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NASA NTRS ยท 19950065227

Flame-Resistant Composite Materials For Structural Members

Abstract

Matrix-fiber composite materials developed for structural members occasionally exposed to hot, corrosive gases. Integral ceramic fabric surface layer essential for resistance to flames and chemicals. Endures high temperature, impedes flame from penetrating to interior, inhibits diffusion of oxygen to interior where it degrades matrix resin, resists attack by chemicals, helps resist erosion, and provides additional strength. In original intended application, composite members replace steel structural members of rocket-launching structures that deteriorate under combined influences of atmosphere, spilled propellants, and rocket exhaust. Composites also attractive for other applications in which corrosion- and fire-resistant structural members needed.

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BibTeXRIS

Spears, Richard K.. 1995-02-01. Flame-Resistant Composite Materials For Structural Members. https://ntrs.nasa.gov/citations/19950065227

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