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EN 2.4665 Nickel vs. 3105 Aluminum

EN 2.4665 nickel belongs to the nickel alloys classification, while 3105 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 2.4665 nickel and the bottom bar is 3105 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 210
69
Elongation at Break, % 34
1.1 to 20
Fatigue Strength, MPa 220
39 to 95
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 81
26
Shear Strength, MPa 520
77 to 140
Tensile Strength: Ultimate (UTS), MPa 790
120 to 240
Tensile Strength: Yield (Proof), MPa 300
46 to 220

Thermal Properties

Latent Heat of Fusion, J/g 320
400
Maximum Temperature: Mechanical, °C 990
180
Melting Completion (Liquidus), °C 1460
660
Melting Onset (Solidus), °C 1410
640
Specific Heat Capacity, J/kg-K 450
900
Thermal Conductivity, W/m-K 12
170
Thermal Expansion, µm/m-K 14
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.5
44
Electrical Conductivity: Equal Weight (Specific), % IACS 1.6
140

Otherwise Unclassified Properties

Base Metal Price, % relative 55
9.5
Density, g/cm3 8.4
2.8
Embodied Carbon, kg CO2/kg material 9.2
8.2
Embodied Energy, MJ/kg 130
150
Embodied Water, L/kg 270
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 210
2.6 to 19
Resilience: Unit (Modulus of Resilience), kJ/m3 220
15 to 340
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 23
50
Strength to Weight: Axial, points 26
12 to 24
Strength to Weight: Bending, points 22
20 to 31
Thermal Diffusivity, mm2/s 3.2
68
Thermal Shock Resistance, points 20
5.2 to 11

Alloy Composition

Aluminum (Al), % 0 to 0.5
96 to 99.5
Boron (B), % 0 to 0.010
0
Carbon (C), % 0.050 to 0.15
0
Chromium (Cr), % 20.5 to 23
0 to 0.2
Cobalt (Co), % 0.5 to 2.5
0
Copper (Cu), % 0 to 0.5
0 to 0.3
Iron (Fe), % 17 to 20
0 to 0.7
Magnesium (Mg), % 0
0.2 to 0.8
Manganese (Mn), % 0 to 1.0
0.3 to 0.8
Molybdenum (Mo), % 8.0 to 10
0
Nickel (Ni), % 40.3 to 53.8
0
Phosphorus (P), % 0 to 0.020
0
Silicon (Si), % 0 to 1.0
0 to 0.6
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0
0 to 0.1
Tungsten (W), % 0.2 to 1.0
0
Zinc (Zn), % 0
0 to 0.4
Residuals, % 0
0 to 0.15