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1050A Aluminum vs. EN 2.4608 Nickel

1050A aluminum belongs to the aluminum alloys classification, while EN 2.4608 nickel belongs to the nickel 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 1050A aluminum and the bottom bar is EN 2.4608 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
210
Elongation at Break, % 1.1 to 33
34
Fatigue Strength, MPa 22 to 55
200
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
81
Shear Strength, MPa 44 to 97
410
Tensile Strength: Ultimate (UTS), MPa 68 to 170
620
Tensile Strength: Yield (Proof), MPa 22 to 150
270

Thermal Properties

Latent Heat of Fusion, J/g 400
330
Maximum Temperature: Mechanical, °C 170
1000
Melting Completion (Liquidus), °C 660
1460
Melting Onset (Solidus), °C 650
1410
Specific Heat Capacity, J/kg-K 900
460
Thermal Conductivity, W/m-K 230
11
Thermal Expansion, µm/m-K 24
13

Electrical Properties

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

Otherwise Unclassified Properties

Base Metal Price, % relative 9.0
55
Density, g/cm3 2.7
8.5
Embodied Carbon, kg CO2/kg material 8.2
8.4
Embodied Energy, MJ/kg 150
120
Embodied Water, L/kg 1200
270

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 1.9 to 19
170
Resilience: Unit (Modulus of Resilience), kJ/m3 3.7 to 160
180
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
23
Strength to Weight: Axial, points 6.9 to 18
20
Strength to Weight: Bending, points 14 to 25
19
Thermal Diffusivity, mm2/s 94
2.9
Thermal Shock Resistance, points 3.0 to 7.6
16

Alloy Composition

Aluminum (Al), % 99.5 to 100
0
Carbon (C), % 0
0.030 to 0.080
Chromium (Cr), % 0
24 to 26
Cobalt (Co), % 0
2.5 to 4.0
Copper (Cu), % 0 to 0.050
0
Iron (Fe), % 0 to 0.4
11.4 to 23.8
Magnesium (Mg), % 0 to 0.050
0
Manganese (Mn), % 0 to 0.050
0 to 2.0
Molybdenum (Mo), % 0
2.5 to 4.0
Nickel (Ni), % 0
44 to 47
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0 to 0.25
0.7 to 1.5
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.050
0
Tungsten (W), % 0
2.5 to 4.0
Zinc (Zn), % 0 to 0.070
0