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A study of strength evaluations of EDNi/EDCu/NARloy-Z bonded jointsDissimilar material interfaces can be found in many materials and structural bonds such as composite materials, welded parts, inclusion in matrix, bond between metallic and ceramic materials, and so forth. One of such structural bonds can be seen in the main combustion chamber (MCC) of the Space Shuttle Main Engine (SSME). In this study, from a practical sense, the primary concern is to understand the systems response of EDNi/EDCu/NARloy-Z bonded joints using stress values approximated by the finite element method to determine an influence of the variation of structural bond parameters on the bonded joints, and consequently main combustion chamber of the Space Shuttle Main Engine. The results presented in this study could be an appropriate indicator for a good bond of EDNi/DECu/NARloy-Z layers with the desired thickness of copper deposition in the SSME MCC manufacturing process. Furthermore, the results from this study appear to be applicable to any bonded joints that can be characterized by the parameters and assumptions used in this analysis.
Document ID
19940006803
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Min, J. B.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Spanyer, K. L.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1993
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.15:108418
NASA-TM-108418
Accession Number
94N11275
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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