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ISO-WD32350 Magnesium vs. N10665 Nickel

ISO-WD32350 magnesium belongs to the magnesium alloys classification, while N10665 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-WD32350 magnesium and the bottom bar is N10665 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
220
Elongation at Break, % 5.7 to 10
45
Fatigue Strength, MPa 120 to 130
340
Poisson's Ratio 0.29
0.31
Shear Modulus, GPa 18
84
Shear Strength, MPa 150 to 170
600
Tensile Strength: Ultimate (UTS), MPa 250 to 290
860
Tensile Strength: Yield (Proof), MPa 140 to 180
400

Thermal Properties

Latent Heat of Fusion, J/g 340
310
Maximum Temperature: Mechanical, °C 95
900
Melting Completion (Liquidus), °C 600
1620
Melting Onset (Solidus), °C 560
1570
Specific Heat Capacity, J/kg-K 990
390
Thermal Conductivity, W/m-K 130
11
Thermal Expansion, µm/m-K 25
10

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 12
75
Density, g/cm3 1.7
9.3
Embodied Carbon, kg CO2/kg material 23
15
Embodied Energy, MJ/kg 160
200
Embodied Water, L/kg 960
270

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 23
320
Resilience: Unit (Modulus of Resilience), kJ/m3 210 to 380
360
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 68
22
Strength to Weight: Axial, points 39 to 46
26
Strength to Weight: Bending, points 50 to 55
22
Thermal Diffusivity, mm2/s 73
3.1
Thermal Shock Resistance, points 16 to 18
27

Alloy Composition

Aluminum (Al), % 0 to 0.1
0
Carbon (C), % 0
0 to 0.020
Chromium (Cr), % 0
0 to 1.0
Cobalt (Co), % 0
0 to 1.0
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0 to 0.060
0 to 2.0
Magnesium (Mg), % 95.7 to 97.7
0
Manganese (Mn), % 0.6 to 1.3
0 to 1.0
Molybdenum (Mo), % 0
26 to 30
Nickel (Ni), % 0 to 0.0050
64.8 to 74
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.1
0 to 0.1
Sulfur (S), % 0
0 to 0.030
Zinc (Zn), % 1.8 to 2.3
0
Residuals, % 0 to 0.3
0