• Rocket Engine, Liquid Fuel, Cutaway, Lark Missile
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    One half of a cylindrical steel rocket engine. Engine was cut along length to expose double wall construction, form of rocket nozzle area and fuel inlet/outlet areas. Welded construction. Two AN-8, 90 degree fittings welded to outer wall. One bracket with 5/16 inch hole welded on outer wall, opposite nozzle end.

Created by

Mary Hudgins

Date Created

06/08/2012

Source

Smithsonian National Air and Space Museum

Keywords

Engines; Military; Missiles; Rockets; Space

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