Adhesive Film, Epoxy-Base, High Durability For 95 °C (200 °F) Service
- Aerospace Material Specification
|Technical Paper||Numerical Analysis for Mixing Process of High-speed Unsteady Jets Using PDF-CFD Model|
|Aerospace Material Specification||Adhesive Film, Epoxy-Base, High Durability For 120 °C (250 °F) Service|
|Aerospace Material Specification||Tape, Adhesive, Pressure-Sensitive Thermal Radiation Resistant, Aluminum Coated Glass Cloth|
Data Sets - Support Documents
|TABLE I (SI)|
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.