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EN 2.4663 Nickel vs. 5040 Aluminum

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

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Electrical Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition

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