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333.0 Aluminum vs. N06219 Nickel

333.0 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 (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 N06219 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 73
200
Elongation at Break, % 1.0 to 2.0
48
Fatigue Strength, MPa 83 to 100
270
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 28
79
Shear Strength, MPa 190 to 230
520
Tensile Strength: Ultimate (UTS), MPa 230 to 280
730
Tensile Strength: Yield (Proof), MPa 130 to 210
300

Thermal Properties

Latent Heat of Fusion, J/g 520
330
Maximum Temperature: Mechanical, °C 170
980
Melting Completion (Liquidus), °C 590
1430
Melting Onset (Solidus), °C 530
1380
Specific Heat Capacity, J/kg-K 880
450
Thermal Conductivity, W/m-K 100 to 140
10
Thermal Expansion, µm/m-K 21
12

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 26 to 35
1.3
Electrical Conductivity: Equal Weight (Specific), % IACS 83 to 110
1.4

Otherwise Unclassified Properties

Base Metal Price, % relative 10
60
Density, g/cm3 2.8
8.5
Embodied Carbon, kg CO2/kg material 7.6
11
Embodied Energy, MJ/kg 140
140
Embodied Water, L/kg 1040
290

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.1 to 4.6
280
Resilience: Unit (Modulus of Resilience), kJ/m3 120 to 290
230
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 49
23
Strength to Weight: Axial, points 22 to 27
24
Strength to Weight: Bending, points 29 to 34
21
Thermal Diffusivity, mm2/s 42 to 57
2.7
Thermal Shock Resistance, points 11 to 13
21

Alloy Composition

Aluminum (Al), % 81.8 to 89
0 to 0.5
Carbon (C), % 0
0 to 0.050
Chromium (Cr), % 0
18 to 22
Cobalt (Co), % 0
0 to 1.0
Copper (Cu), % 3.0 to 4.0
0 to 0.5
Iron (Fe), % 0 to 1.0
2.0 to 4.0
Magnesium (Mg), % 0.050 to 0.5
0
Manganese (Mn), % 0 to 0.5
0 to 0.5
Molybdenum (Mo), % 0
7.0 to 9.0
Nickel (Ni), % 0 to 0.5
60.8 to 72.3
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 8.0 to 10
0.7 to 1.1
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0 to 0.25
0 to 0.5
Zinc (Zn), % 0 to 1.0
0
Residuals, % 0 to 0.5
0