.
- Saturn_C-2 wikiPageWikiLink RP-1.
- Saturn_C-2 wikiPageWikiLink Rocketdyne_H-1.
- Saturn_C-2 wikiPageWikiLink Rocketdyne_J-2.
- Saturn_C-2 wikiPageWikiLink S-II.
- Saturn_C-2 wikiPageWikiLink S-III.
- Saturn_C-2 wikiPageWikiLink S-IV.
- Saturn_C-2 wikiPageWikiLink Saturn_(rocket_family).
- Saturn_C-2 wikiPageWikiLink Saturn_C-3.
- Saturn_C-2 wikiPageWikiLink Saturn_I.
- Saturn_C-2 wikiPageWikiLink Saturn_II.
- Saturn_C-2 wikiPageWikiLink Saturn_V.
- Saturn_C-2 wikiPageWikiLink Space_Launch_System.
- Saturn_C-2 wikiPageWikiLink Titan_(rocket_family).
- Saturn_C-2 wikiPageWikiLink Trans-lunar_injection.
- Saturn_C-2 wikiPageWikiLink United_States.
- Saturn_C-2 wikiPageWikiLinkText "C-2".
- Saturn_C-2 wikiPageWikiLinkText "Saturn C-2".
- Saturn_C-2 countryOrigin United_States.
- Saturn_C-2 family Saturn_(rocket_family).
- Saturn_C-2 function "Launch vehicle for Project Horizon and Apollo".
- Saturn_C-2 mass "gross".
- Saturn_C-2 sites Kennedy_Space_Center.
- Saturn_C-2 status "Study, not developed".
- Saturn_C-2 wikiPageUsesTemplate Template:Convert.
- Saturn_C-2 wikiPageUsesTemplate Template:Dablink.
- Saturn_C-2 wikiPageUsesTemplate Template:Include-NASA.
- Saturn_C-2 wikiPageUsesTemplate Template:Infobox_rocket.
- Saturn_C-2 wikiPageUsesTemplate Payload.
- Saturn_C-2 wikiPageUsesTemplate Stage.
- Saturn_C-2 wikiPageUsesTemplate Template:Reflist.
- Saturn_C-2 subject Category:Cancelled_space_launch_vehicles.
- Saturn_C-2 subject Category:Saturn_(rocket_family).
- Saturn_C-2 hypernym Rocket.
- Saturn_C-2 type MeanOfTransportation.
- Saturn_C-2 type Rocket.
- Saturn_C-2 type Source.
- Saturn_C-2 type Vehicle.
- Saturn_C-2 type DesignedArtifact.
- Saturn_C-2 type Thing.
- Saturn_C-2 type Q41291.
- Saturn_C-2 comment "The Saturn C-2 was the second rocket in the Saturn C series studied from 1959 to 1962. The design was for a four-stage launch vehicle that could launch 21,500 kg (47,300 lb) to low Earth orbit and send 6,800 kg (14,900 lb) to the Moon via Trans-Lunar Injection.The C-2 design concept was for a proposed manned circumlunar flight and the Earth orbit rendezvous (EOR) missions. It was initially considered for the Apollo lunar landing at the earliest possible date (1967).".
- Saturn_C-2 label "Saturn C-2".
- Saturn_C-2 sameAs Q1996766.
- Saturn_C-2 sameAs Saturno_C-2.
- Saturn_C-2 sameAs Saturn_C-2.
- Saturn_C-2 sameAs m.0273611.
- Saturn_C-2 sameAs Saturn_C-2.
- Saturn_C-2 sameAs Q1996766.
- Saturn_C-2 wasDerivedFrom Saturn_C-2?oldid=704657230.
- Saturn_C-2 isPrimaryTopicOf Saturn_C-2.