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ISO-WD21150 Magnesium vs. C17500 Copper

ISO-WD21150 magnesium belongs to the magnesium alloys classification, while C17500 copper belongs to the copper alloys. There are 29 material properties with values for both materials. Properties with values for just one material (2, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.

For each property being compared, the top bar is ISO-WD21150 magnesium and the bottom bar is C17500 copper.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
120
Elongation at Break, % 5.7 to 11
6.0 to 30
Poisson's Ratio 0.29
0.34
Shear Modulus, GPa 17
45
Shear Strength, MPa 150 to 170
200 to 520
Tensile Strength: Ultimate (UTS), MPa 240 to 290
310 to 860
Tensile Strength: Yield (Proof), MPa 120 to 200
170 to 760

Thermal Properties

Latent Heat of Fusion, J/g 350
220
Maximum Temperature: Mechanical, °C 110
220
Melting Completion (Liquidus), °C 600
1060
Melting Onset (Solidus), °C 550
1020
Specific Heat Capacity, J/kg-K 990
390
Thermal Conductivity, W/m-K 100
200
Thermal Expansion, µm/m-K 27
18

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 19
24 to 53
Electrical Conductivity: Equal Weight (Specific), % IACS 100
24 to 54

Otherwise Unclassified Properties

Base Metal Price, % relative 12
60
Density, g/cm3 1.7
8.9
Embodied Carbon, kg CO2/kg material 23
4.7
Embodied Energy, MJ/kg 160
73
Embodied Water, L/kg 980
320

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 15 to 24
30 to 120
Resilience: Unit (Modulus of Resilience), kJ/m3 160 to 460
120 to 2390
Stiffness to Weight: Axial, points 15
7.5
Stiffness to Weight: Bending, points 70
18
Strength to Weight: Axial, points 40 to 48
9.7 to 27
Strength to Weight: Bending, points 52 to 58
11 to 23
Thermal Diffusivity, mm2/s 60
59
Thermal Shock Resistance, points 15 to 17
11 to 29

Alloy Composition


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Aluminum (Al), % 2.4 to 3.6
0 to 0.2
Beryllium (Be), % 0
0.4 to 0.7
Cobalt (Co), % 0
2.4 to 2.7
Copper (Cu), % 0 to 0.050
95.6 to 97.2
Iron (Fe), % 0 to 0.0050
0 to 0.1
Magnesium (Mg), % 94 to 97
0
Manganese (Mn), % 0.15 to 0.4
0
Nickel (Ni), % 0 to 0.0050
0
Silicon (Si), % 0 to 0.1
0 to 0.2
Zinc (Zn), % 0.5 to 1.5
0
Residuals, % 0 to 0.3
0 to 0.5