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Saturn Apollo Program

1960-01-01

NASA

NASA
Washington, DC, United States

H-1 engine characteristics: The H-1 engine was developed under the management of the Marshall Space Flight Center (MSFC). The cluster of eight H-1 engines was used to power the first stage of the Saturn I (S-I stage) and Saturn IB (S-IVB stage) launch vehicles, and produced 188,00 pounds of thrust, a combined thrust of 1,500,000 pounds, later uprated to 205,000 pounds of thrust and a combined total thrust of 1,650,000 pounds for the Saturn IB program.

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

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