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EN 2.4856 Nickel vs. 6182 Aluminum

EN 2.4856 nickel belongs to the nickel alloys classification, while 6182 aluminum belongs to the aluminum 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 6182 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
70
Elongation at Break, % 28
6.8 to 13
Fatigue Strength, MPa 280
63 to 99
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 79
26
Shear Strength, MPa 570
140 to 190
Tensile Strength: Ultimate (UTS), MPa 880
230 to 320
Tensile Strength: Yield (Proof), MPa 430
130 to 270

Thermal Properties

Latent Heat of Fusion, J/g 330
410
Maximum Temperature: Mechanical, °C 1000
190
Melting Completion (Liquidus), °C 1480
640
Melting Onset (Solidus), °C 1430
600
Specific Heat Capacity, J/kg-K 440
900
Thermal Conductivity, W/m-K 10
160
Thermal Expansion, µm/m-K 11
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.3
40
Electrical Conductivity: Equal Weight (Specific), % IACS 1.4
130

Otherwise Unclassified Properties

Base Metal Price, % relative 80
9.5
Density, g/cm3 8.6
2.7
Embodied Carbon, kg CO2/kg material 14
8.4
Embodied Energy, MJ/kg 190
150
Embodied Water, L/kg 290
1170

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 200
21 to 26
Resilience: Unit (Modulus of Resilience), kJ/m3 440
110 to 520
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 23
50
Strength to Weight: Axial, points 28
23 to 32
Strength to Weight: Bending, points 24
30 to 38
Thermal Diffusivity, mm2/s 2.7
65
Thermal Shock Resistance, points 29
10 to 14

Alloy Composition

Aluminum (Al), % 0 to 0.4
95 to 97.9
Carbon (C), % 0.030 to 0.1
0
Chromium (Cr), % 20 to 23
0 to 0.25
Cobalt (Co), % 0 to 1.0
0
Copper (Cu), % 0 to 0.5
0 to 0.1
Iron (Fe), % 0 to 5.0
0 to 0.5
Magnesium (Mg), % 0
0.7 to 1.2
Manganese (Mn), % 0 to 0.5
0.5 to 1.0
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
0.9 to 1.3
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0 to 0.4
0 to 0.1
Zinc (Zn), % 0
0 to 0.2
Zirconium (Zr), % 0
0.050 to 0.2
Residuals, % 0
0 to 0.15