Orbital Workshop at Astronautix
Image credit: NASA
Image source: Mike Acs
Tag: S-IVB
CSM/OW
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Apollo CSM
AAP Cluster
Parasol Thermal Shield
74-SL-7200-244A
Skylab
Six Man Mars Spacecraft
Apollo Flight Configuration
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.
Image credit: NASA
Image source: NASA MSFC
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