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Subject Item

dbpedia:Saturn_C-2

rdfs: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).

dbpedia-owl:countryOrigin

dbpedia:United_States

dbpedia-owl:diameter

6.52272

dbpedia-owl:height

68.4581

dbpedia-owl:mass

6.20071e+08

dbpedia-owl:rocketFunction

dbpedia:Launch_vehicle dbpedia:Apollo_program

dbpedia-owl:status

Study, not developed