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EN 2.4650 Nickel vs. A360.0 Aluminum

EN 2.4650 nickel belongs to the nickel alloys classification, while A360.0 aluminum belongs to the aluminum alloys. There are 30 material properties with values for both materials. Properties with values for just one material (2, 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 2.4650 nickel and the bottom bar is A360.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 210
72
Elongation at Break, % 34
1.6 to 5.0
Fatigue Strength, MPa 480
82 to 150
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 80
27
Shear Strength, MPa 730
180
Tensile Strength: Ultimate (UTS), MPa 1090
180 to 320
Tensile Strength: Yield (Proof), MPa 650
170 to 260

Thermal Properties

Latent Heat of Fusion, J/g 320
530
Maximum Temperature: Mechanical, °C 1010
170
Melting Completion (Liquidus), °C 1400
680
Melting Onset (Solidus), °C 1350
590
Specific Heat Capacity, J/kg-K 450
900
Thermal Conductivity, W/m-K 12
110
Thermal Expansion, µm/m-K 11
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.5
30
Electrical Conductivity: Equal Weight (Specific), % IACS 1.6
100

Otherwise Unclassified Properties

Base Metal Price, % relative 80
9.5
Density, g/cm3 8.5
2.6
Embodied Carbon, kg CO2/kg material 10
7.8
Embodied Energy, MJ/kg 140
150
Embodied Water, L/kg 360
1070

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 320
4.6 to 13
Resilience: Unit (Modulus of Resilience), kJ/m3 1030
190 to 470
Stiffness to Weight: Axial, points 13
15
Stiffness to Weight: Bending, points 23
53
Strength to Weight: Axial, points 36
19 to 34
Strength to Weight: Bending, points 28
27 to 39
Thermal Diffusivity, mm2/s 3.1
48
Thermal Shock Resistance, points 33
8.5 to 15

Alloy Composition

Aluminum (Al), % 0.3 to 0.6
85.8 to 90.6
Boron (B), % 0 to 0.0050
0
Carbon (C), % 0.040 to 0.080
0
Chromium (Cr), % 19 to 21
0
Cobalt (Co), % 19 to 21
0
Copper (Cu), % 0 to 0.2
0 to 0.6
Iron (Fe), % 0 to 0.7
0 to 1.3
Magnesium (Mg), % 0
0.4 to 0.6
Manganese (Mn), % 0 to 0.6
0 to 0.35
Molybdenum (Mo), % 5.6 to 6.1
0
Nickel (Ni), % 46.9 to 54.2
0 to 0.5
Phosphorus (P), % 0 to 0.020
0
Silicon (Si), % 0 to 0.4
9.0 to 10
Sulfur (S), % 0 to 0.0070
0
Tin (Sn), % 0
0 to 0.15
Titanium (Ti), % 1.9 to 2.4
0
Zinc (Zn), % 0
0 to 0.5
Residuals, % 0
0 to 0.25