Bell-shaped nozzle with attached slightly tapering combustion chamber on top, with adjoining pumps and associated plumbing fixed on one side and top of combustion chamber. Nozzle with longitudinally placed nickel alloy cooling tubes with 10 equi-distant support bands around nozzle, plus one rim band. Created by Smithsonian National Air and Space Museum Date Created 11/19/2021 Source Smithsonian National Air and Space Museum Keywords Engines; Rockets; Space Rights and Restrictions Not determined
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