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N06230 Nickel vs. ZC63A Magnesium

N06230 nickel belongs to the nickel alloys classification, while ZC63A magnesium belongs to the magnesium alloys. There are 30 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 N06230 nickel and the bottom bar is ZC63A magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 210
48
Elongation at Break, % 38 to 48
3.3
Fatigue Strength, MPa 250 to 360
94
Poisson's Ratio 0.28
0.29
Shear Modulus, GPa 83
19
Shear Strength, MPa 420 to 600
130
Tensile Strength: Ultimate (UTS), MPa 620 to 840
220
Tensile Strength: Yield (Proof), MPa 330 to 400
130

Thermal Properties

Latent Heat of Fusion, J/g 310
330
Maximum Temperature: Mechanical, °C 990
98
Melting Completion (Liquidus), °C 1370
550
Melting Onset (Solidus), °C 1300
470
Specific Heat Capacity, J/kg-K 420
950
Thermal Conductivity, W/m-K 8.9
120
Thermal Expansion, µm/m-K 13
26

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.4
32
Electrical Conductivity: Equal Weight (Specific), % IACS 1.3
140

Otherwise Unclassified Properties

Base Metal Price, % relative 85
13
Density, g/cm3 9.5
2.1
Embodied Carbon, kg CO2/kg material 11
22
Embodied Energy, MJ/kg 160
150
Embodied Water, L/kg 290
920

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 200 to 330
6.3
Resilience: Unit (Modulus of Resilience), kJ/m3 250 to 380
190
Stiffness to Weight: Axial, points 12
13
Stiffness to Weight: Bending, points 21
58
Strength to Weight: Axial, points 18 to 25
29
Strength to Weight: Bending, points 17 to 21
38
Thermal Diffusivity, mm2/s 2.3
58
Thermal Shock Resistance, points 17 to 23
12

Alloy Composition


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Aluminum (Al), % 0.2 to 0.5
0
Boron (B), % 0 to 0.015
0
Carbon (C), % 0.050 to 0.15
0
Chromium (Cr), % 20 to 24
0
Cobalt (Co), % 0 to 5.0
0
Copper (Cu), % 0
2.4 to 3.0
Iron (Fe), % 0 to 3.0
0
Lanthanum (La), % 0.0050 to 0.050
0
Magnesium (Mg), % 0
89.2 to 91.9
Manganese (Mn), % 0.3 to 1.0
0.25 to 0.75
Molybdenum (Mo), % 1.0 to 3.0
0
Nickel (Ni), % 47.5 to 65.2
0 to 0.010
Phosphorus (P), % 0 to 0.030
0
Silicon (Si), % 0.25 to 0.75
0 to 0.2
Sulfur (S), % 0 to 0.015
0
Tungsten (W), % 13 to 15
0
Zinc (Zn), % 0
5.5 to 6.5
Residuals, % 0
0 to 0.3