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SAE AMS 6562:2023-08-01

Medium Temperature, Out-of-Autoclave, Oven-Vacuum-Bag Cure Epoxy Resin Impregnated Fiber Reinforced Composite Materials

Summary

The purpose of this specification is to allow procurement of defined carbon fiber and fiberglass epoxy prepreg materials corresponding to their statistically derived material properties published in CMH-17 (formerly MIL-HDBK-17). As a result, no qualification or equivalency threshold values are provided. Users that intend to conduct a new material qualification or equivalency program shall notify the Qualifying Agency per 4.2.1.

Technical characteristics

Publisher SAE International
Publication Date 08/01/2023
Page Count 25
Themes Aerospace
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ISBN ---
Weight (in grams) ---
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