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ISO-WD21150 Magnesium vs. C71520 Copper-nickel

ISO-WD21150 magnesium belongs to the magnesium alloys classification, while C71520 copper-nickel belongs to the copper alloys. There are 29 material properties with values for both materials. Properties with values for just one material (1, 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 C71520 copper-nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
140
Elongation at Break, % 5.7 to 11
10 to 45
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 17
51
Shear Strength, MPa 150 to 170
250 to 340
Tensile Strength: Ultimate (UTS), MPa 240 to 290
370 to 570
Tensile Strength: Yield (Proof), MPa 120 to 200
140 to 430

Thermal Properties

Latent Heat of Fusion, J/g 350
230
Maximum Temperature: Mechanical, °C 110
260
Melting Completion (Liquidus), °C 600
1170
Melting Onset (Solidus), °C 550
1120
Specific Heat Capacity, J/kg-K 990
400
Thermal Conductivity, W/m-K 100
32
Thermal Expansion, µm/m-K 27
15

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 19
5.7
Electrical Conductivity: Equal Weight (Specific), % IACS 100
5.8

Otherwise Unclassified Properties

Base Metal Price, % relative 12
40
Density, g/cm3 1.7
8.9
Embodied Carbon, kg CO2/kg material 23
5.0
Embodied Energy, MJ/kg 160
73
Embodied Water, L/kg 980
280

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 15 to 24
54 to 130
Resilience: Unit (Modulus of Resilience), kJ/m3 160 to 460
67 to 680
Stiffness to Weight: Axial, points 15
8.6
Stiffness to Weight: Bending, points 70
19
Strength to Weight: Axial, points 40 to 48
12 to 18
Strength to Weight: Bending, points 52 to 58
13 to 17
Thermal Diffusivity, mm2/s 60
8.9
Thermal Shock Resistance, points 15 to 17
12 to 19

Alloy Composition

Aluminum (Al), % 2.4 to 3.6
0
Carbon (C), % 0
0 to 0.050
Copper (Cu), % 0 to 0.050
65 to 71.6
Iron (Fe), % 0 to 0.0050
0.4 to 1.0
Lead (Pb), % 0
0 to 0.020
Magnesium (Mg), % 94 to 97
0
Manganese (Mn), % 0.15 to 0.4
0 to 1.0
Nickel (Ni), % 0 to 0.0050
28 to 33
Phosphorus (P), % 0
0 to 0.2
Silicon (Si), % 0 to 0.1
0
Sulfur (S), % 0
0 to 0.020
Zinc (Zn), % 0.5 to 1.5
0 to 0.5
Residuals, % 0
0 to 0.5