Matches in DBpedia 2016-04 for { <http://dbpedia.org/resource/Saturn_C-4> ?p ?o }
- Saturn_C-4 diameter "8.128".
- Saturn_C-4 height "81991.2".
- Saturn_C-4 mass "464336.712".
- Saturn_C-4 mass "464336.712".
- Saturn_C-4 abstract "The Saturn C-4 was the fourth rocket in the Saturn C series studied from 1959 to 1962. The C-4 design was proposed in 1960 for a three-stage launch vehicle that could launch 99,000 kg (218,000 lb) to Low Earth orbit and send 32,000 kg (70,000 lb) to the Moon via Trans-lunar injection. It met the initial requirements for a lunar orbit rendezvous and lunar landing mission.It would have consisted of three stages; an S-IB-4 first stage, a S-II-4 second stage and a S-IVB third stage. The first and second stages were essentially four-engine variants of the stages that would be used on the Saturn V, while the IVB stage was actually used on both the Saturn V and the Saturn IB.It would have been capable of sending the 30,000 kg (67,000 lb) Apollo Command/Service Module into lunar orbit, but it would not have been able to carry the 15,000 kg (32,000 lb) Apollo Lunar Module as well. Although NASA eventually used the lunar orbit rendezvous method to go to the Moon, it decided to use the larger Saturn V which would provide a reserve payload capacity.".
- Saturn_C-4 comparable Saturn_V.
- Saturn_C-4 countryOrigin United_States.
- Saturn_C-4 diameter "8.128".
- Saturn_C-4 height "81.9912".
- Saturn_C-4 launchSite Cape_Canaveral_Air_Force_Station_Space_Launch_Complex_37.
- Saturn_C-4 launchSite Kennedy_Space_Center.
- Saturn_C-4 manufacturer Boeing.
- Saturn_C-4 manufacturer Douglas_Aircraft_Company.
- Saturn_C-4 manufacturer North_American_Aviation.
- Saturn_C-4 mass "4.64336712E8".
- Saturn_C-4 rocketFunction Low_Earth_orbit.
- Saturn_C-4 rocketFunction Moon.
- Saturn_C-4 rocketStages "3".
- Saturn_C-4 status "Proposed (1962)".
- Saturn_C-4 wikiPageExternalLink saturnc4.htm.
- Saturn_C-4 wikiPageID "9702322".
- Saturn_C-4 wikiPageLength "4872".
- Saturn_C-4 wikiPageOutDegree "47".
- Saturn_C-4 wikiPageRevisionID "661393084".
- Saturn_C-4 wikiPageWikiLink Service_Module.
- Saturn_C-4 wikiPageWikiLink Apollo_Lunar_Module.
- Saturn_C-4 wikiPageWikiLink Boeing.
- Saturn_C-4 wikiPageWikiLink Cape_Canaveral_Air_Force_Station_Space_Launch_Complex_37.
- Saturn_C-4 wikiPageWikiLink Category:Apollo_program.
- Saturn_C-4 wikiPageWikiLink Category:Cancelled_space_launch_vehicles.
- Saturn_C-4 wikiPageWikiLink Category:Saturn_(rocket_family).
- Saturn_C-4 wikiPageWikiLink Douglas_Aircraft_Company.
- Saturn_C-4 wikiPageWikiLink Kennedy_Space_Center.
- Saturn_C-4 wikiPageWikiLink Launch_vehicle.
- Saturn_C-4 wikiPageWikiLink Liquid_hydrogen.
- Saturn_C-4 wikiPageWikiLink Liquid_oxygen.
- Saturn_C-4 wikiPageWikiLink List_of_space_launch_system_designs.
- Saturn_C-4 wikiPageWikiLink Low_Earth_orbit.
- Saturn_C-4 wikiPageWikiLink Lunar_orbit_rendezvous.
- Saturn_C-4 wikiPageWikiLink Moon.
- Saturn_C-4 wikiPageWikiLink Moon_landing.
- Saturn_C-4 wikiPageWikiLink NASA.
- Saturn_C-4 wikiPageWikiLink North_American_Aviation.
- Saturn_C-4 wikiPageWikiLink RP-1.
- Saturn_C-4 wikiPageWikiLink Rocketdyne.
- Saturn_C-4 wikiPageWikiLink Rocketdyne_F-1.
- Saturn_C-4 wikiPageWikiLink Rocketdyne_J-2.
- Saturn_C-4 wikiPageWikiLink S-IB.
- Saturn_C-4 wikiPageWikiLink S-IB-4.
- Saturn_C-4 wikiPageWikiLink S-II.
- Saturn_C-4 wikiPageWikiLink S-II-4.
- Saturn_C-4 wikiPageWikiLink S-IV.
- Saturn_C-4 wikiPageWikiLink S-IVB.
- Saturn_C-4 wikiPageWikiLink Saturn_(rocket_family).
- Saturn_C-4 wikiPageWikiLink Saturn_C-3.
- Saturn_C-4 wikiPageWikiLink Saturn_IB.
- Saturn_C-4 wikiPageWikiLink Saturn_V.
- Saturn_C-4 wikiPageWikiLink Space_Launch_System.
- Saturn_C-4 wikiPageWikiLink Trans-lunar_injection.
- Saturn_C-4 wikiPageWikiLink United_States.
- Saturn_C-4 wikiPageWikiLinkText "C-4".
- Saturn_C-4 wikiPageWikiLinkText "Saturn C-4".
- Saturn_C-4 comparable Saturn_V.
- Saturn_C-4 countryOrigin United_States.
- Saturn_C-4 cpl "43500000".
- Saturn_C-4 cplYear "1985".
- Saturn_C-4 family Saturn_(rocket_family).
- Saturn_C-4 function "LEO and Lunar launch vehicle".
- Saturn_C-4 manufacturer Boeing.
- Saturn_C-4 manufacturer North_American_Aviation.
- Saturn_C-4 manufacturer "Douglas".
- Saturn_C-4 name "Saturn C-4".
- Saturn_C-4 sites "planned SLC 37, Kennedy Space Center".
- Saturn_C-4 stages "3".
- Saturn_C-4 status "Proposed".
- Saturn_C-4 wikiPageUsesTemplate Template:Convert.
- Saturn_C-4 wikiPageUsesTemplate Template:Expendable_launch_systems.
- Saturn_C-4 wikiPageUsesTemplate Template:Include-NASA.
- Saturn_C-4 wikiPageUsesTemplate Template:Infobox_rocket.
- Saturn_C-4 wikiPageUsesTemplate Payload.
- Saturn_C-4 wikiPageUsesTemplate Stage.
- Saturn_C-4 wikiPageUsesTemplate Template:Reflist.
- Saturn_C-4 wikiPageUsesTemplate Template:Saturns.
- Saturn_C-4 subject Category:Apollo_program.
- Saturn_C-4 subject Category:Cancelled_space_launch_vehicles.
- Saturn_C-4 subject Category:Saturn_(rocket_family).
- Saturn_C-4 hypernym Rocket.
- Saturn_C-4 type MeanOfTransportation.
- Saturn_C-4 type Rocket.
- Saturn_C-4 type Mission.
- Saturn_C-4 type Program.
- Saturn_C-4 type Programme.
- Saturn_C-4 type Source.
- Saturn_C-4 type Vehicle.
- Saturn_C-4 type DesignedArtifact.
- Saturn_C-4 type Thing.
- Saturn_C-4 type Q41291.
- Saturn_C-4 comment "The Saturn C-4 was the fourth rocket in the Saturn C series studied from 1959 to 1962. The C-4 design was proposed in 1960 for a three-stage launch vehicle that could launch 99,000 kg (218,000 lb) to Low Earth orbit and send 32,000 kg (70,000 lb) to the Moon via Trans-lunar injection. It met the initial requirements for a lunar orbit rendezvous and lunar landing mission.It would have consisted of three stages; an S-IB-4 first stage, a S-II-4 second stage and a S-IVB third stage.".
- Saturn_C-4 label "Saturn C-4".
- Saturn_C-4 sameAs Q7426780.