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5040 Aluminum vs. EN 2.4663 Nickel

5040 aluminum belongs to the aluminum alloys classification, while EN 2.4663 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 5040 aluminum and the bottom bar is EN 2.4663 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
210
Elongation at Break, % 5.7 to 6.8
40
Fatigue Strength, MPa 100 to 130
250
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
81
Shear Strength, MPa 140 to 150
540
Tensile Strength: Ultimate (UTS), MPa 240 to 260
780
Tensile Strength: Yield (Proof), MPa 190 to 230
310

Thermal Properties

Latent Heat of Fusion, J/g 400
320
Maximum Temperature: Mechanical, °C 190
1010
Melting Completion (Liquidus), °C 650
1430
Melting Onset (Solidus), °C 600
1380
Specific Heat Capacity, J/kg-K 900
450
Thermal Conductivity, W/m-K 160
13
Thermal Expansion, µm/m-K 23
12

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 41
1.4
Electrical Conductivity: Equal Weight (Specific), % IACS 130
1.5

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
75
Density, g/cm3 2.8
8.6
Embodied Carbon, kg CO2/kg material 8.3
11
Embodied Energy, MJ/kg 150
140
Embodied Water, L/kg 1180
350

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 15
250
Resilience: Unit (Modulus of Resilience), kJ/m3 260 to 380
230
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
23
Strength to Weight: Axial, points 24 to 26
25
Strength to Weight: Bending, points 31 to 32
22
Thermal Diffusivity, mm2/s 64
3.5
Thermal Shock Resistance, points 10 to 11
22

Alloy Composition

Aluminum (Al), % 95.2 to 98
0.7 to 1.4
Boron (B), % 0
0 to 0.0060
Carbon (C), % 0
0.050 to 0.1
Chromium (Cr), % 0.1 to 0.3
20 to 23
Cobalt (Co), % 0
11 to 14
Copper (Cu), % 0 to 0.25
0 to 0.5
Iron (Fe), % 0 to 0.7
0 to 2.0
Magnesium (Mg), % 1.0 to 1.5
0
Manganese (Mn), % 0.9 to 1.4
0 to 0.2
Molybdenum (Mo), % 0
8.5 to 10
Nickel (Ni), % 0
48 to 59.6
Phosphorus (P), % 0
0 to 0.010
Silicon (Si), % 0 to 0.3
0 to 0.2
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0
0.2 to 0.6
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0