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5040 Aluminum vs. EN 2.4665 Nickel

5040 aluminum belongs to the aluminum alloys classification, while EN 2.4665 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 2.4665 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
210
Elongation at Break, % 5.7 to 6.8
34
Fatigue Strength, MPa 100 to 130
220
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
81
Shear Strength, MPa 140 to 150
520
Tensile Strength: Ultimate (UTS), MPa 240 to 260
790
Tensile Strength: Yield (Proof), MPa 190 to 230
300

Thermal Properties

Latent Heat of Fusion, J/g 400
320
Maximum Temperature: Mechanical, °C 190
990
Melting Completion (Liquidus), °C 650
1460
Melting Onset (Solidus), °C 600
1410
Specific Heat Capacity, J/kg-K 900
450
Thermal Conductivity, W/m-K 160
12
Thermal Expansion, µm/m-K 23
14

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 41
1.5
Electrical Conductivity: Equal Weight (Specific), % IACS 130
1.6

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
55
Density, g/cm3 2.8
8.4
Embodied Carbon, kg CO2/kg material 8.3
9.2
Embodied Energy, MJ/kg 150
130
Embodied Water, L/kg 1180
270

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 15
210
Resilience: Unit (Modulus of Resilience), kJ/m3 260 to 380
220
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
23
Strength to Weight: Axial, points 24 to 26
26
Strength to Weight: Bending, points 31 to 32
22
Thermal Diffusivity, mm2/s 64
3.2
Thermal Shock Resistance, points 10 to 11
20

Alloy Composition

Aluminum (Al), % 95.2 to 98
0 to 0.5
Boron (B), % 0
0 to 0.010
Carbon (C), % 0
0.050 to 0.15
Chromium (Cr), % 0.1 to 0.3
20.5 to 23
Cobalt (Co), % 0
0.5 to 2.5
Copper (Cu), % 0 to 0.25
0 to 0.5
Iron (Fe), % 0 to 0.7
17 to 20
Magnesium (Mg), % 1.0 to 1.5
0
Manganese (Mn), % 0.9 to 1.4
0 to 1.0
Molybdenum (Mo), % 0
8.0 to 10
Nickel (Ni), % 0
40.3 to 53.8
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0 to 0.3
0 to 1.0
Sulfur (S), % 0
0 to 0.015
Tungsten (W), % 0
0.2 to 1.0
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0