"Form: This specification covers glass roving impregnated with epoxy resin@ the resin being partially processed to a ""B"" stage condition. Application: 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. Safety - Hazardous Materials: While the materials@ methods@ applications@ and processes described or referenced in this specification may involve the use of hazardous materials@ this specification does not address the hazards which may be involved in such use. It is the sole responsibility of the user to ensure familiarity with the safe and proper use of any hazardous materials and to take necessary precautionary measures to ensure the health and safety of all personnel involved."
SAE AMS3828D-2016 history
2016SAE AMS3828D-2016 Glass Roving@ Epoxy Resin Preimpregnated Type E Glass
1998SAE AMS3828C-1998 Glass Roving, Epoxy Resin Preimpregnated Type E Glass
1993SAE AMS3828C-1993 Glass Roving, Epoxy Resin Preimpregnated Type E Glass
1989SAE AMS3828B-1989 GLASS ROVING, EPOXY RESIN PREIMPREGNATED Type E Glass
1983SAE AMS3828A-1983 GLASS ROVING, EPOXY RESIN PREIMPREGNATED Type E Glass
1968SAE AMS3828-1968 GLASS ROVING, EPOXY RESIN PREIMPREGNATED Type E Glass