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WE54A Magnesium vs. Nickel 600

WE54A magnesium belongs to the magnesium alloys classification, while nickel 600 belongs to the nickel alloys. There are 30 material properties with values for both materials. Properties with values for just one material (4, 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 nickel 600.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 44
190
Elongation at Break, % 4.3 to 5.6
3.4 to 35
Fatigue Strength, MPa 98 to 130
220 to 300
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 17
75
Shear Strength, MPa 150 to 170
430 to 570
Tensile Strength: Ultimate (UTS), MPa 270 to 300
650 to 990
Tensile Strength: Yield (Proof), MPa 180
270 to 760

Thermal Properties

Latent Heat of Fusion, J/g 330
310
Maximum Temperature: Mechanical, °C 170
1100
Melting Completion (Liquidus), °C 640
1410
Melting Onset (Solidus), °C 570
1350
Specific Heat Capacity, J/kg-K 960
460
Thermal Conductivity, W/m-K 52
14
Thermal Expansion, µm/m-K 25
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 10
1.7
Electrical Conductivity: Equal Weight (Specific), % IACS 47
1.8

Otherwise Unclassified Properties

Base Metal Price, % relative 34
55
Density, g/cm3 1.9
8.5
Embodied Carbon, kg CO2/kg material 29
9.0
Embodied Energy, MJ/kg 260
130
Embodied Water, L/kg 900
250

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 10 to 14
31 to 180
Resilience: Unit (Modulus of Resilience), kJ/m3 360 to 380
190 to 1490
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 62
23
Strength to Weight: Axial, points 39 to 43
21 to 32
Strength to Weight: Bending, points 49 to 51
20 to 26
Thermal Diffusivity, mm2/s 28
3.6
Thermal Shock Resistance, points 18 to 19
19 to 29

Alloy Composition


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Carbon (C), % 0
0 to 0.15
Chromium (Cr), % 0
14 to 17
Copper (Cu), % 0 to 0.030
0 to 0.5
Iron (Fe), % 0 to 0.010
6.0 to 10
Lithium (Li), % 0 to 0.2
0
Magnesium (Mg), % 88.7 to 93.4
0
Manganese (Mn), % 0 to 0.030
0 to 1.0
Nickel (Ni), % 0 to 0.0050
72 to 80
Silicon (Si), % 0 to 0.010
0 to 0.5
Sulfur (S), % 0
0 to 0.015
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