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SAE AMS4457
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SAE AMS4457 2008 Edition, August 1, 2008
Aluminum Alloy, Sheet 3.5Cu - 1.1Li - 0.50Mg - 0.40Ag - 0.12Zr (2098-T8)
Solution Heat Treated, Cold Worked, and Artificially Aged
Description / Abstract:
Form
This specification covers an aluminum alloy in the form of sheet.
Application
This product has been used for aircraft applications where if offers a combination of high strength and low density, but usage is not limited to such applications.
This specification covers an aluminum alloy in the form of sheet.
Application
This product has been used for aircraft applications where if offers a combination of high strength and low density, but usage is not limited to such applications.
SAE AMS4457 2008 Edition, August 1, 2008
Aluminum Alloy, Sheet 3.5Cu - 1.1Li - 0.50Mg - 0.40Ag - 0.12Zr (2098-T8)
Solution Heat Treated, Cold Worked, and Artificially Aged