5086 Aluminum vs. A206.0 Aluminum
Both 5086 aluminum and A206.0 aluminum are aluminum alloys. They have a very high 95% of their average alloy composition in common. There are 31 material properties with values for both materials. Properties with values for just one material (2, in this case) are not shown.
For each property being compared, the top bar is 5086 aluminum and the bottom bar is A206.0 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
Brinell Hardness | 65 to 100 | |
100 to 110 |
Elastic (Young's, Tensile) Modulus, GPa | 68 | |
70 |
Elongation at Break, % | 1.7 to 20 | |
4.2 to 10 |
Fatigue Strength, MPa | 88 to 180 | |
90 to 180 |
Poisson's Ratio | 0.33 | |
0.33 |
Shear Modulus, GPa | 26 | |
26 |
Shear Strength, MPa | 160 to 230 | |
260 |
Tensile Strength: Ultimate (UTS), MPa | 270 to 390 | |
390 to 440 |
Tensile Strength: Yield (Proof), MPa | 110 to 320 | |
250 to 380 |
Thermal Properties
Latent Heat of Fusion, J/g | 400 | |
390 |
Maximum Temperature: Mechanical, °C | 190 | |
170 |
Melting Completion (Liquidus), °C | 640 | |
670 |
Melting Onset (Solidus), °C | 590 | |
550 |
Specific Heat Capacity, J/kg-K | 900 | |
880 |
Thermal Conductivity, W/m-K | 130 | |
130 |
Thermal Expansion, µm/m-K | 24 | |
23 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 31 | |
30 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 100 | |
90 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 9.5 | |
11 |
Density, g/cm3 | 2.7 | |
3.0 |
Embodied Carbon, kg CO2/kg material | 8.8 | |
8.0 |
Embodied Energy, MJ/kg | 150 | |
150 |
Embodied Water, L/kg | 1180 | |
1150 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 5.8 to 42 | |
16 to 37 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 86 to 770 | |
440 to 1000 |
Stiffness to Weight: Axial, points | 14 | |
13 |
Stiffness to Weight: Bending, points | 50 | |
46 |
Strength to Weight: Axial, points | 28 to 40 | |
36 to 41 |
Strength to Weight: Bending, points | 34 to 44 | |
39 to 43 |
Thermal Diffusivity, mm2/s | 52 | |
48 |
Thermal Shock Resistance, points | 12 to 17 | |
17 to 19 |
Alloy Composition
Aluminum (Al), % | 93 to 96.3 | |
93.9 to 95.7 |
Chromium (Cr), % | 0.050 to 0.25 | |
0 |
Copper (Cu), % | 0 to 0.1 | |
4.2 to 5.0 |
Iron (Fe), % | 0 to 0.5 | |
0 to 0.1 |
Magnesium (Mg), % | 3.5 to 4.5 | |
0 to 0.15 |
Manganese (Mn), % | 0.2 to 0.7 | |
0 to 0.2 |
Nickel (Ni), % | 0 | |
0 to 0.050 |
Silicon (Si), % | 0 to 0.4 | |
0 to 0.050 |
Tin (Sn), % | 0 | |
0 to 0.050 |
Titanium (Ti), % | 0 to 0.15 | |
0.15 to 0.3 |
Zinc (Zn), % | 0 to 0.25 | |
0 to 0.1 |
Residuals, % | 0 | |
0 to 0.15 |