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7050 Aluminum vs. EN 2.4856 Nickel

7050 aluminum belongs to the aluminum alloys classification, while EN 2.4856 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 7050 aluminum and the bottom bar is EN 2.4856 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
200
Elongation at Break, % 2.2 to 12
28
Fatigue Strength, MPa 130 to 210
280
Poisson's Ratio 0.32
0.29
Shear Modulus, GPa 26
79
Shear Strength, MPa 280 to 330
570
Tensile Strength: Ultimate (UTS), MPa 490 to 570
880
Tensile Strength: Yield (Proof), MPa 390 to 500
430

Thermal Properties

Latent Heat of Fusion, J/g 370
330
Maximum Temperature: Mechanical, °C 190
1000
Melting Completion (Liquidus), °C 630
1480
Melting Onset (Solidus), °C 490
1430
Specific Heat Capacity, J/kg-K 860
440
Thermal Conductivity, W/m-K 140
10
Thermal Expansion, µm/m-K 24
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
1.3
Electrical Conductivity: Equal Weight (Specific), % IACS 100
1.4

Otherwise Unclassified Properties

Base Metal Price, % relative 10
80
Density, g/cm3 3.1
8.6
Embodied Carbon, kg CO2/kg material 8.2
14
Embodied Energy, MJ/kg 150
190
Embodied Water, L/kg 1120
290

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 10 to 55
200
Resilience: Unit (Modulus of Resilience), kJ/m3 1110 to 1760
440
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 45
23
Strength to Weight: Axial, points 45 to 51
28
Strength to Weight: Bending, points 45 to 50
24
Thermal Diffusivity, mm2/s 54
2.7
Thermal Shock Resistance, points 21 to 25
29

Alloy Composition


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Aluminum (Al), % 87.3 to 92.1
0 to 0.4
Carbon (C), % 0
0.030 to 0.1
Chromium (Cr), % 0 to 0.040
20 to 23
Cobalt (Co), % 0
0 to 1.0
Copper (Cu), % 2.0 to 2.6
0 to 0.5
Iron (Fe), % 0 to 0.15
0 to 5.0
Magnesium (Mg), % 1.9 to 2.6
0
Manganese (Mn), % 0 to 0.1
0 to 0.5
Molybdenum (Mo), % 0
8.0 to 10
Nickel (Ni), % 0
58 to 68.8
Niobium (Nb), % 0
3.2 to 4.2
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0 to 0.12
0 to 0.5
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.060
0 to 0.4
Zinc (Zn), % 5.7 to 6.7
0
Zirconium (Zr), % 0.080 to 0.15
0
Residuals, % 0 to 0.15
0