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Inertial Weldment of Rhenium and Inconel 718Inertia welding has been found to be a successful method for joining pure rhenium to Inconel 718, and with additional experimentation, this process may have great potential for rocket nozzle applications. Refractory metals are ideally suited to this application, where high temperatures and oxidizing environment survivability is required, but not all of the thruster must be made of these materials, only the areas that require them. A bolted joint between the two metals is not ideal, especially for small thrusters where the mess of a bolted join will come at a steep price. A welded joint would be preferred for flight thrusters.
Document ID
20180002401
Acquisition Source
Marshall Space Flight Center
Document Type
Technical Publication (TP)
Authors
Cavender, D. P.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Courtright, Z. S.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Hostetter, G.
(Manufacturing Technology, Inc. South Bend, IN, United States)
Laiman, M.
(Manufacturing Technology, Inc. South Bend, IN, United States)
Date Acquired
April 11, 2018
Publication Date
March 1, 2018
Subject Category
Metals And Metallic Materials
Report/Patent Number
M-1454
NASA/TP-2018-219851
Report Number: M-1454
Report Number: NASA/TP-2018-219851
Distribution Limits
Public
Copyright
Public Use Permitted.
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