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EN-MC21120 Magnesium vs. N06455 Nickel

EN-MC21120 magnesium belongs to the magnesium alloys classification, while N06455 nickel belongs to the nickel 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 EN-MC21120 magnesium and the bottom bar is N06455 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
210
Elongation at Break, % 2.2 to 6.7
47
Fatigue Strength, MPa 84 to 96
290
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 18
82
Shear Strength, MPa 110 to 160
550
Tensile Strength: Ultimate (UTS), MPa 200 to 270
780
Tensile Strength: Yield (Proof), MPa 130 to 170
330

Thermal Properties

Latent Heat of Fusion, J/g 350
320
Maximum Temperature: Mechanical, °C 130
960
Melting Completion (Liquidus), °C 600
1510
Melting Onset (Solidus), °C 490
1450
Specific Heat Capacity, J/kg-K 990
430
Thermal Conductivity, W/m-K 76
10
Thermal Expansion, µm/m-K 26
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 11
1.4
Electrical Conductivity: Equal Weight (Specific), % IACS 59
1.4

Otherwise Unclassified Properties

Base Metal Price, % relative 12
65
Density, g/cm3 1.7
8.8
Embodied Carbon, kg CO2/kg material 22
12
Embodied Energy, MJ/kg 160
160
Embodied Water, L/kg 990
290

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 5.0 to 15
300
Resilience: Unit (Modulus of Resilience), kJ/m3 180 to 320
260
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 69
23
Strength to Weight: Axial, points 31 to 43
24
Strength to Weight: Bending, points 43 to 53
21
Thermal Diffusivity, mm2/s 44
2.7
Thermal Shock Resistance, points 11 to 16
24

Alloy Composition


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Aluminum (Al), % 8.3 to 9.7
0
Carbon (C), % 0
0 to 0.015
Chromium (Cr), % 0
14 to 18
Cobalt (Co), % 0
0 to 2.0
Copper (Cu), % 0 to 0.030
0
Iron (Fe), % 0 to 0.0050
0 to 3.0
Magnesium (Mg), % 88.6 to 91.3
0
Manganese (Mn), % 0.1 to 0.5
0 to 1.0
Molybdenum (Mo), % 0
14 to 17
Nickel (Ni), % 0 to 0.0020
58.1 to 72
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.2
0 to 0.080
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0
0 to 0.7
Zinc (Zn), % 0.35 to 1.0
0
Residuals, % 0 to 0.010
0