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7050 Aluminum vs. N10675 Nickel

7050 aluminum belongs to the aluminum alloys classification, while N10675 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 N10675 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
220
Elongation at Break, % 2.2 to 12
47
Fatigue Strength, MPa 130 to 210
350
Poisson's Ratio 0.32
0.31
Shear Modulus, GPa 26
85
Shear Strength, MPa 280 to 330
610
Tensile Strength: Ultimate (UTS), MPa 490 to 570
860
Tensile Strength: Yield (Proof), MPa 390 to 500
400

Thermal Properties

Latent Heat of Fusion, J/g 370
320
Maximum Temperature: Mechanical, °C 190
910
Melting Completion (Liquidus), °C 630
1420
Melting Onset (Solidus), °C 490
1370
Specific Heat Capacity, J/kg-K 860
380
Thermal Conductivity, W/m-K 140
11
Thermal Expansion, µm/m-K 24
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
1.3
Electrical Conductivity: Equal Weight (Specific), % IACS 100
1.2

Otherwise Unclassified Properties

Base Metal Price, % relative 10
80
Density, g/cm3 3.1
9.3
Embodied Carbon, kg CO2/kg material 8.2
16
Embodied Energy, MJ/kg 150
210
Embodied Water, L/kg 1120
280

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 10 to 55
330
Resilience: Unit (Modulus of Resilience), kJ/m3 1110 to 1760
350
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 45
22
Strength to Weight: Axial, points 45 to 51
26
Strength to Weight: Bending, points 45 to 50
22
Thermal Diffusivity, mm2/s 54
3.1
Thermal Shock Resistance, points 21 to 25
26

Alloy Composition

Aluminum (Al), % 87.3 to 92.1
0 to 0.5
Carbon (C), % 0
0 to 0.010
Chromium (Cr), % 0 to 0.040
1.0 to 3.0
Cobalt (Co), % 0
0 to 3.0
Copper (Cu), % 2.0 to 2.6
0 to 0.2
Iron (Fe), % 0 to 0.15
1.0 to 3.0
Magnesium (Mg), % 1.9 to 2.6
0
Manganese (Mn), % 0 to 0.1
0 to 3.0
Molybdenum (Mo), % 0
27 to 32
Nickel (Ni), % 0
51.3 to 71
Niobium (Nb), % 0
0 to 0.2
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0 to 0.12
0 to 0.1
Sulfur (S), % 0
0 to 0.010
Tantalum (Ta), % 0
0 to 0.2
Titanium (Ti), % 0 to 0.060
0 to 0.2
Tungsten (W), % 0
0 to 3.0
Vanadium (V), % 0
0 to 0.2
Zinc (Zn), % 5.7 to 6.7
0 to 0.1
Zirconium (Zr), % 0.080 to 0.15
0
Residuals, % 0 to 0.15
0