Adhesive Compound, Epoxy Resin High Temperature Application
- Aerospace Material Specification
|Ground Vehicle Standard||Laboratory Cyclic Corrosion Test|
|Aerospace Material Specification||Adhesive Compound, Epoxy Room Temperature Curing|
|Aerospace Material Specification||Silicone (VMQ) Rubber Sheet, Glass Cloth Reinforced|
Data Sets - Support Documents
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.