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ISO-WD32250 Magnesium vs. Nickel 601

ISO-WD32250 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 (1, 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 ISO-WD32250 magnesium and the bottom bar is nickel 601.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
200
Elongation at Break, % 4.5 to 8.6
10 to 38
Fatigue Strength, MPa 170 to 210
220 to 380
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 17
76
Shear Strength, MPa 180 to 190
440 to 530
Tensile Strength: Ultimate (UTS), MPa 310 to 330
660 to 890
Tensile Strength: Yield (Proof), MPa 240 to 290
290 to 800

Thermal Properties

Latent Heat of Fusion, J/g 340
320
Maximum Temperature: Mechanical, °C 120
1100
Melting Completion (Liquidus), °C 600
1410
Melting Onset (Solidus), °C 550
1360
Specific Heat Capacity, J/kg-K 980
470
Thermal Conductivity, W/m-K 130
11
Thermal Expansion, µm/m-K 26
14

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 25
1.5
Electrical Conductivity: Equal Weight (Specific), % IACS 130
1.6

Otherwise Unclassified Properties

Base Metal Price, % relative 13
49
Density, g/cm3 1.8
8.3
Embodied Carbon, kg CO2/kg material 24
8.0
Embodied Energy, MJ/kg 160
110
Embodied Water, L/kg 950
280

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 26
86 to 200
Resilience: Unit (Modulus of Resilience), kJ/m3 630 to 930
210 to 1630
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 67
23
Strength to Weight: Axial, points 49 to 51
22 to 30
Strength to Weight: Bending, points 58 to 60
20 to 25
Thermal Diffusivity, mm2/s 72
2.8
Thermal Shock Resistance, points 19 to 20
17 to 23

Alloy Composition


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Aluminum (Al), % 0
1.0 to 1.7
Carbon (C), % 0
0 to 0.1
Chromium (Cr), % 0
21 to 25
Copper (Cu), % 0
0 to 1.0
Iron (Fe), % 0
7.7 to 20
Magnesium (Mg), % 94.9 to 97.1
0
Manganese (Mn), % 0
0 to 1.0
Nickel (Ni), % 0
58 to 63
Silicon (Si), % 0
0 to 0.5
Sulfur (S), % 0
0 to 0.015
Zinc (Zn), % 2.5 to 4.0
0
Zirconium (Zr), % 0.45 to 0.8
0
Residuals, % 0 to 0.3
0