NASA NTRS · 19780000221
Brazed boron-silicon carbide/aluminum structural panels
Abstract
Fluxless 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.
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Arnold, W. E., Jr., Bales, T. T., Brooks, T. G., Lawson, A. G., Mitchell, P. D., Royster, D. M., Wiant, R.. 1978-10-01. Brazed boron-silicon carbide/aluminum structural panels. https://ntrs.nasa.gov/citations/19780000221
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