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EN 2.4856 Nickel vs. ISO-WD32260 Magnesium

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

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Electrical Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition

Aluminum (Al), % 0 to 0.4
0
Carbon (C), % 0.030 to 0.1
0
Chromium (Cr), % 20 to 23
0
Cobalt (Co), % 0 to 1.0
0
Copper (Cu), % 0 to 0.5
0
Iron (Fe), % 0 to 5.0
0
Magnesium (Mg), % 0
92.7 to 94.8
Manganese (Mn), % 0 to 0.5
0
Molybdenum (Mo), % 8.0 to 10
0
Nickel (Ni), % 58 to 68.8
0
Niobium (Nb), % 3.2 to 4.2
0
Phosphorus (P), % 0 to 0.020
0
Silicon (Si), % 0 to 0.5
0
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0 to 0.4
0
Zinc (Zn), % 0
4.8 to 6.2
Zirconium (Zr), % 0
0.45 to 0.8
Residuals, % 0
0 to 0.3