This specification covers glass roving impregnated with epoxy resin, the resin being partially processed to a "B" stage condition.
This roving has been used typically in high strength filament-wound structures for aircraft, missiles, and related structures, but usage is not limited to such applications.
This roving has been used typically in high strength filament-wound structures for aircraft, missiles, and related structures, but usage is not limited to such applications.
SAE AMS3828C History
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