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N06230 Nickel vs. WE43A Magnesium

N06230 nickel belongs to the nickel alloys classification, while WE43A magnesium belongs to the magnesium alloys. There are 30 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 N06230 nickel and the bottom bar is WE43A magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 210
44
Elongation at Break, % 38 to 48
5.2 to 5.4
Fatigue Strength, MPa 250 to 360
85 to 120
Poisson's Ratio 0.28
0.29
Shear Modulus, GPa 83
17
Shear Strength, MPa 420 to 600
160
Tensile Strength: Ultimate (UTS), MPa 620 to 840
250 to 270
Tensile Strength: Yield (Proof), MPa 330 to 400
160 to 170

Thermal Properties

Latent Heat of Fusion, J/g 310
330
Maximum Temperature: Mechanical, °C 990
180
Melting Completion (Liquidus), °C 1370
640
Melting Onset (Solidus), °C 1300
570
Specific Heat Capacity, J/kg-K 420
960
Thermal Conductivity, W/m-K 8.9
51
Thermal Expansion, µm/m-K 13
27

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.4
12
Electrical Conductivity: Equal Weight (Specific), % IACS 1.3
55

Otherwise Unclassified Properties

Base Metal Price, % relative 85
34
Density, g/cm3 9.5
1.9
Embodied Carbon, kg CO2/kg material 11
28
Embodied Energy, MJ/kg 160
250
Embodied Water, L/kg 290
910

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 200 to 330
12
Resilience: Unit (Modulus of Resilience), kJ/m3 250 to 380
280 to 310
Stiffness to Weight: Axial, points 12
13
Stiffness to Weight: Bending, points 21
61
Strength to Weight: Axial, points 18 to 25
36 to 39
Strength to Weight: Bending, points 17 to 21
46 to 48
Thermal Diffusivity, mm2/s 2.3
28
Thermal Shock Resistance, points 17 to 23
15 to 16

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
0 to 0.030
Iron (Fe), % 0 to 3.0
0 to 0.010
Lanthanum (La), % 0.0050 to 0.050
0
Lithium (Li), % 0
0 to 0.2
Magnesium (Mg), % 0
89.5 to 93.5
Manganese (Mn), % 0.3 to 1.0
0 to 0.15
Molybdenum (Mo), % 1.0 to 3.0
0
Nickel (Ni), % 47.5 to 65.2
0 to 0.0050
Phosphorus (P), % 0 to 0.030
0
Silicon (Si), % 0.25 to 0.75
0 to 0.010
Sulfur (S), % 0 to 0.015
0
Tungsten (W), % 13 to 15
0
Unspecified Rare Earths, % 0
2.4 to 4.4
Yttrium (Y), % 0
3.7 to 4.3
Zinc (Zn), % 0
0 to 0.2
Zirconium (Zr), % 0
0.4 to 1.0
Residuals, % 0
0 to 0.3