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Brazed boron-silicon carbide/aluminum structural panelsFluxless brazing process minimizes degradation of mechanical properties composite material of silicon carbide coated boron fibers in an aluminum matrix. Process is being used to fabricate full-scale Boron-Silicon Carbide/Aluminum-Titanium honeycomb core panels for flight testing and ground testing.
Document ID
19780000221
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Arnold, W. E., Jr.
(Vought Corp.)
Bales, T. T.
Brooks, T. G.
Lawson, A. G.
Mitchell, P. D.
Royster, D. M.
Wiant, R.
Date Acquired
August 9, 2013
Publication Date
October 1, 1978
Publication Information
Publication: NASA Tech Briefs
Volume: 3
Issue: 2
ISSN: 0145-319X
Subject Category
Materials
Report/Patent Number
LAR-12244
Accession Number
78B10221
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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