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Saturn Apollo Program

This illustration, with callouts, is of the Saturn V SII (2nd Stage) developed by the Space Division of North American Aviation under the direction of the Marshall Space Flight Center. The 82-foot-long and 33-foot-diameter S-II stage utilized five J-2 engines, each with a 200,000-pound thrust capability. The engine used liquid oxygen and liquid hydrogen as its propellants.

Date
1964-02-07
Collection
MSFC
Archive
NASA Image and Video Library
Type
illustration (NASA artwork)

Public domainsafest

Reason: a NASA work: not copyrighted in the United States.

Read from: NASA media usage guidelines: NASA material is not copyrighted in the US unless noted; no third-party credit or mark found.

Credit line

"Saturn Apollo Program" (1964-02-07). NASA/MSFC. Public domain. https://images.nasa.gov/details/0600310

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