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8090 Aluminum vs. N06230 Nickel

8090 aluminum belongs to the aluminum alloys classification, while N06230 nickel belongs to the nickel alloys. There are 29 material properties with values for both materials. Properties with values for just one material (2, 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 8090 aluminum and the bottom bar is N06230 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 67
210
Elongation at Break, % 3.5 to 13
38 to 48
Fatigue Strength, MPa 91 to 140
250 to 360
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 25
83
Tensile Strength: Ultimate (UTS), MPa 340 to 490
620 to 840
Tensile Strength: Yield (Proof), MPa 210 to 420
330 to 400

Thermal Properties

Latent Heat of Fusion, J/g 400
310
Maximum Temperature: Mechanical, °C 190
990
Melting Completion (Liquidus), °C 660
1370
Melting Onset (Solidus), °C 600
1300
Specific Heat Capacity, J/kg-K 960
420
Thermal Conductivity, W/m-K 95 to 160
8.9
Thermal Expansion, µm/m-K 24
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 20
1.4
Electrical Conductivity: Equal Weight (Specific), % IACS 66
1.3

Otherwise Unclassified Properties

Base Metal Price, % relative 18
85
Density, g/cm3 2.7
9.5
Embodied Carbon, kg CO2/kg material 8.6
11
Embodied Energy, MJ/kg 170
160
Embodied Water, L/kg 1160
290

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 16 to 41
200 to 330
Resilience: Unit (Modulus of Resilience), kJ/m3 340 to 1330
250 to 380
Stiffness to Weight: Axial, points 14
12
Stiffness to Weight: Bending, points 50
21
Strength to Weight: Axial, points 34 to 49
18 to 25
Strength to Weight: Bending, points 39 to 50
17 to 21
Thermal Diffusivity, mm2/s 36 to 60
2.3
Thermal Shock Resistance, points 15 to 22
17 to 23

Alloy Composition

Aluminum (Al), % 93 to 98.4
0.2 to 0.5
Boron (B), % 0
0 to 0.015
Carbon (C), % 0
0.050 to 0.15
Chromium (Cr), % 0 to 0.1
20 to 24
Cobalt (Co), % 0
0 to 5.0
Copper (Cu), % 1.0 to 1.6
0
Iron (Fe), % 0 to 0.3
0 to 3.0
Lanthanum (La), % 0
0.0050 to 0.050
Lithium (Li), % 2.2 to 2.7
0
Magnesium (Mg), % 0.6 to 1.3
0
Manganese (Mn), % 0 to 0.1
0.3 to 1.0
Molybdenum (Mo), % 0
1.0 to 3.0
Nickel (Ni), % 0
47.5 to 65.2
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0 to 0.2
0.25 to 0.75
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.1
0
Tungsten (W), % 0
13 to 15
Zinc (Zn), % 0 to 0.25
0
Zirconium (Zr), % 0.040 to 0.16
0
Residuals, % 0 to 0.15
0