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EN 2.4668 Nickel vs. 2007 Aluminum

EN 2.4668 nickel belongs to the nickel alloys classification, while 2007 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 2.4668 nickel and the bottom bar is 2007 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
71
Elongation at Break, % 14
5.6 to 8.0
Fatigue Strength, MPa 590
91 to 110
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 75
27
Shear Strength, MPa 840
220 to 250
Tensile Strength: Ultimate (UTS), MPa 1390
370 to 420
Tensile Strength: Yield (Proof), MPa 1160
240 to 270

Thermal Properties

Latent Heat of Fusion, J/g 310
390
Maximum Temperature: Mechanical, °C 980
190
Melting Completion (Liquidus), °C 1460
640
Melting Onset (Solidus), °C 1410
510
Specific Heat Capacity, J/kg-K 450
870
Thermal Conductivity, W/m-K 13
130
Thermal Expansion, µm/m-K 13
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.4
47
Electrical Conductivity: Equal Weight (Specific), % IACS 1.5
140

Otherwise Unclassified Properties

Base Metal Price, % relative 75
11
Density, g/cm3 8.3
3.1
Embodied Carbon, kg CO2/kg material 13
8.0
Embodied Energy, MJ/kg 190
150
Embodied Water, L/kg 250
1130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 180
21 to 26
Resilience: Unit (Modulus of Resilience), kJ/m3 3490
390 to 530
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 23
44
Strength to Weight: Axial, points 46
33 to 38
Strength to Weight: Bending, points 33
37 to 40
Thermal Diffusivity, mm2/s 3.5
48
Thermal Shock Resistance, points 40
16 to 19

Alloy Composition

Aluminum (Al), % 0.3 to 0.7
87.5 to 95
Bismuth (Bi), % 0
0 to 0.2
Boron (B), % 0.0020 to 0.0060
0
Carbon (C), % 0.020 to 0.080
0
Chromium (Cr), % 17 to 21
0 to 0.1
Cobalt (Co), % 0 to 1.0
0
Copper (Cu), % 0 to 0.3
3.3 to 4.6
Iron (Fe), % 11.2 to 24.6
0 to 0.8
Lead (Pb), % 0
0.8 to 1.5
Magnesium (Mg), % 0
0.4 to 1.8
Manganese (Mn), % 0 to 0.35
0.5 to 1.0
Molybdenum (Mo), % 2.8 to 3.3
0
Nickel (Ni), % 50 to 55
0 to 0.2
Niobium (Nb), % 4.7 to 5.5
0
Phosphorus (P), % 0 to 0.015
0
Silicon (Si), % 0 to 0.35
0 to 0.8
Sulfur (S), % 0 to 0.015
0
Tin (Sn), % 0
0 to 0.2
Titanium (Ti), % 0.6 to 1.2
0 to 0.2
Zinc (Zn), % 0
0 to 0.8
Residuals, % 0
0 to 0.3