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ISO-WD32260 Magnesium vs. EN 2.4856 Nickel

ISO-WD32260 magnesium belongs to the magnesium alloys classification, while EN 2.4856 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 ISO-WD32260 magnesium and the bottom bar is EN 2.4856 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
200
Elongation at Break, % 4.5 to 6.0
28
Fatigue Strength, MPa 150 to 190
280
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 18
79
Shear Strength, MPa 190 to 200
570
Tensile Strength: Ultimate (UTS), MPa 330 to 340
880
Tensile Strength: Yield (Proof), MPa 230 to 250
430

Thermal Properties

Latent Heat of Fusion, J/g 330
330
Maximum Temperature: Mechanical, °C 120
1000
Melting Completion (Liquidus), °C 600
1480
Melting Onset (Solidus), °C 520
1430
Specific Heat Capacity, J/kg-K 970
440
Thermal Conductivity, W/m-K 110
10
Thermal Expansion, µm/m-K 27
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 28
1.3
Electrical Conductivity: Equal Weight (Specific), % IACS 140
1.4

Otherwise Unclassified Properties

Base Metal Price, % relative 13
80
Density, g/cm3 1.9
8.6
Embodied Carbon, kg CO2/kg material 23
14
Embodied Energy, MJ/kg 160
190
Embodied Water, L/kg 940
290

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 19
200
Resilience: Unit (Modulus of Resilience), kJ/m3 560 to 700
440
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 63
23
Strength to Weight: Axial, points 48 to 51
28
Strength to Weight: Bending, points 56 to 58
24
Thermal Diffusivity, mm2/s 63
2.7
Thermal Shock Resistance, points 19 to 20
29

Alloy Composition


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Aluminum (Al), % 0
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
0 to 0.5
Iron (Fe), % 0
0 to 5.0
Magnesium (Mg), % 92.7 to 94.8
0
Manganese (Mn), % 0
0 to 0.5
Molybdenum (Mo), % 0
8.0 to 10
Nickel (Ni), % 0
58 to 68.8
Niobium (Nb), % 0
3.2 to 4.2
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0
0 to 0.5
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0
0 to 0.4
Zinc (Zn), % 4.8 to 6.2
0
Zirconium (Zr), % 0.45 to 0.8
0
Residuals, % 0 to 0.3
0