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EN 2.4668 Nickel vs. 5383 Aluminum

EN 2.4668 nickel belongs to the nickel alloys classification, while 5383 aluminum belongs to the aluminum 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 EN 2.4668 nickel and the bottom bar is 5383 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
68
Elongation at Break, % 14
6.7 to 15
Fatigue Strength, MPa 590
130 to 200
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 75
26
Shear Strength, MPa 840
190 to 220
Tensile Strength: Ultimate (UTS), MPa 1390
310 to 370
Tensile Strength: Yield (Proof), MPa 1160
150 to 310

Thermal Properties

Latent Heat of Fusion, J/g 310
390
Maximum Temperature: Mechanical, °C 980
200
Melting Completion (Liquidus), °C 1460
650
Melting Onset (Solidus), °C 1410
540
Specific Heat Capacity, J/kg-K 450
900
Thermal Conductivity, W/m-K 13
130
Thermal Expansion, µm/m-K 13
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.4
29
Electrical Conductivity: Equal Weight (Specific), % IACS 1.5
97

Otherwise Unclassified Properties

Base Metal Price, % relative 75
9.5
Density, g/cm3 8.3
2.7
Embodied Carbon, kg CO2/kg material 13
9.0
Embodied Energy, MJ/kg 190
160
Embodied Water, L/kg 250
1170

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 180
23 to 40
Resilience: Unit (Modulus of Resilience), kJ/m3 3490
170 to 690
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 23
50
Strength to Weight: Axial, points 46
32 to 38
Strength to Weight: Bending, points 33
38 to 42
Thermal Diffusivity, mm2/s 3.5
51
Thermal Shock Resistance, points 40
14 to 16

Alloy Composition

Aluminum (Al), % 0.3 to 0.7
92 to 95.3
Boron (B), % 0.0020 to 0.0060
0
Carbon (C), % 0.020 to 0.080
0
Chromium (Cr), % 17 to 21
0 to 0.25
Cobalt (Co), % 0 to 1.0
0
Copper (Cu), % 0 to 0.3
0 to 0.2
Iron (Fe), % 11.2 to 24.6
0 to 0.25
Magnesium (Mg), % 0
4.0 to 5.2
Manganese (Mn), % 0 to 0.35
0.7 to 1.0
Molybdenum (Mo), % 2.8 to 3.3
0
Nickel (Ni), % 50 to 55
0
Niobium (Nb), % 4.7 to 5.5
0
Phosphorus (P), % 0 to 0.015
0
Silicon (Si), % 0 to 0.35
0 to 0.25
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0.6 to 1.2
0 to 0.15
Zinc (Zn), % 0
0 to 0.4
Zirconium (Zr), % 0
0 to 0.2
Residuals, % 0
0 to 0.15