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EN 2.4669 Nickel vs. EN-MC21120 Magnesium

EN 2.4669 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 (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 2.4669 nickel and the bottom bar is EN-MC21120 magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
46
Elongation at Break, % 16
2.2 to 6.7
Fatigue Strength, MPa 390
84 to 96
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 73
18
Shear Strength, MPa 680
110 to 160
Tensile Strength: Ultimate (UTS), MPa 1110
200 to 270
Tensile Strength: Yield (Proof), MPa 720
130 to 170

Thermal Properties

Latent Heat of Fusion, J/g 310
350
Maximum Temperature: Mechanical, °C 960
130
Melting Completion (Liquidus), °C 1380
600
Melting Onset (Solidus), °C 1330
490
Specific Heat Capacity, J/kg-K 460
990
Thermal Conductivity, W/m-K 12
76
Thermal Expansion, µm/m-K 13
26

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.4
11
Electrical Conductivity: Equal Weight (Specific), % IACS 1.5
59

Otherwise Unclassified Properties

Base Metal Price, % relative 60
12
Density, g/cm3 8.4
1.7
Embodied Carbon, kg CO2/kg material 10
22
Embodied Energy, MJ/kg 150
160
Embodied Water, L/kg 260
990

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 160
5.0 to 15
Resilience: Unit (Modulus of Resilience), kJ/m3 1380
180 to 320
Stiffness to Weight: Axial, points 13
15
Stiffness to Weight: Bending, points 23
69
Strength to Weight: Axial, points 37
31 to 43
Strength to Weight: Bending, points 28
43 to 53
Thermal Diffusivity, mm2/s 3.1
44
Thermal Shock Resistance, points 33
11 to 16

Alloy Composition

Aluminum (Al), % 0.4 to 1.0
8.3 to 9.7
Carbon (C), % 0 to 0.080
0
Chromium (Cr), % 14 to 17
0
Cobalt (Co), % 0 to 1.0
0
Copper (Cu), % 0 to 0.5
0 to 0.030
Iron (Fe), % 5.0 to 9.0
0 to 0.0050
Magnesium (Mg), % 0
88.6 to 91.3
Manganese (Mn), % 0 to 1.0
0.1 to 0.5
Nickel (Ni), % 65.9 to 77.7
0 to 0.0020
Niobium (Nb), % 0.7 to 1.2
0
Phosphorus (P), % 0 to 0.020
0
Silicon (Si), % 0 to 0.5
0 to 0.2
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 2.3 to 2.8
0
Zinc (Zn), % 0
0.35 to 1.0
Residuals, % 0
0 to 0.010