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EN 2.4650 Nickel vs. 1050A Aluminum

EN 2.4650 nickel belongs to the nickel alloys classification, while 1050A 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 2.4650 nickel and the bottom bar is 1050A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 210
68
Elongation at Break, % 34
1.1 to 33
Fatigue Strength, MPa 480
22 to 55
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 80
26
Shear Strength, MPa 730
44 to 97
Tensile Strength: Ultimate (UTS), MPa 1090
68 to 170
Tensile Strength: Yield (Proof), MPa 650
22 to 150

Thermal Properties

Latent Heat of Fusion, J/g 320
400
Maximum Temperature: Mechanical, °C 1010
170
Melting Completion (Liquidus), °C 1400
660
Melting Onset (Solidus), °C 1350
650
Specific Heat Capacity, J/kg-K 450
900
Thermal Conductivity, W/m-K 12
230
Thermal Expansion, µm/m-K 11
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.5
59
Electrical Conductivity: Equal Weight (Specific), % IACS 1.6
200

Otherwise Unclassified Properties

Base Metal Price, % relative 80
9.0
Density, g/cm3 8.5
2.7
Embodied Carbon, kg CO2/kg material 10
8.2
Embodied Energy, MJ/kg 140
150
Embodied Water, L/kg 360
1200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 320
1.9 to 19
Resilience: Unit (Modulus of Resilience), kJ/m3 1030
3.7 to 160
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 23
50
Strength to Weight: Axial, points 36
6.9 to 18
Strength to Weight: Bending, points 28
14 to 25
Thermal Diffusivity, mm2/s 3.1
94
Thermal Shock Resistance, points 33
3.0 to 7.6

Alloy Composition

Aluminum (Al), % 0.3 to 0.6
99.5 to 100
Boron (B), % 0 to 0.0050
0
Carbon (C), % 0.040 to 0.080
0
Chromium (Cr), % 19 to 21
0
Cobalt (Co), % 19 to 21
0
Copper (Cu), % 0 to 0.2
0 to 0.050
Iron (Fe), % 0 to 0.7
0 to 0.4
Magnesium (Mg), % 0
0 to 0.050
Manganese (Mn), % 0 to 0.6
0 to 0.050
Molybdenum (Mo), % 5.6 to 6.1
0
Nickel (Ni), % 46.9 to 54.2
0
Phosphorus (P), % 0 to 0.020
0
Silicon (Si), % 0 to 0.4
0 to 0.25
Sulfur (S), % 0 to 0.0070
0
Titanium (Ti), % 1.9 to 2.4
0 to 0.050
Zinc (Zn), % 0
0 to 0.070