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Subject Item

dbpedia:Saturn_C-4

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.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.

foaf:name

Saturn C-4

dbpedia-owl:comparable

dbpedia:Saturn_V

dbpedia-owl:countryOrigin

dbpedia:United_States

dbpedia-owl:diameter

8.128

dbpedia-owl:height

81.9912

dbpedia-owl:launchSite

dbpedia:Cape_Canaveral_Air_Force_Station_Space_Launch_Complex_37

dbpedia-owl:manufacturer

dbpedia:Douglas_Aircraft_Company dbpedia:North_American_Aviation dbpedia:Boeing

dbpedia-owl:mass

4.64337e+08

dbpedia-owl:rocketFunction

dbpedia:Moon dbpedia:Low_Earth_orbit

dbpedia-owl:rocketStages

3

dbpedia-owl:status

Proposed (1962)