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6463 Aluminum vs. N10665 Nickel

6463 aluminum belongs to the aluminum alloys classification, while N10665 nickel belongs to the nickel alloys. There are 30 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 6463 aluminum and the bottom bar is N10665 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
220
Elongation at Break, % 9.0 to 17
45
Fatigue Strength, MPa 45 to 76
340
Poisson's Ratio 0.33
0.31
Shear Modulus, GPa 26
84
Shear Strength, MPa 86 to 150
600
Tensile Strength: Ultimate (UTS), MPa 140 to 230
860
Tensile Strength: Yield (Proof), MPa 82 to 200
400

Thermal Properties

Latent Heat of Fusion, J/g 400
310
Maximum Temperature: Mechanical, °C 160
900
Melting Completion (Liquidus), °C 660
1620
Melting Onset (Solidus), °C 620
1570
Specific Heat Capacity, J/kg-K 900
390
Thermal Conductivity, W/m-K 190 to 210
11
Thermal Expansion, µm/m-K 23
10

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 50 to 55
1.3
Electrical Conductivity: Equal Weight (Specific), % IACS 170 to 180
1.2

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
75
Density, g/cm3 2.7
9.3
Embodied Carbon, kg CO2/kg material 8.3
15
Embodied Energy, MJ/kg 150
200
Embodied Water, L/kg 1190
270

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 17 to 25
320
Resilience: Unit (Modulus of Resilience), kJ/m3 50 to 300
360
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
22
Strength to Weight: Axial, points 14 to 24
26
Strength to Weight: Bending, points 22 to 31
22
Thermal Diffusivity, mm2/s 79 to 86
3.1
Thermal Shock Resistance, points 6.3 to 10
27

Alloy Composition

Aluminum (Al), % 97.9 to 99.4
0
Carbon (C), % 0
0 to 0.020
Chromium (Cr), % 0
0 to 1.0
Cobalt (Co), % 0
0 to 1.0
Copper (Cu), % 0 to 0.2
0
Iron (Fe), % 0 to 0.15
0 to 2.0
Magnesium (Mg), % 0.45 to 0.9
0
Manganese (Mn), % 0 to 0.050
0 to 1.0
Molybdenum (Mo), % 0
26 to 30
Nickel (Ni), % 0
64.8 to 74
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0.2 to 0.6
0 to 0.1
Sulfur (S), % 0
0 to 0.030
Zinc (Zn), % 0 to 0.050
0
Residuals, % 0 to 0.15
0