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206.0 Aluminum vs. Nickel 200

206.0 aluminum belongs to the aluminum alloys classification, while nickel 200 belongs to the nickel alloys. There are 31 material properties with values for both materials. Properties with values for just one material (3, 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 206.0 aluminum and the bottom bar is nickel 200.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 71
180
Elongation at Break, % 8.4 to 12
23 to 44
Fatigue Strength, MPa 88 to 210
120 to 350
Poisson's Ratio 0.33
0.31
Shear Modulus, GPa 27
70
Shear Strength, MPa 260
300 to 340
Tensile Strength: Ultimate (UTS), MPa 330 to 440
420 to 540
Tensile Strength: Yield (Proof), MPa 190 to 350
120 to 370

Thermal Properties

Latent Heat of Fusion, J/g 390
290
Maximum Temperature: Mechanical, °C 170
900
Melting Completion (Liquidus), °C 650
1460
Melting Onset (Solidus), °C 570
1440
Specific Heat Capacity, J/kg-K 880
450
Thermal Conductivity, W/m-K 120
69
Thermal Expansion, µm/m-K 19
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 33
18
Electrical Conductivity: Equal Weight (Specific), % IACS 99
18

Otherwise Unclassified Properties

Base Metal Price, % relative 11
65
Calomel Potential, mV -680
-150
Density, g/cm3 3.0
8.9
Embodied Carbon, kg CO2/kg material 8.0
11
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1150
230

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 24 to 49
110 to 150
Resilience: Unit (Modulus of Resilience), kJ/m3 270 to 840
42 to 370
Stiffness to Weight: Axial, points 13
11
Stiffness to Weight: Bending, points 46
21
Strength to Weight: Axial, points 30 to 40
13 to 17
Strength to Weight: Bending, points 35 to 42
14 to 17
Thermal Diffusivity, mm2/s 46
17
Thermal Shock Resistance, points 17 to 23
13 to 16

Alloy Composition


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Aluminum (Al), % 93.3 to 95.3
0
Carbon (C), % 0
0 to 0.15
Copper (Cu), % 4.2 to 5.0
0 to 0.25
Iron (Fe), % 0 to 0.15
0 to 0.4
Magnesium (Mg), % 0.15 to 0.35
0
Manganese (Mn), % 0.2 to 0.5
0 to 0.35
Nickel (Ni), % 0 to 0.050
99 to 100
Silicon (Si), % 0 to 0.1
0 to 0.35
Sulfur (S), % 0
0 to 0.010
Tin (Sn), % 0 to 0.050
0
Titanium (Ti), % 0.15 to 0.3
0
Zinc (Zn), % 0 to 0.1
0
Residuals, % 0 to 0.15
0