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AZ91E Magnesium vs. EN 2.4856 Nickel

AZ91E magnesium belongs to the magnesium alloys classification, while EN 2.4856 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 2.4856 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 75
210
Elastic (Young's, Tensile) Modulus, GPa 46
200
Elongation at Break, % 2.5 to 6.2
28
Fatigue Strength, MPa 81 to 85
280
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 18
79
Shear Strength, MPa 89 to 150
570
Tensile Strength: Ultimate (UTS), MPa 160 to 260
880
Tensile Strength: Yield (Proof), MPa 96 to 130
430

Thermal Properties

Latent Heat of Fusion, J/g 350
330
Maximum Temperature: Mechanical, °C 130
1000
Melting Completion (Liquidus), °C 600
1480
Melting Onset (Solidus), °C 500
1430
Specific Heat Capacity, J/kg-K 990
440
Thermal Conductivity, W/m-K 84
10
Thermal Expansion, µm/m-K 27
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 10 to 12
1.3
Electrical Conductivity: Equal Weight (Specific), % IACS 52 to 60
1.4

Otherwise Unclassified Properties

Base Metal Price, % relative 12
80
Density, g/cm3 1.7
8.6
Embodied Carbon, kg CO2/kg material 22
14
Embodied Energy, MJ/kg 160
190
Embodied Water, L/kg 990
290

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 3.4 to 12
200
Resilience: Unit (Modulus of Resilience), kJ/m3 100 to 190
440
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 69
23
Strength to Weight: Axial, points 25 to 42
28
Strength to Weight: Bending, points 37 to 53
24
Thermal Diffusivity, mm2/s 49
2.7
Thermal Shock Resistance, points 9.0 to 15
29

Alloy Composition


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Aluminum (Al), % 8.1 to 9.3
0 to 0.4
Carbon (C), % 0
0.030 to 0.1
Chromium (Cr), % 0
20 to 23
Cobalt (Co), % 0
0 to 1.0
Copper (Cu), % 0 to 0.015
0 to 0.5
Iron (Fe), % 0 to 0.0050
0 to 5.0
Magnesium (Mg), % 88.8 to 91.3
0
Manganese (Mn), % 0.17 to 0.35
0 to 0.5
Molybdenum (Mo), % 0
8.0 to 10
Nickel (Ni), % 0 to 0.0010
58 to 68.8
Niobium (Nb), % 0
3.2 to 4.2
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0 to 0.2
0 to 0.5
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0
0 to 0.4
Zinc (Zn), % 0.4 to 1.0
0
Residuals, % 0 to 0.3
0