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EN 2.4856 Nickel vs. 5449 Aluminum

EN 2.4856 nickel belongs to the nickel alloys classification, while 5449 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 2.4856 nickel and the bottom bar is 5449 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
69
Elongation at Break, % 28
4.0 to 17
Fatigue Strength, MPa 280
78 to 120
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 79
26
Shear Strength, MPa 570
130 to 190
Tensile Strength: Ultimate (UTS), MPa 880
210 to 330
Tensile Strength: Yield (Proof), MPa 430
91 to 260

Thermal Properties

Latent Heat of Fusion, J/g 330
400
Maximum Temperature: Mechanical, °C 1000
190
Melting Completion (Liquidus), °C 1480
650
Melting Onset (Solidus), °C 1430
590
Specific Heat Capacity, J/kg-K 440
900
Thermal Conductivity, W/m-K 10
140
Thermal Expansion, µm/m-K 11
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.3
35
Electrical Conductivity: Equal Weight (Specific), % IACS 1.4
110

Otherwise Unclassified Properties

Base Metal Price, % relative 80
9.5
Density, g/cm3 8.6
2.8
Embodied Carbon, kg CO2/kg material 14
8.5
Embodied Energy, MJ/kg 190
150
Embodied Water, L/kg 290
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 200
12 to 29
Resilience: Unit (Modulus of Resilience), kJ/m3 440
60 to 480
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 23
50
Strength to Weight: Axial, points 28
22 to 33
Strength to Weight: Bending, points 24
29 to 39
Thermal Diffusivity, mm2/s 2.7
56
Thermal Shock Resistance, points 29
9.4 to 15

Alloy Composition

Aluminum (Al), % 0 to 0.4
94.1 to 97.8
Carbon (C), % 0.030 to 0.1
0
Chromium (Cr), % 20 to 23
0 to 0.3
Cobalt (Co), % 0 to 1.0
0
Copper (Cu), % 0 to 0.5
0 to 0.3
Iron (Fe), % 0 to 5.0
0 to 0.7
Magnesium (Mg), % 0
1.6 to 2.6
Manganese (Mn), % 0 to 0.5
0.6 to 1.1
Molybdenum (Mo), % 8.0 to 10
0
Nickel (Ni), % 58 to 68.8
0
Niobium (Nb), % 3.2 to 4.2
0
Phosphorus (P), % 0 to 0.020
0
Silicon (Si), % 0 to 0.5
0 to 0.4
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0 to 0.4
0 to 0.1
Zinc (Zn), % 0
0 to 0.3
Residuals, % 0
0 to 0.15