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EN 2.4856 Nickel vs. 7010 Aluminum

EN 2.4856 nickel belongs to the nickel alloys classification, while 7010 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 7010 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
70
Elongation at Break, % 28
3.9 to 6.8
Fatigue Strength, MPa 280
160 to 190
Poisson's Ratio 0.29
0.32
Shear Modulus, GPa 79
26
Shear Strength, MPa 570
300 to 340
Tensile Strength: Ultimate (UTS), MPa 880
520 to 590
Tensile Strength: Yield (Proof), MPa 430
410 to 540

Thermal Properties

Latent Heat of Fusion, J/g 330
380
Maximum Temperature: Mechanical, °C 1000
200
Melting Completion (Liquidus), °C 1480
630
Melting Onset (Solidus), °C 1430
480
Specific Heat Capacity, J/kg-K 440
860
Thermal Conductivity, W/m-K 10
150
Thermal Expansion, µm/m-K 11
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.3
40
Electrical Conductivity: Equal Weight (Specific), % IACS 1.4
120

Otherwise Unclassified Properties

Base Metal Price, % relative 80
10
Density, g/cm3 8.6
3.0
Embodied Carbon, kg CO2/kg material 14
8.3
Embodied Energy, MJ/kg 190
150
Embodied Water, L/kg 290
1120

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 200
22 to 33
Resilience: Unit (Modulus of Resilience), kJ/m3 440
1230 to 2130
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 23
45
Strength to Weight: Axial, points 28
47 to 54
Strength to Weight: Bending, points 24
47 to 52
Thermal Diffusivity, mm2/s 2.7
58
Thermal Shock Resistance, points 29
22 to 26

Alloy Composition

Aluminum (Al), % 0 to 0.4
87.9 to 90.6
Carbon (C), % 0.030 to 0.1
0
Chromium (Cr), % 20 to 23
0 to 0.050
Cobalt (Co), % 0 to 1.0
0
Copper (Cu), % 0 to 0.5
1.5 to 2.0
Iron (Fe), % 0 to 5.0
0 to 0.15
Magnesium (Mg), % 0
2.1 to 2.6
Manganese (Mn), % 0 to 0.5
0 to 0.1
Molybdenum (Mo), % 8.0 to 10
0
Nickel (Ni), % 58 to 68.8
0 to 0.050
Niobium (Nb), % 3.2 to 4.2
0
Phosphorus (P), % 0 to 0.020
0
Silicon (Si), % 0 to 0.5
0 to 0.12
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0 to 0.4
0 to 0.060
Zinc (Zn), % 0
5.7 to 6.7
Zirconium (Zr), % 0
0.1 to 0.16
Residuals, % 0
0 to 0.15