Browse Standards AMS6891
WIP 2012-01-17

Carbon Fiber and Fiberglass Epoxy Prepreg Products with 350°F Cure for Aerospace Applications AMS6891

The purpose of this specification is to allow procurement of a defined material corresponding to statistically derived material properties published in CMH-17. This material is intended for use in laminate applications with a service temperature up to 250°F for primary or secondary aircraft structures.
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This Standard is currently a WIP.