Rocket Engine, Liquid Fuel, Auxiliary Propulsion,System (APS) Thruster, Saturn V
Cylindrical combustion chamber with rounded top, to which is attached a shorter, straight cylinder with electronic components and wire bundle prortruding from top. Appears to be incomplete.
Created by
2015 NASM Mass Digitization Production Project (Ortery system)
Date Created
12/09/2015
Source
National Air and Space Museum, Smithsonian Institution.
Keywords
Engines; Launch Vehicles; Rockets; Space
Rights and Restrictions
Not determined
For more information, visit the Smithsonians Terms of Use.