Yarn, Organic Fiber (Para-Aramid) Intermediate Modulus 1000 Denier (1110 Dtex), 1.0% Finish
- Aerospace Material Specification
|Aerospace Material Specification||Yarn, Organic Fiber (Para-Aramid) Intermediate Modulus 1500 Denier (1670 Dtex), 0.9% Finish|
|Aerospace Standard||CONNECTOR ACCESSORIES, FIBER OPTIC BACKSHELL, 45°, SELF-LOCKING CATEGORY 3B FOR MIL-DTL-38999 SERIES III & SAE AS5590/1 CONNECTORS|
|Aerospace Material Specification||Tow or Yarn, Carbon Fibers For Structural Composites GF 400 (2758) Tensile Strength, 33 (228) 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.