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EN 2.4665 Nickel vs. EN-MC21120 Magnesium

EN 2.4665 nickel belongs to the nickel alloys classification, while EN-MC21120 magnesium belongs to the magnesium 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 2.4665 nickel and the bottom bar is EN-MC21120 magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 210
46
Elongation at Break, % 34
2.2 to 6.7
Fatigue Strength, MPa 220
84 to 96
Poisson's Ratio 0.28
0.29
Shear Modulus, GPa 81
18
Shear Strength, MPa 520
110 to 160
Tensile Strength: Ultimate (UTS), MPa 790
200 to 270
Tensile Strength: Yield (Proof), MPa 300
130 to 170

Thermal Properties

Latent Heat of Fusion, J/g 320
350
Maximum Temperature: Mechanical, °C 990
130
Melting Completion (Liquidus), °C 1460
600
Melting Onset (Solidus), °C 1410
490
Specific Heat Capacity, J/kg-K 450
990
Thermal Conductivity, W/m-K 12
76
Thermal Expansion, µm/m-K 14
26

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.5
11
Electrical Conductivity: Equal Weight (Specific), % IACS 1.6
59

Otherwise Unclassified Properties

Base Metal Price, % relative 55
12
Density, g/cm3 8.4
1.7
Embodied Carbon, kg CO2/kg material 9.2
22
Embodied Energy, MJ/kg 130
160
Embodied Water, L/kg 270
990

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 210
5.0 to 15
Resilience: Unit (Modulus of Resilience), kJ/m3 220
180 to 320
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 23
69
Strength to Weight: Axial, points 26
31 to 43
Strength to Weight: Bending, points 22
43 to 53
Thermal Diffusivity, mm2/s 3.2
44
Thermal Shock Resistance, points 20
11 to 16

Alloy Composition

Aluminum (Al), % 0 to 0.5
8.3 to 9.7
Boron (B), % 0 to 0.010
0
Carbon (C), % 0.050 to 0.15
0
Chromium (Cr), % 20.5 to 23
0
Cobalt (Co), % 0.5 to 2.5
0
Copper (Cu), % 0 to 0.5
0 to 0.030
Iron (Fe), % 17 to 20
0 to 0.0050
Magnesium (Mg), % 0
88.6 to 91.3
Manganese (Mn), % 0 to 1.0
0.1 to 0.5
Molybdenum (Mo), % 8.0 to 10
0
Nickel (Ni), % 40.3 to 53.8
0 to 0.0020
Phosphorus (P), % 0 to 0.020
0
Silicon (Si), % 0 to 1.0
0 to 0.2
Sulfur (S), % 0 to 0.015
0
Tungsten (W), % 0.2 to 1.0
0
Zinc (Zn), % 0
0.35 to 1.0
Residuals, % 0
0 to 0.010