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WE43A Magnesium vs. N06230 Nickel

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

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Electrical Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition


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Aluminum (Al), % 0
0.2 to 0.5
Boron (B), % 0
0 to 0.015
Carbon (C), % 0
0.050 to 0.15
Chromium (Cr), % 0
20 to 24
Cobalt (Co), % 0
0 to 5.0
Copper (Cu), % 0 to 0.030
0
Iron (Fe), % 0 to 0.010
0 to 3.0
Lanthanum (La), % 0
0.0050 to 0.050
Lithium (Li), % 0 to 0.2
0
Magnesium (Mg), % 89.5 to 93.5
0
Manganese (Mn), % 0 to 0.15
0.3 to 1.0
Molybdenum (Mo), % 0
1.0 to 3.0
Nickel (Ni), % 0 to 0.0050
47.5 to 65.2
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0 to 0.010
0.25 to 0.75
Sulfur (S), % 0
0 to 0.015
Tungsten (W), % 0
13 to 15
Unspecified Rare Earths, % 2.4 to 4.4
0
Yttrium (Y), % 3.7 to 4.3
0
Zinc (Zn), % 0 to 0.2
0
Zirconium (Zr), % 0.4 to 1.0
0
Residuals, % 0 to 0.3
0