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Nickel 601 vs. WE54A Magnesium

Nickel 601 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 (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 nickel 601 and the bottom bar is WE54A magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Electrical Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition

Aluminum (Al), % 1.0 to 1.7
0
Carbon (C), % 0 to 0.1
0
Chromium (Cr), % 21 to 25
0
Copper (Cu), % 0 to 1.0
0 to 0.030
Iron (Fe), % 7.7 to 20
0 to 0.010
Lithium (Li), % 0
0 to 0.2
Magnesium (Mg), % 0
88.7 to 93.4
Manganese (Mn), % 0 to 1.0
0 to 0.030
Nickel (Ni), % 58 to 63
0 to 0.0050
Silicon (Si), % 0 to 0.5
0 to 0.010
Sulfur (S), % 0 to 0.015
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