Image credit: Grumman
Image source: National Archives
Tag: Lunar Excursion Module
Lunar Module Derivatives
Apollo (Early)
S70-31774
Robert Watts
S69-39011
S69-33765
S63-00048
Early LEM
Collecting Lunar Samples
From Drew Granston‘s collection: a beautiful early rendering of Grumman’s LM by Craig Kavafes.
Image credit: NASA
Image source: Drew Granston
LM Separation
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 
