SAE AMS3915A-2015 PDF

Scope: Form This specification establishes the requirements for a nominal 250 ??cure epoxy preimpregnated 7781 glass fabric. The prepreg has a nominal fiber areal weight of 294 gsm@ and nominal resin content of 38%. Purpose a. The purpose of this specification is to allow procurement of a defined material corresponding to the statistically derived material properties published in CMH-17 Volume II. b. This material is intended for use in laminate applications with a service temperature of -65 to 180 ?? c. The composite may be used for the manufacture of primary and secondary aircraft structure.

SAE AMS3915A-2015 history

2015 SAE AMS3915A-2015 Advanced Composites Prepreg - Nominal 250 degree F Cure - Glass Fiber and Epoxy Resin, 7781 Weave Fabric
2013 SAE AMS3915-2013 Advanced Composites Prepreg - Nominal 250 degree F Cure - Glass Fiber and Epoxy Resin, 7781 Weave Fabric