SAE AMS6891 PDF
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Carbon Fiber and Fiberglass Epoxy Prepreg Products with 350 °F (177 °C) Cure for Aerospace Applications
Description
The intent of this specification is for the procurement of carbon fiber and fiberglass epoxy prepreg products with 350 °F (177 °C) cure for aerospace applications; therefore, no qualification or equivalency threshold values are provided. Users that intend to conduct a new material qualification or equivalency program must refer to the production quality assurance section (4.3) of this base specification, AMS6891.
History
| AMS6891 | 2020-12-30 | Latest | Issued |
| ISSUING COMMITTEE | AMS P17 Polymer Matrix Composites Committee |
|---|---|
| DATE | 2020-12-30 |
| DOI | |
| ISCURRENT | Current |
| PAGE | 27 |
| PUBLISHER | SAE International |
| REVISED | ISSUED |
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