Jump to content

S-IV

From Wikipedia, the free encyclopedia

This is an old revision of this page, as edited by Thijs!bot (talk | contribs) at 21:08, 26 March 2008 (robot Adding: fi:S-IV). The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.

The S-IV was the second stage of the Saturn I, a rocket-powered launch vehicle used by NASA for early flights in the Apollo program.

The S-IV is similar to, but distinct from, the S-IVB stage used on the Saturn IB and Saturn V rockets.

See also

S-IV stage of the Saturn I

References

NASA (April 1975). "Apollo Program Summary Report, Part 1" (PDF).