SAE AMS4302A
Aluminum Alloy, Laminated, Sheet, Aramid Fiber Reinforced, 5.7zn 2.2mg 1.6cu 0.22cr, 3, 5, Or 7 Ply.
Standard:
AKA:
- AMS4302
- Revision: A
- 2000-10-01
- 1992-01-01
- Historical. Access the latest revision: AMS4302B
- Ams D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of sheet laminated with one or more layers of unidirectional aramid fiber/epoxy prepreg. This product has been used typically for structural parts requiring a combination of high fatigue-crack-growth resistance, fracture toughness, and resistance to corrosion, but usage is not limited to such applications.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS4302B | 2006-09-22 | Latest | |
| AMS4302A | 1992-01-01 | Historical | |
| AMS4302 | 1990-01-01 | Historical |
- SAE AMS 4302
- Aerospace
- Aluminum alloys
- Aluminum