Carbon Fiber Tape and Sheet Epoxy Resin Impregnated G 200,000 (1379) Tensile, 21,000,000 (145) Modulus, 175 (347)
- Aerospace Material Specification
Data Sets - Support Documents
|Unnamed Dataset 1|
|TABLE I||MECHANICAL PROPERTIES OF CURED LAMINATES|
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.