Cloth, Organic Fiver (Para-Aramid), High Modulus For Structural Composites
- Aerospace Material Specification
- AMS3902E
- Reaffirmed
Scope
Rationale
Recommended Content
Aerospace Material Specification | Coating System, Polyurethane, Nonyellowing, White, Rain Erosion Resistant, Thermally Reflective |
Aerospace Material Specification | Core, Honeycomb Fibrous, Aramid Base, Phenolic Coated |
Aerospace Material Specification | Tow or Yarn, Carbon Fibers For Structural Composites GF 400 (2758) Tensile Strength, 33 (228) Tensile Modulus |
Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 | ||
TABLE 1 | Construction of Woven Organic Cloth | |
TABLE 2 | Classification of Imperfections | |
TABLE 3 | Weight Tolerances | |
TABLE 4A | Thickness Tolerances, Inch/Pound Units | |
TABLE 4B | Thickness Tolerances, SI Units | |
TABLE 5A | Sample Size, Inch/Pound Units | |
TABLE 5B | Sample Size, SI Units | |
Unnamed Dataset 9 |
Issuing Committee
AMS P17 Polymer Matrix Composites Committee
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.