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Magnesium alloys have high strength-to-weight ratios due to their light density of 1.8 gm/cc. They are two-thirds the weight of aluminum and one-fourth the weight of steel. This allows for weight savings in aircraft, vehicles, and other structural applications. Magnesium alloys can be heat treated to further increase their strength through processes like solutionizing, aging, and precipitation hardening. Common alloying elements in magnesium alloys include aluminum, manganese, and zinc, which enhance proper

Author

Nelson Alvarez

Language

EN