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EN 2.4856 Nickel vs. 6066 Aluminum

EN 2.4856 nickel belongs to the nickel alloys classification, while 6066 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 6066 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
70
Elongation at Break, % 28
7.8 to 17
Fatigue Strength, MPa 280
94 to 130
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 79
26
Shear Strength, MPa 570
95 to 240
Tensile Strength: Ultimate (UTS), MPa 880
160 to 400
Tensile Strength: Yield (Proof), MPa 430
93 to 360

Thermal Properties

Latent Heat of Fusion, J/g 330
410
Maximum Temperature: Mechanical, °C 1000
170
Melting Completion (Liquidus), °C 1480
650
Melting Onset (Solidus), °C 1430
560
Specific Heat Capacity, J/kg-K 440
890
Thermal Conductivity, W/m-K 10
150
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
2.8
Embodied Carbon, kg CO2/kg material 14
8.3
Embodied Energy, MJ/kg 190
150
Embodied Water, L/kg 290
1160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 200
23 to 52
Resilience: Unit (Modulus of Resilience), kJ/m3 440
61 to 920
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 23
49
Strength to Weight: Axial, points 28
16 to 39
Strength to Weight: Bending, points 24
23 to 43
Thermal Diffusivity, mm2/s 2.7
61
Thermal Shock Resistance, points 29
6.9 to 17

Alloy Composition

Aluminum (Al), % 0 to 0.4
93 to 97
Carbon (C), % 0.030 to 0.1
0
Chromium (Cr), % 20 to 23
0 to 0.4
Cobalt (Co), % 0 to 1.0
0
Copper (Cu), % 0 to 0.5
0.7 to 1.2
Iron (Fe), % 0 to 5.0
0 to 0.5
Magnesium (Mg), % 0
0.8 to 1.4
Manganese (Mn), % 0 to 0.5
0.6 to 1.1
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 1.8
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0 to 0.4
0 to 0.2
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0
0 to 0.15