NASA NTRS · 19770011276
Brazed Borsic/aluminum structural panels
Abstract
A fluxless brazing process has been developed that minimizes degradation of the mechanical properties of Borsic/aluminum composites. The process, which employs 718 aluminum alloy braze, is being used to fabricate full scale Borsic/aluminum-titanium honeycomb-core panels for Mach 3 flight testing on the YF-12 aircraft and ground testing in support of the Supersonic Cruise Aircraft Research (SCAR) Program. The manufacturing development and results of shear tests on full scale panels are presented.
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Bales, T. T., Wiant, H. R., Royster, D. M.. 1977-03-01. Brazed Borsic/aluminum structural panels. https://ntrs.nasa.gov/citations/19770011276
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