Yarn, Organic Fiber (Para-Aramid) Intermediate Modulus 3000 Denier (3300 Dtex), 0.9% Finish
- Aerospace Material Specification
|Aerospace Material Specification||Yarn, Organic Fiber (Para-Aramid), High Modulus 2160 Denier (2400 d tex), 0.6% Finish|
|Aerospace Material Specification||Yarn, Organic Fiber (Para-Aramid), High Modulus 2840 (3160 d tex) Denier, 0.6% Finish|
|Aerospace Material Specification||Tow, Carbon Fiber For Structural Composites 500 (3447) Tensile Strength, 32 (221) Tensile Modulus|
Data Sets - Support Documents
|[Unnamed Dataset 1]|
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.