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Saturn Apollo Program

1960-01-01

NASA

NASA
Washington, DC, United States

RL-10 engine characteristics. The RL-10 engine was developed under the management of the Marshall Space Flight Center (MSFC) to power the Saturn I upper stage (S-IV stage). The six RL-10 engines, which used liquid hydrogen and liquid oxygen as propellants, were arranged in a circle on the aft end of the S-IV stage.

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  • Title: Saturn Apollo Program
  • Date Created: 1960-01-01
  • Rights: MSFC
  • Album: rlobrie1

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