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ISO-WD32250 Magnesium vs. N10675 Nickel

ISO-WD32250 magnesium belongs to the magnesium alloys classification, while N10675 nickel 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 N10675 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
220
Elongation at Break, % 4.5 to 8.6
47
Fatigue Strength, MPa 170 to 210
350
Poisson's Ratio 0.29
0.31
Shear Modulus, GPa 17
85
Shear Strength, MPa 180 to 190
610
Tensile Strength: Ultimate (UTS), MPa 310 to 330
860
Tensile Strength: Yield (Proof), MPa 240 to 290
400

Thermal Properties

Latent Heat of Fusion, J/g 340
320
Maximum Temperature: Mechanical, °C 120
910
Melting Completion (Liquidus), °C 600
1420
Melting Onset (Solidus), °C 550
1370
Specific Heat Capacity, J/kg-K 980
380
Thermal Conductivity, W/m-K 130
11
Thermal Expansion, µm/m-K 26
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 25
1.3
Electrical Conductivity: Equal Weight (Specific), % IACS 130
1.2

Otherwise Unclassified Properties

Base Metal Price, % relative 13
80
Density, g/cm3 1.8
9.3
Embodied Carbon, kg CO2/kg material 24
16
Embodied Energy, MJ/kg 160
210
Embodied Water, L/kg 950
280

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 26
330
Resilience: Unit (Modulus of Resilience), kJ/m3 630 to 930
350
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 67
22
Strength to Weight: Axial, points 49 to 51
26
Strength to Weight: Bending, points 58 to 60
22
Thermal Diffusivity, mm2/s 72
3.1
Thermal Shock Resistance, points 19 to 20
26

Alloy Composition


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Aluminum (Al), % 0
0 to 0.5
Carbon (C), % 0
0 to 0.010
Chromium (Cr), % 0
1.0 to 3.0
Cobalt (Co), % 0
0 to 3.0
Copper (Cu), % 0
0 to 0.2
Iron (Fe), % 0
1.0 to 3.0
Magnesium (Mg), % 94.9 to 97.1
0
Manganese (Mn), % 0
0 to 3.0
Molybdenum (Mo), % 0
27 to 32
Nickel (Ni), % 0
51.3 to 71
Niobium (Nb), % 0
0 to 0.2
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0
0 to 0.1
Sulfur (S), % 0
0 to 0.010
Tantalum (Ta), % 0
0 to 0.2
Titanium (Ti), % 0
0 to 0.2
Tungsten (W), % 0
0 to 3.0
Vanadium (V), % 0
0 to 0.2
Zinc (Zn), % 2.5 to 4.0
0 to 0.1
Zirconium (Zr), % 0.45 to 0.8
0
Residuals, % 0 to 0.3
0