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N06230 Nickel vs. 5010 Aluminum

N06230 nickel belongs to the nickel alloys classification, while 5010 aluminum belongs to the aluminum 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 N06230 nickel and the bottom bar is 5010 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 210
69
Elongation at Break, % 38 to 48
1.1 to 23
Fatigue Strength, MPa 250 to 360
35 to 83
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 83
26
Shear Strength, MPa 420 to 600
64 to 120
Tensile Strength: Ultimate (UTS), MPa 620 to 840
100 to 210
Tensile Strength: Yield (Proof), MPa 330 to 400
38 to 190

Thermal Properties

Latent Heat of Fusion, J/g 310
400
Maximum Temperature: Mechanical, °C 990
180
Melting Completion (Liquidus), °C 1370
650
Melting Onset (Solidus), °C 1300
630
Specific Heat Capacity, J/kg-K 420
900
Thermal Conductivity, W/m-K 8.9
200
Thermal Expansion, µm/m-K 13
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.4
45
Electrical Conductivity: Equal Weight (Specific), % IACS 1.3
150

Otherwise Unclassified Properties

Base Metal Price, % relative 85
9.5
Density, g/cm3 9.5
2.7
Embodied Carbon, kg CO2/kg material 11
8.2
Embodied Energy, MJ/kg 160
150
Embodied Water, L/kg 290
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 200 to 330
2.3 to 20
Resilience: Unit (Modulus of Resilience), kJ/m3 250 to 380
10 to 270
Stiffness to Weight: Axial, points 12
14
Stiffness to Weight: Bending, points 21
50
Strength to Weight: Axial, points 18 to 25
10 to 22
Strength to Weight: Bending, points 17 to 21
18 to 29
Thermal Diffusivity, mm2/s 2.3
82
Thermal Shock Resistance, points 17 to 23
4.5 to 9.4

Alloy Composition

Aluminum (Al), % 0.2 to 0.5
97.1 to 99.7
Boron (B), % 0 to 0.015
0
Carbon (C), % 0.050 to 0.15
0
Chromium (Cr), % 20 to 24
0 to 0.15
Cobalt (Co), % 0 to 5.0
0
Copper (Cu), % 0
0 to 0.25
Iron (Fe), % 0 to 3.0
0 to 0.7
Lanthanum (La), % 0.0050 to 0.050
0
Magnesium (Mg), % 0
0.2 to 0.6
Manganese (Mn), % 0.3 to 1.0
0.1 to 0.3
Molybdenum (Mo), % 1.0 to 3.0
0
Nickel (Ni), % 47.5 to 65.2
0
Phosphorus (P), % 0 to 0.030
0
Silicon (Si), % 0.25 to 0.75
0 to 0.4
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0
0 to 0.1
Tungsten (W), % 13 to 15
0
Zinc (Zn), % 0
0 to 0.3
Residuals, % 0
0 to 0.15