Image credit: NASA
Image source: NASA MSFC
Tag: S-IVB
AAP Cluster
Image credit: NASA Marshall
Image source: NASA Images
Parasol Thermal Shield
Image credit: NASA
Image source: NASA Marshall
74-SL-7200-244A
Image credit: NASA Marshall
Image source: NASA Images
Skylab
Mission Module Spacecraft
Image credit: Douglas
Image source: Numbers Station
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 MSFC
Image source: NASA Images
Saturn V Apollo
Image credit: NASA MSFC
Image source: NASA Images
Orbital Workshop
Image credit: McDonnell Douglas
Image source: SDASM Archives
Artist Concepts
Image credit: NASA JSC
Image source: NASA Images
