Image credit: North American Rockwell
Image source: Mike Acs
Tag: command module
LEM by Gary Meyer
S63-11349
Robert Watts
Early Apollo
Image credit: NASA
Image source: Mike Acs
Apollo Spacecraft Re-Entry
Gary Meyer
S63-00048
LM Separation
Gjertson’s ASTP
S-69-60223
Space Station 1970 at Astronautix
Image credit: North American Rockwell
Image source(s):
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
numbers station 
