SAE AMS3828C PDF

Description

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.

Product Details

Published:

09/01/1998

File Size:

1 file , 30 KB

Note:

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