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EN 2.4663 Nickel vs. 1050 Aluminum

EN 2.4663 nickel belongs to the nickel alloys classification, while 1050 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 2.4663 nickel and the bottom bar is 1050 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 210
68
Elongation at Break, % 40
4.6 to 37
Fatigue Strength, MPa 250
31 to 57
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 81
26
Shear Strength, MPa 540
52 to 81
Tensile Strength: Ultimate (UTS), MPa 780
76 to 140
Tensile Strength: Yield (Proof), MPa 310
25 to 120

Thermal Properties

Latent Heat of Fusion, J/g 320
400
Maximum Temperature: Mechanical, °C 1010
170
Melting Completion (Liquidus), °C 1430
640
Melting Onset (Solidus), °C 1380
650
Specific Heat Capacity, J/kg-K 450
900
Thermal Conductivity, W/m-K 13
230
Thermal Expansion, µm/m-K 12
24

Electrical Properties

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

Otherwise Unclassified Properties

Base Metal Price, % relative 75
9.5
Density, g/cm3 8.6
2.7
Embodied Carbon, kg CO2/kg material 11
8.3
Embodied Energy, MJ/kg 140
160
Embodied Water, L/kg 350
1200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 250
5.4 to 22
Resilience: Unit (Modulus of Resilience), kJ/m3 230
4.6 to 110
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 23
50
Strength to Weight: Axial, points 25
7.8 to 14
Strength to Weight: Bending, points 22
15 to 22
Thermal Diffusivity, mm2/s 3.5
94
Thermal Shock Resistance, points 22
3.4 to 6.2

Alloy Composition

Aluminum (Al), % 0.7 to 1.4
99.5 to 100
Boron (B), % 0 to 0.0060
0
Carbon (C), % 0.050 to 0.1
0
Chromium (Cr), % 20 to 23
0
Cobalt (Co), % 11 to 14
0
Copper (Cu), % 0 to 0.5
0 to 0.050
Iron (Fe), % 0 to 2.0
0 to 0.4
Magnesium (Mg), % 0
0 to 0.050
Manganese (Mn), % 0 to 0.2
0 to 0.050
Molybdenum (Mo), % 8.5 to 10
0
Nickel (Ni), % 48 to 59.6
0
Phosphorus (P), % 0 to 0.010
0
Silicon (Si), % 0 to 0.2
0 to 0.25
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 0.2 to 0.6
0 to 0.030
Vanadium (V), % 0
0 to 0.050
Zinc (Zn), % 0
0 to 0.050