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333.0 Aluminum vs. N06002 Nickel

333.0 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 333.0 aluminum and the bottom bar is N06002 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 73
210
Elongation at Break, % 1.0 to 2.0
41
Fatigue Strength, MPa 83 to 100
250
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 28
81
Shear Strength, MPa 190 to 230
520
Tensile Strength: Ultimate (UTS), MPa 230 to 280
760
Tensile Strength: Yield (Proof), MPa 130 to 210
310

Thermal Properties

Latent Heat of Fusion, J/g 520
320
Maximum Temperature: Mechanical, °C 170
990
Melting Completion (Liquidus), °C 590
1360
Melting Onset (Solidus), °C 530
1260
Specific Heat Capacity, J/kg-K 880
450
Thermal Conductivity, W/m-K 100 to 140
9.9
Thermal Expansion, µm/m-K 21
14

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 26 to 35
1.5
Electrical Conductivity: Equal Weight (Specific), % IACS 83 to 110
1.6

Otherwise Unclassified Properties

Base Metal Price, % relative 10
55
Density, g/cm3 2.8
8.5
Embodied Carbon, kg CO2/kg material 7.6
9.3
Embodied Energy, MJ/kg 140
130
Embodied Water, L/kg 1040
270

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.1 to 4.6
250
Resilience: Unit (Modulus of Resilience), kJ/m3 120 to 290
230
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 49
23
Strength to Weight: Axial, points 22 to 27
25
Strength to Weight: Bending, points 29 to 34
22
Thermal Diffusivity, mm2/s 42 to 57
2.6
Thermal Shock Resistance, points 11 to 13
19

Alloy Composition

Aluminum (Al), % 81.8 to 89
0
Carbon (C), % 0
0.050 to 0.15
Chromium (Cr), % 0
20.5 to 23
Cobalt (Co), % 0
0.5 to 2.5
Copper (Cu), % 3.0 to 4.0
0
Iron (Fe), % 0 to 1.0
17 to 20
Magnesium (Mg), % 0.050 to 0.5
0
Manganese (Mn), % 0 to 0.5
0 to 1.0
Molybdenum (Mo), % 0
8.0 to 10
Nickel (Ni), % 0 to 0.5
42.3 to 54
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 8.0 to 10
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.25
0
Tungsten (W), % 0
0.2 to 1.0
Zinc (Zn), % 0 to 1.0
0
Residuals, % 0 to 0.5
0