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WE54A Magnesium vs. Nickel 601

WE54A magnesium belongs to the magnesium alloys classification, while nickel 601 belongs to the nickel alloys. There are 30 material properties with values for both materials. Properties with values for just one material (3, 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 601.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 44
200
Elongation at Break, % 4.3 to 5.6
10 to 38
Fatigue Strength, MPa 98 to 130
220 to 380
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 17
76
Shear Strength, MPa 150 to 170
440 to 530
Tensile Strength: Ultimate (UTS), MPa 270 to 300
660 to 890
Tensile Strength: Yield (Proof), MPa 180
290 to 800

Thermal Properties

Latent Heat of Fusion, J/g 330
320
Maximum Temperature: Mechanical, °C 170
1100
Melting Completion (Liquidus), °C 640
1410
Melting Onset (Solidus), °C 570
1360
Specific Heat Capacity, J/kg-K 960
470
Thermal Conductivity, W/m-K 52
11
Thermal Expansion, µm/m-K 25
14

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 10
1.5
Electrical Conductivity: Equal Weight (Specific), % IACS 47
1.6

Otherwise Unclassified Properties

Base Metal Price, % relative 34
49
Density, g/cm3 1.9
8.3
Embodied Carbon, kg CO2/kg material 29
8.0
Embodied Energy, MJ/kg 260
110
Embodied Water, L/kg 900
280

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 10 to 14
86 to 200
Resilience: Unit (Modulus of Resilience), kJ/m3 360 to 380
210 to 1630
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 62
23
Strength to Weight: Axial, points 39 to 43
22 to 30
Strength to Weight: Bending, points 49 to 51
20 to 25
Thermal Diffusivity, mm2/s 28
2.8
Thermal Shock Resistance, points 18 to 19
17 to 23

Alloy Composition

Aluminum (Al), % 0
1.0 to 1.7
Carbon (C), % 0
0 to 0.1
Chromium (Cr), % 0
21 to 25
Copper (Cu), % 0 to 0.030
0 to 1.0
Iron (Fe), % 0 to 0.010
7.7 to 20
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
58 to 63
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