Advanced Composites Prepreg – Nominal 250 °F Cure –Glass Fiber and Epoxy Resin, 7781 Weave Fabric
- Aerospace Material Specification
- AMS3915
- Issued
Scope
Rationale
Recommended Content
Topic
Data Sets - Support Documents
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| TABLE 1 | UNCURED PREPREG PHYSICAL AND CHEMICAL PROPERTIES | |
| TABLE 2 | CURED LAMINA PHYSICAL PROPERTIES | |
| TABLE 4 | TEST PANEL REQUIREMENTS |
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.