Carbon Fiber and Fiberglass Epoxy Prepreg Products with 350 °F (177 °C) Cure for Aerospace Applications: Type 35, Class 1, Grade 191
- Aerospace Material Specification
- AMS6891/1
- Issued
Scope
Rationale
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Table 1 | Uncured prepreg physical and chemical property | |
| Table 2 | Cured laminate physical properties | |
| Table 3 | Cured laminate mechanical properties |
Issuing Committee
AMS P17 Polymer Matrix Composites Committee
AMS P-17, Polymer Matrix Composites, is a technical committee in SAE’s Aerospace Materials Systems Group with the responsibility to develop and maintain material specifications and other SAE technical reports for composite materials, including prepregs, reinforcing fibers and fabrics, matrix resins, adhesives, and core materials. The committee works in conjunction with related bodies such as the Composite Materials Handbook -17 (CMH-17), ASTM Committee D30 on Composite Materials, the National Center for Advanced Materials Performance (NCAMP), the Performance Review Institute (PRI), and regulatory authorities such as FAA and EASA.
Reference
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