Alloy 5052

Alloy 5052

Product catalog summary
Chemical Composition Limits:
The document outlines the chemical composition limits for Alloy 5052, including elements such as Copper (Cu), Magnesium (Mg), Manganese (Mn), Silicon (Si), Iron (Fe), Zinc (Zn), and Titanium (Ti). The specified ranges are crucial for maintaining the alloy's properties.
Typical Physical Properties:
The average melting range is between 1125-1200°F, with a thermal conductivity of 960 in English units. The coefficient of thermal expansion is 13.2 per °F from 68-212°F.
Typical US Mechanical Properties:
The document provides mechanical properties such as tension strength, hardness, and shear strength for different tempers of Alloy 5052. For example, the ultimate tensile strength ranges from 28 to 42 KSI, and the yield strength ranges from 13 to 37 KSI.
Electrical Properties:
Electrical conductivity and resistivity are provided at 682°F, with conductivity equal to 35 and resistivity equal to 116 ohm-cir. mil/foot.
Fatigue and Modulus Properties:
The fatigue endurance limit ranges from 16 to 20 KSI, and the modulus of elasticity is consistently 10.2 x 103 KSI across different tempers.
Disclaimer:
The document notes that the typical properties are averages and not guaranteed, as they vary based on size, product forms, and manufacturing methods. They are intended for comparison purposes and not for engineering specifications or design purposes.
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Catalog excerpts

Alloy 5052-1

Chemical Composition Limits WEIGHT% MINIMUM MAXIMUM Typical Physical Properties AVERAGE COEFFICIENT OF THERMAL EXPANSION (68-212°F PER F) MELTING RANGE APPROX. THERMAL ELECTRICAL EQUAL EQUAL VOLUME WEIGHT OHM-CIR. MIL/FOOT 116 30 Typical US Mechanical Properties ALLOY AND TEMPER The following typical properties are not guaranteed, since in most cases they are averages for various sizes, product forms and methods of manufacture and may not be exactly representative of any particular product or size. This data is intended only as a basis for comparing alloys and tempers and should not be specified as engineering requirements or used for design purposes. AMK Aero Metals Alliance

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