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 02/07/2022 Source Smithsonian National Air and Space Museum Keywords Engines; Rockets; Space Rights and Restrictions Not determined
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