Radome, Foam Sandwich Hot-Melt, Addition-Type Polyimide
- Aerospace Material Specification
- AMS3913B
- Reaffirmed
Scope
Rationale
Recommended Content
Aerospace Standard | EFFECTS OF NO-BREAK POWER TRANSFER ON 400 HZ AUXILIARY-POWER UNITS AND GROUND-POWER UNITS |
Aerospace Material Specification | Radomes, Foam Sandwich Polyimide/Quartz Cloth Construction |
Aerospace Material Specification | Adhesive, Contact Polychloroprene (CR) Rubber, Resin Modified |
Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 | ||
Unnamed Dataset 2 | ||
TABLE 1 | Polyimide Syntactic Foam Grout Formulation | |
TABLE 2 | Polyimide Surface Filler Formulation | |
TABLE 3 | Properties |
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.