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
07/15/2009
Source
Smithsonian National Air and Space Museum
Keywords
Engines; Rockets; Space
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