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AZ91E Magnesium vs. EN 2.4668 Nickel

AZ91E magnesium belongs to the magnesium alloys classification, while EN 2.4668 nickel belongs to the nickel alloys. There are 31 material properties with values for both materials. Properties with values for just one material (4, 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 AZ91E magnesium and the bottom bar is EN 2.4668 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
190
Elongation at Break, % 2.5 to 6.2
14
Fatigue Strength, MPa 81 to 85
590
Impact Strength: V-Notched Charpy, J 0.79 to 2.8
14
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 18
75
Shear Strength, MPa 89 to 150
840
Tensile Strength: Ultimate (UTS), MPa 160 to 260
1390
Tensile Strength: Yield (Proof), MPa 96 to 130
1160

Thermal Properties

Latent Heat of Fusion, J/g 350
310
Maximum Temperature: Mechanical, °C 130
980
Melting Completion (Liquidus), °C 600
1460
Melting Onset (Solidus), °C 500
1410
Specific Heat Capacity, J/kg-K 990
450
Thermal Conductivity, W/m-K 84
13
Thermal Expansion, µm/m-K 27
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 10 to 12
1.4
Electrical Conductivity: Equal Weight (Specific), % IACS 52 to 60
1.5

Otherwise Unclassified Properties

Base Metal Price, % relative 12
75
Density, g/cm3 1.7
8.3
Embodied Carbon, kg CO2/kg material 22
13
Embodied Energy, MJ/kg 160
190
Embodied Water, L/kg 990
250

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 3.4 to 12
180
Resilience: Unit (Modulus of Resilience), kJ/m3 100 to 190
3490
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 69
23
Strength to Weight: Axial, points 25 to 42
46
Strength to Weight: Bending, points 37 to 53
33
Thermal Diffusivity, mm2/s 49
3.5
Thermal Shock Resistance, points 9.0 to 15
40

Alloy Composition

Aluminum (Al), % 8.1 to 9.3
0.3 to 0.7
Boron (B), % 0
0.0020 to 0.0060
Carbon (C), % 0
0.020 to 0.080
Chromium (Cr), % 0
17 to 21
Cobalt (Co), % 0
0 to 1.0
Copper (Cu), % 0 to 0.015
0 to 0.3
Iron (Fe), % 0 to 0.0050
11.2 to 24.6
Magnesium (Mg), % 88.8 to 91.3
0
Manganese (Mn), % 0.17 to 0.35
0 to 0.35
Molybdenum (Mo), % 0
2.8 to 3.3
Nickel (Ni), % 0 to 0.0010
50 to 55
Niobium (Nb), % 0
4.7 to 5.5
Phosphorus (P), % 0
0 to 0.015
Silicon (Si), % 0 to 0.2
0 to 0.35
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0
0.6 to 1.2
Zinc (Zn), % 0.4 to 1.0
0
Residuals, % 0 to 0.3
0