From Wikipedia, the free encyclopedia Saturn C-2
Saturn C-2
The Saturn C-2 was a conceptual American launch vehi- design was first studied in 1960, and it was calculated that
cle, which was proposed for the Earth orbit rendezvous 15 launches would be required to assemble a lunar space-
(EOR) approach to a lunar landing. craft in Low Earth orbit.
It consisted of an S-I first stage, later flown on the
Saturn I, an S-II second stage, later flown on the Saturn
V, an S-IV third stage, later flown on the Saturn I, and
External links
an S-V (Centaur) fourth stage, which, whilst never flying Encyclopedia Astronautica
on any Saturn rockets, would be used on Atlas and Titan
rockets, and is still in use on the Atlas V to this day. The
Retrieved from "http://en.wikipedia.org/w/index.php?title=Saturn_C-2&oldid=419344454"
Categories:
• Rocketry stubs
• Saturn rockets
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