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6063 Aluminum vs. N06219 Nickel

6063 aluminum belongs to the aluminum alloys classification, while N06219 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 6063 aluminum and the bottom bar is N06219 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
200
Elongation at Break, % 7.3 to 21
48
Fatigue Strength, MPa 39 to 95
270
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
79
Shear Strength, MPa 70 to 190
520
Tensile Strength: Ultimate (UTS), MPa 110 to 300
730
Tensile Strength: Yield (Proof), MPa 49 to 270
300

Thermal Properties

Latent Heat of Fusion, J/g 400
330
Maximum Temperature: Mechanical, °C 160
980
Melting Completion (Liquidus), °C 650
1430
Melting Onset (Solidus), °C 620
1380
Specific Heat Capacity, J/kg-K 900
450
Thermal Conductivity, W/m-K 190 to 220
10
Thermal Expansion, µm/m-K 23
12

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 49 to 58
1.3
Electrical Conductivity: Equal Weight (Specific), % IACS 160 to 190
1.4

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
60
Density, g/cm3 2.7
8.5
Embodied Carbon, kg CO2/kg material 8.3
11
Embodied Energy, MJ/kg 150
140
Embodied Water, L/kg 1190
290

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 13 to 27
280
Resilience: Unit (Modulus of Resilience), kJ/m3 18 to 540
230
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
23
Strength to Weight: Axial, points 11 to 31
24
Strength to Weight: Bending, points 18 to 37
21
Thermal Diffusivity, mm2/s 79 to 89
2.7
Thermal Shock Resistance, points 4.8 to 13
21

Alloy Composition

Aluminum (Al), % 97.5 to 99.4
0 to 0.5
Carbon (C), % 0
0 to 0.050
Chromium (Cr), % 0 to 0.1
18 to 22
Cobalt (Co), % 0
0 to 1.0
Copper (Cu), % 0 to 0.1
0 to 0.5
Iron (Fe), % 0 to 0.35
2.0 to 4.0
Magnesium (Mg), % 0.45 to 0.9
0
Manganese (Mn), % 0 to 0.1
0 to 0.5
Molybdenum (Mo), % 0
7.0 to 9.0
Nickel (Ni), % 0
60.8 to 72.3
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0.2 to 0.6
0.7 to 1.1
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0 to 0.1
0 to 0.5
Zinc (Zn), % 0 to 0.1
0
Residuals, % 0 to 0.15
0