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EN 2.4668 Nickel vs. 6262A Aluminum

EN 2.4668 nickel belongs to the nickel alloys classification, while 6262A 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 6262A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
68
Elongation at Break, % 14
4.5 to 11
Fatigue Strength, MPa 590
94 to 110
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 75
26
Shear Strength, MPa 840
190 to 240
Tensile Strength: Ultimate (UTS), MPa 1390
310 to 410
Tensile Strength: Yield (Proof), MPa 1160
270 to 370

Thermal Properties

Latent Heat of Fusion, J/g 310
400
Maximum Temperature: Mechanical, °C 980
160
Melting Completion (Liquidus), °C 1460
640
Melting Onset (Solidus), °C 1410
580
Specific Heat Capacity, J/kg-K 450
890
Thermal Conductivity, W/m-K 13
170
Thermal Expansion, µm/m-K 13
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.4
45
Electrical Conductivity: Equal Weight (Specific), % IACS 1.5
140

Otherwise Unclassified Properties

Base Metal Price, % relative 75
11
Density, g/cm3 8.3
2.8
Embodied Carbon, kg CO2/kg material 13
8.4
Embodied Energy, MJ/kg 190
150
Embodied Water, L/kg 250
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 180
17 to 34
Resilience: Unit (Modulus of Resilience), kJ/m3 3490
540 to 1000
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 23
49
Strength to Weight: Axial, points 46
31 to 41
Strength to Weight: Bending, points 33
36 to 44
Thermal Diffusivity, mm2/s 3.5
67
Thermal Shock Resistance, points 40
14 to 18

Alloy Composition

Aluminum (Al), % 0.3 to 0.7
94.2 to 97.8
Bismuth (Bi), % 0
0.4 to 0.9
Boron (B), % 0.0020 to 0.0060
0
Carbon (C), % 0.020 to 0.080
0
Chromium (Cr), % 17 to 21
0.040 to 0.14
Cobalt (Co), % 0 to 1.0
0
Copper (Cu), % 0 to 0.3
0.15 to 0.4
Iron (Fe), % 11.2 to 24.6
0 to 0.7
Magnesium (Mg), % 0
0.8 to 1.2
Manganese (Mn), % 0 to 0.35
0 to 0.15
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
0.4 to 0.8
Sulfur (S), % 0 to 0.015
0
Tin (Sn), % 0
0.4 to 1.0
Titanium (Ti), % 0.6 to 1.2
0 to 0.1
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0
0 to 0.15