Name | Support | Language | Availability | Edition date | Price | ||
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PDF |
English |
Active |
12/30/2020 |
€120.00 |
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Details
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.
Additional Info
Author | Society of Automotive Engineers International (SAE) |
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Committee | AMS P17 Polymer Matrix Composites Committee |
Published by | SAE |
Document type | Standard |
Number of pages | 27 |
Keyword | SAE 6891,SAE AMS6891,SAE AMS6891,SAE AMS 6891 |