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EN-MC21120 Magnesium vs. N08024 Nickel

EN-MC21120 magnesium belongs to the magnesium alloys classification, while N08024 nickel belongs to the nickel alloys. There are 30 material properties with values for both materials. Properties with values for just one material (2, 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 EN-MC21120 magnesium and the bottom bar is N08024 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
200
Elongation at Break, % 2.2 to 6.7
34
Fatigue Strength, MPa 84 to 96
200
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
79
Shear Strength, MPa 110 to 160
410
Tensile Strength: Ultimate (UTS), MPa 200 to 270
620
Tensile Strength: Yield (Proof), MPa 130 to 170
270

Thermal Properties

Latent Heat of Fusion, J/g 350
310
Maximum Temperature: Mechanical, °C 130
990
Melting Completion (Liquidus), °C 600
1430
Melting Onset (Solidus), °C 490
1380
Specific Heat Capacity, J/kg-K 990
460
Thermal Conductivity, W/m-K 76
12
Thermal Expansion, µm/m-K 26
15

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 11
1.6
Electrical Conductivity: Equal Weight (Specific), % IACS 59
1.8

Otherwise Unclassified Properties

Base Metal Price, % relative 12
41
Density, g/cm3 1.7
8.2
Embodied Carbon, kg CO2/kg material 22
7.2
Embodied Energy, MJ/kg 160
99
Embodied Water, L/kg 990
230

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 5.0 to 15
170
Resilience: Unit (Modulus of Resilience), kJ/m3 180 to 320
180
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 69
24
Strength to Weight: Axial, points 31 to 43
21
Strength to Weight: Bending, points 43 to 53
20
Thermal Diffusivity, mm2/s 44
3.2
Thermal Shock Resistance, points 11 to 16
15

Alloy Composition

Aluminum (Al), % 8.3 to 9.7
0
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0
22.5 to 25
Copper (Cu), % 0 to 0.030
0.5 to 1.5
Iron (Fe), % 0 to 0.0050
26.6 to 38.4
Magnesium (Mg), % 88.6 to 91.3
0
Manganese (Mn), % 0.1 to 0.5
0 to 1.0
Molybdenum (Mo), % 0
3.5 to 5.0
Nickel (Ni), % 0 to 0.0020
35 to 40
Niobium (Nb), % 0
0.15 to 0.35
Phosphorus (P), % 0
0 to 0.035
Silicon (Si), % 0 to 0.2
0 to 0.5
Sulfur (S), % 0
0 to 0.035
Zinc (Zn), % 0.35 to 1.0
0
Residuals, % 0 to 0.010
0