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1050 Aluminum vs. EN 2.4668 Nickel

1050 aluminum belongs to the aluminum alloys classification, while EN 2.4668 nickel belongs to the nickel 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 1050 aluminum and the bottom bar is EN 2.4668 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
190
Elongation at Break, % 4.6 to 37
14
Fatigue Strength, MPa 31 to 57
590
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
75
Shear Strength, MPa 52 to 81
840
Tensile Strength: Ultimate (UTS), MPa 76 to 140
1390
Tensile Strength: Yield (Proof), MPa 25 to 120
1160

Thermal Properties

Latent Heat of Fusion, J/g 400
310
Maximum Temperature: Mechanical, °C 170
980
Melting Completion (Liquidus), °C 640
1460
Melting Onset (Solidus), °C 650
1410
Specific Heat Capacity, J/kg-K 900
450
Thermal Conductivity, W/m-K 230
13
Thermal Expansion, µm/m-K 24
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 61
1.4
Electrical Conductivity: Equal Weight (Specific), % IACS 200
1.5

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
75
Density, g/cm3 2.7
8.3
Embodied Carbon, kg CO2/kg material 8.3
13
Embodied Energy, MJ/kg 160
190
Embodied Water, L/kg 1200
250

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 5.4 to 22
180
Resilience: Unit (Modulus of Resilience), kJ/m3 4.6 to 110
3490
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
23
Strength to Weight: Axial, points 7.8 to 14
46
Strength to Weight: Bending, points 15 to 22
33
Thermal Diffusivity, mm2/s 94
3.5
Thermal Shock Resistance, points 3.4 to 6.2
40

Alloy Composition

Aluminum (Al), % 99.5 to 100
0.3 to 0.7
Boron (B), % 0
0.0020 to 0.0060
Carbon (C), % 0
0.020 to 0.080
Chromium (Cr), % 0
17 to 21
Cobalt (Co), % 0
0 to 1.0
Copper (Cu), % 0 to 0.050
0 to 0.3
Iron (Fe), % 0 to 0.4
11.2 to 24.6
Magnesium (Mg), % 0 to 0.050
0
Manganese (Mn), % 0 to 0.050
0 to 0.35
Molybdenum (Mo), % 0
2.8 to 3.3
Nickel (Ni), % 0
50 to 55
Niobium (Nb), % 0
4.7 to 5.5
Phosphorus (P), % 0
0 to 0.015
Silicon (Si), % 0 to 0.25
0 to 0.35
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.030
0.6 to 1.2
Vanadium (V), % 0 to 0.050
0
Zinc (Zn), % 0 to 0.050
0