Rocket Engine, Liquid Fuel, Cutaway, LR2-RM-4, for Lark Missile
Two thrust chambers, both cut along their lengths to expose their double wall construction; form of rocket nozzle area and fuel inlet / outlet areas. Welded construction. On black, square, steel base with rounded corners.
Created by
Smithsonian National Air and Space Museum
Date Created
02/14/2022
Source
Smithsonian National Air and Space Museum
Keywords
Engines; Military; Missiles; Rockets; Space
Rights and Restrictions
Not determined
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