About: Saturn C-4

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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.

Attributes	Values
rdf:type	Thing mean of transportation Rocket rocket yago:WikicatCancelledSpaceLaunchVehicles yago:Artifact100021939 yago:Conveyance103100490 yago:Instrumentality103575240 yago:Object100002684 yago:PhysicalEntity100001930 yago:Rocket104099429 yago:Vehicle104524313 yago:Whole100003553
rdfs:label	Saturn C-4 (en)
rdfs: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. (en)
foaf:name	Saturn C-4 (en)
name	Saturn C-4 (en)
dcterms:subject	Apollo program Saturn (rocket family) Cancelled space launch vehicles
Wikipage page ID	9702322 (xsd:integer)
Wikipage revision ID	1040538956 (xsd:integer)
Link from a Wikipage to another Wikipage	Rocketdyne J-2 Saturn C-3 Saturn IB Saturn V Boeing List of space launch system designs LH2 LC-39 S-IB S-II S-IV S-IVB Moon NASA Apollo Lunar Module Lunar orbit rendezvous Apollo program Trans-lunar injection Launch vehicle Liquid oxygen North American Aviation Saturn (rocket family) Cancelled space launch vehicles Kennedy Space Center Douglas Aircraft Company Apollo Command/Service Module RP-1 Saturn (rocket family) LOX Low Earth orbit Rocketdyne Saturn rocket Lunar landing J-2 (rocket engine) SLC 37 F-1 (rocket engine) dbr:S-IB-4 dbr:S-II-4
Link from a Wikipage to an external page	https://web.archive.org/web/20111011054546/http:/astronautix.com/lvs/saturnc4.htm
sameAs	Saturn C-4 Saturn C-4 Saturn C-4 Saturn C-4
sites	planned SLC 37, LC-39; Kennedy Space Center (en)
dbp:wikiPageUsesTemplate	dbt:Expendable_launch_systems dbt:Convert dbt:Cvt dbt:ISBN dbt:Reflist dbt:Short_description dbt:Infobox_rocket/Stage dbt:Include-NASA dbt:Infobox_rocket dbt:Infobox_rocket/Payload dbt:Saturns
family	Saturn rocket
manufacturer	Douglas Aircraft Company Boeing (en) (en) North American (en)
status	Proposed (en)
stages	3 (xsd:integer)
has 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. (en)
comparable	Saturn V
country-origin	United States (en)
cpl	43500000 (xsd:integer)
cpl-year	1985 (xsd:integer)
function	LEO and Lunar launch vehicle (en)
launch site	LC-39 Kennedy Space Center SLC 37
rocket function	Moon Low Earth orbit
gold:hypernym	Rocket
comparable	Saturn V
prov:wasDerivedFrom	wikipedia-en:Saturn_C-4?oldid=1040538956&ns=0
page length (characters) of wiki page	4588 (xsd:nonNegativeInteger)
status	Proposed (1962)

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