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NASA NTRS · 19840003146

Metal matrix composite structural panel construction

Abstract

Lightweight capped honeycomb stiffeners for use in fabricating metal or metal/matrix exterior structural panels on aerospace type vehicles and the process for fabricating same are disclosed. The stiffener stringers are formed in sheets, cut to the desired width and length and brazed in spaced relationship to a skin with the honeycomb material serving directly as the required lightweight stiffeners and not requiring separate metal encasement for the exposed honeycomb cells.

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BibTeXRIS

Mcwithey, R. R., Royster, D. M., Bales, T. T.. 1983-10-25. Metal matrix composite structural panel construction. https://ntrs.nasa.gov/citations/19840003146

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