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EN-MC21120 Magnesium vs. N06219 Nickel

EN-MC21120 magnesium belongs to the magnesium alloys classification, while N06219 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 EN-MC21120 magnesium and the bottom bar is N06219 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
200
Elongation at Break, % 2.2 to 6.7
48
Fatigue Strength, MPa 84 to 96
270
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 18
79
Shear Strength, MPa 110 to 160
520
Tensile Strength: Ultimate (UTS), MPa 200 to 270
730
Tensile Strength: Yield (Proof), MPa 130 to 170
300

Thermal Properties

Latent Heat of Fusion, J/g 350
330
Maximum Temperature: Mechanical, °C 130
980
Melting Completion (Liquidus), °C 600
1430
Melting Onset (Solidus), °C 490
1380
Specific Heat Capacity, J/kg-K 990
450
Thermal Conductivity, W/m-K 76
10
Thermal Expansion, µm/m-K 26
12

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 11
1.3
Electrical Conductivity: Equal Weight (Specific), % IACS 59
1.4

Otherwise Unclassified Properties

Base Metal Price, % relative 12
60
Density, g/cm3 1.7
8.5
Embodied Carbon, kg CO2/kg material 22
11
Embodied Energy, MJ/kg 160
140
Embodied Water, L/kg 990
290

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 5.0 to 15
280
Resilience: Unit (Modulus of Resilience), kJ/m3 180 to 320
230
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
21

Alloy Composition


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Aluminum (Al), % 8.3 to 9.7
0 to 0.5
Carbon (C), % 0
0 to 0.050
Chromium (Cr), % 0
18 to 22
Cobalt (Co), % 0
0 to 1.0
Copper (Cu), % 0 to 0.030
0 to 0.5
Iron (Fe), % 0 to 0.0050
2.0 to 4.0
Magnesium (Mg), % 88.6 to 91.3
0
Manganese (Mn), % 0.1 to 0.5
0 to 0.5
Molybdenum (Mo), % 0
7.0 to 9.0
Nickel (Ni), % 0 to 0.0020
60.8 to 72.3
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0 to 0.2
0.7 to 1.1
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0
0 to 0.5
Zinc (Zn), % 0.35 to 1.0
0
Residuals, % 0 to 0.010
0