NASA NTRS · 19730013693
Brazing of beryllium for structural applications
Abstract
Progress made in fabricating a beryllium compression tube structure and a stiffened beryllium panel. The compression tube was 7.6cm in diameter and 30.5cm long with titanium end fittings. The panel was 203cm long and stiffened with longitudinal stringers. Both units were assembled by brazing with BAg-18 braze alloy. The detail parts were fabricated by hot forming 0.305cm beryllium sheet and the brazing parameters established.
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Vogan, J. W.. 1972-01-01. Brazing of beryllium for structural applications. https://ntrs.nasa.gov/citations/19730013693
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