R31538 Cobalt vs. 8090 Aluminum
R31538 cobalt belongs to the cobalt alloys classification, while 8090 aluminum belongs to the aluminum alloys. There are 27 material properties with values for both materials. Properties with values for just one material (5, 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 R31538 cobalt and the bottom bar is 8090 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 220 | |
| 67 |
| Elongation at Break, % | 13 to 23 | |
| 3.5 to 13 |
| Fatigue Strength, MPa | 310 to 480 | |
| 91 to 140 |
| Poisson's Ratio | 0.29 | |
| 0.33 |
| Shear Modulus, GPa | 86 | |
| 25 |
| Tensile Strength: Ultimate (UTS), MPa | 1020 to 1360 | |
| 340 to 490 |
| Tensile Strength: Yield (Proof), MPa | 580 to 930 | |
| 210 to 420 |
Thermal Properties
| Latent Heat of Fusion, J/g | 320 | |
| 400 |
| Melting Completion (Liquidus), °C | 1360 | |
| 660 |
| Melting Onset (Solidus), °C | 1290 | |
| 600 |
| Specific Heat Capacity, J/kg-K | 450 | |
| 960 |
| Thermal Conductivity, W/m-K | 13 | |
| 95 to 160 |
| Thermal Expansion, µm/m-K | 13 | |
| 24 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 2.0 | |
| 20 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 2.1 | |
| 66 |
Otherwise Unclassified Properties
| Density, g/cm3 | 8.4 | |
| 2.7 |
| Embodied Carbon, kg CO2/kg material | 8.1 | |
| 8.6 |
| Embodied Energy, MJ/kg | 110 | |
| 170 |
| Embodied Water, L/kg | 530 | |
| 1160 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 140 to 200 | |
| 16 to 41 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 750 to 1920 | |
| 340 to 1330 |
| Stiffness to Weight: Axial, points | 15 | |
| 14 |
| Stiffness to Weight: Bending, points | 24 | |
| 50 |
| Strength to Weight: Axial, points | 34 to 45 | |
| 34 to 49 |
| Strength to Weight: Bending, points | 27 to 32 | |
| 39 to 50 |
| Thermal Diffusivity, mm2/s | 3.5 | |
| 36 to 60 |
| Thermal Shock Resistance, points | 25 to 33 | |
| 15 to 22 |
Alloy Composition
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| Aluminum (Al), % | 0 | |
| 93 to 98.4 |
| Carbon (C), % | 0.15 to 0.35 | |
| 0 |
| Chromium (Cr), % | 26 to 30 | |
| 0 to 0.1 |
| Cobalt (Co), % | 58.7 to 68.9 | |
| 0 |
| Copper (Cu), % | 0 | |
| 1.0 to 1.6 |
| Iron (Fe), % | 0 to 0.75 | |
| 0 to 0.3 |
| Lithium (Li), % | 0 | |
| 2.2 to 2.7 |
| Magnesium (Mg), % | 0 | |
| 0.6 to 1.3 |
| Manganese (Mn), % | 0 to 1.0 | |
| 0 to 0.1 |
| Molybdenum (Mo), % | 5.0 to 7.0 | |
| 0 |
| Nickel (Ni), % | 0 to 1.0 | |
| 0 |
| Nitrogen (N), % | 0 to 0.25 | |
| 0 |
| Silicon (Si), % | 0 to 1.0 | |
| 0 to 0.2 |
| Titanium (Ti), % | 0 | |
| 0 to 0.1 |
| Zinc (Zn), % | 0 | |
| 0 to 0.25 |
| Zirconium (Zr), % | 0 | |
| 0.040 to 0.16 |
| Residuals, % | 0 | |
| 0 to 0.15 |