Saturn II

The Saturn II was a proposed American Expendable launch vehicle, derived from the Saturn V rocket that was used for the Apollo lunar program. The basic concept of the Saturn II was to save money by ceasing production of the Saturn IB rocket, and replacing it with a more capable rocket, that was built using Saturn V components. This would allow them to close down production lines for the S-IB stage, and would allow for more efficient integration o... more

Rocket

Rocket Function:

Country Of Origin:

Height:

  • 51 m (170 ft )

Diameter:

  • 10.6 m (34.8 ft )

Mass:

  • 328,300 kg (723778 lb )

Number Of Stages:

  • 2
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