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5086 Aluminum vs. EN 2.4642 Nickel

5086 aluminum belongs to the aluminum alloys classification, while EN 2.4642 nickel belongs to the nickel alloys. There are 30 material properties with values for both materials. Properties with values for just one material (3, 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 5086 aluminum and the bottom bar is EN 2.4642 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
200
Elongation at Break, % 1.7 to 20
34
Fatigue Strength, MPa 88 to 180
200
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
78
Shear Strength, MPa 160 to 230
450
Tensile Strength: Ultimate (UTS), MPa 270 to 390
670
Tensile Strength: Yield (Proof), MPa 110 to 320
270

Thermal Properties

Latent Heat of Fusion, J/g 400
320
Maximum Temperature: Mechanical, °C 190
1010
Melting Completion (Liquidus), °C 640
1360
Melting Onset (Solidus), °C 590
1320
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 130
12
Thermal Expansion, µm/m-K 24
14

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 31
1.5
Electrical Conductivity: Equal Weight (Specific), % IACS 100
1.6

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
50
Density, g/cm3 2.7
8.3
Embodied Carbon, kg CO2/kg material 8.8
8.2
Embodied Energy, MJ/kg 150
120
Embodied Water, L/kg 1180
290

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 5.8 to 42
180
Resilience: Unit (Modulus of Resilience), kJ/m3 86 to 770
180
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 28 to 40
23
Strength to Weight: Bending, points 34 to 44
21
Thermal Diffusivity, mm2/s 52
3.1
Thermal Shock Resistance, points 12 to 17
18

Alloy Composition

Aluminum (Al), % 93 to 96.3
0 to 0.5
Carbon (C), % 0
0 to 0.050
Chromium (Cr), % 0.050 to 0.25
27 to 31
Copper (Cu), % 0 to 0.1
0 to 0.5
Iron (Fe), % 0 to 0.5
7.0 to 11
Magnesium (Mg), % 3.5 to 4.5
0
Manganese (Mn), % 0.2 to 0.7
0 to 0.5
Nickel (Ni), % 0
55.9 to 66
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0 to 0.4
0 to 0.5
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.15
0
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0