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N06230 Nickel vs. WE54A Magnesium

N06230 nickel belongs to the nickel alloys classification, while WE54A 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 WE54A magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 210
44
Elongation at Break, % 38 to 48
4.3 to 5.6
Fatigue Strength, MPa 250 to 360
98 to 130
Poisson's Ratio 0.28
0.29
Shear Modulus, GPa 83
17
Shear Strength, MPa 420 to 600
150 to 170
Tensile Strength: Ultimate (UTS), MPa 620 to 840
270 to 300
Tensile Strength: Yield (Proof), MPa 330 to 400
180

Thermal Properties

Latent Heat of Fusion, J/g 310
330
Maximum Temperature: Mechanical, °C 990
170
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
52
Thermal Expansion, µm/m-K 13
25

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.4
10
Electrical Conductivity: Equal Weight (Specific), % IACS 1.3
47

Otherwise Unclassified Properties

Base Metal Price, % relative 85
34
Density, g/cm3 9.5
1.9
Embodied Carbon, kg CO2/kg material 11
29
Embodied Energy, MJ/kg 160
260
Embodied Water, L/kg 290
900

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 200 to 330
10 to 14
Resilience: Unit (Modulus of Resilience), kJ/m3 250 to 380
360 to 380
Stiffness to Weight: Axial, points 12
13
Stiffness to Weight: Bending, points 21
62
Strength to Weight: Axial, points 18 to 25
39 to 43
Strength to Weight: Bending, points 17 to 21
49 to 51
Thermal Diffusivity, mm2/s 2.3
28
Thermal Shock Resistance, points 17 to 23
18 to 19

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
88.7 to 93.4
Manganese (Mn), % 0.3 to 1.0
0 to 0.030
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
1.5 to 4.0
Yttrium (Y), % 0
4.8 to 5.5
Zinc (Zn), % 0
0 to 0.2
Zirconium (Zr), % 0
0.4 to 1.0
Residuals, % 0
0 to 0.3