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WE54A Magnesium vs. N06230 Nickel

WE54A 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 (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 WE54A 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, % 4.3 to 5.6
38 to 48
Fatigue Strength, MPa 98 to 130
250 to 360
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 17
83
Shear Strength, MPa 150 to 170
420 to 600
Tensile Strength: Ultimate (UTS), MPa 270 to 300
620 to 840
Tensile Strength: Yield (Proof), MPa 180
330 to 400

Thermal Properties

Latent Heat of Fusion, J/g 330
310
Maximum Temperature: Mechanical, °C 170
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 52
8.9
Thermal Expansion, µm/m-K 25
13

Electrical Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition

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