File:Saturn Apollo Program (9253429).jpg
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Summary
[edit]DescriptionSaturn Apollo Program (9253429).jpg |
English: The Saturn V configuration is shown in inches and meters as illustrated by the Boeing Company. The Saturn V vehicle consisted of three stages: the S-IC (first) stage powered by five F-1 engines, the S-II (second) stage powered by five J-2 engines, the S-IVB (third) stage powered by one J-2 engine. A top for the first three stages was designed to contain the instrument unit, the guidance system, the Apollo spacecraft, and the escape system. The Apollo spacecraft consisted of the lunar module, the service module, and the command module. The Saturn V was designed perform lunar and planetary missions and it was capable of placing 280,000 pounds into Earth orbit. |
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Date | Taken on 1 March 1967 | ||
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Author | NASA Marshall Space Flight Center | ||
Keywords InfoField | Configuration; Saturn V; Boeing Company |
Licensing
[edit]Public domainPublic domainfalsefalse |
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This file is in the public domain in the United States because it was solely created by NASA. NASA copyright policy states that "NASA material is not protected by copyright unless noted". (See Template:PD-USGov, NASA copyright policy page or JPL Image Use Policy.) | ![]() |
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Image title | Saturn V apollo flight configuration (In english and metric measurements) |
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IIM version | 2 |
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