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6016 Aluminum vs. N06002 Nickel

6016 aluminum belongs to the aluminum alloys classification, while N06002 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 6016 aluminum and the bottom bar is N06002 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
210
Elongation at Break, % 11 to 27
41
Fatigue Strength, MPa 68 to 89
250
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
81
Shear Strength, MPa 130 to 170
520
Tensile Strength: Ultimate (UTS), MPa 200 to 280
760
Tensile Strength: Yield (Proof), MPa 110 to 210
310

Thermal Properties

Latent Heat of Fusion, J/g 410
320
Maximum Temperature: Mechanical, °C 160
990
Melting Completion (Liquidus), °C 660
1360
Melting Onset (Solidus), °C 610
1260
Specific Heat Capacity, J/kg-K 900
450
Thermal Conductivity, W/m-K 190 to 210
9.9
Thermal Expansion, µm/m-K 23
14

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 48 to 54
1.5
Electrical Conductivity: Equal Weight (Specific), % IACS 160 to 180
1.6

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
55
Density, g/cm3 2.7
8.5
Embodied Carbon, kg CO2/kg material 8.2
9.3
Embodied Energy, MJ/kg 150
130
Embodied Water, L/kg 1180
270

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 29 to 47
250
Resilience: Unit (Modulus of Resilience), kJ/m3 82 to 340
230
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 51
23
Strength to Weight: Axial, points 21 to 29
25
Strength to Weight: Bending, points 29 to 35
22
Thermal Diffusivity, mm2/s 77 to 86
2.6
Thermal Shock Resistance, points 9.1 to 12
19

Alloy Composition

Aluminum (Al), % 96.4 to 98.8
0
Carbon (C), % 0
0.050 to 0.15
Chromium (Cr), % 0 to 0.1
20.5 to 23
Cobalt (Co), % 0
0.5 to 2.5
Copper (Cu), % 0 to 0.2
0
Iron (Fe), % 0 to 0.5
17 to 20
Magnesium (Mg), % 0.25 to 0.6
0
Manganese (Mn), % 0 to 0.2
0 to 1.0
Molybdenum (Mo), % 0
8.0 to 10
Nickel (Ni), % 0
42.3 to 54
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 1.0 to 1.5
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.15
0
Tungsten (W), % 0
0.2 to 1.0
Zinc (Zn), % 0 to 0.2
0
Residuals, % 0 to 0.15
0