R31539 Cobalt vs. 6110A Aluminum
R31539 cobalt belongs to the cobalt alloys classification, while 6110A 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 R31539 cobalt and the bottom bar is 6110A aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 220 | |
| 70 |
| Elongation at Break, % | 13 to 22 | |
| 11 to 18 |
| Fatigue Strength, MPa | 310 to 480 | |
| 140 to 210 |
| Poisson's Ratio | 0.29 | |
| 0.33 |
| Shear Modulus, GPa | 86 | |
| 26 |
| Tensile Strength: Ultimate (UTS), MPa | 1000 to 1340 | |
| 360 to 470 |
| Tensile Strength: Yield (Proof), MPa | 590 to 940 | |
| 250 to 430 |
Thermal Properties
| Latent Heat of Fusion, J/g | 320 | |
| 410 |
| Melting Completion (Liquidus), °C | 1360 | |
| 650 |
| Melting Onset (Solidus), °C | 1290 | |
| 600 |
| Specific Heat Capacity, J/kg-K | 450 | |
| 900 |
| Thermal Conductivity, W/m-K | 13 | |
| 160 |
| Thermal Expansion, µm/m-K | 13 | |
| 23 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 2.0 | |
| 42 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 2.1 | |
| 140 |
Otherwise Unclassified Properties
| Density, g/cm3 | 8.4 | |
| 2.8 |
| Embodied Carbon, kg CO2/kg material | 8.2 | |
| 8.4 |
| Embodied Energy, MJ/kg | 110 | |
| 150 |
| Embodied Water, L/kg | 530 | |
| 1170 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 140 to 190 | |
| 47 to 58 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 780 to 2000 | |
| 450 to 1300 |
| Stiffness to Weight: Axial, points | 15 | |
| 14 |
| Stiffness to Weight: Bending, points | 24 | |
| 50 |
| Strength to Weight: Axial, points | 33 to 44 | |
| 36 to 47 |
| Strength to Weight: Bending, points | 27 to 32 | |
| 41 to 48 |
| Thermal Diffusivity, mm2/s | 3.5 | |
| 65 |
| Thermal Shock Resistance, points | 24 to 32 | |
| 16 to 21 |
Alloy Composition
| Aluminum (Al), % | 0.3 to 1.0 | |
| 94.8 to 98 |
| Carbon (C), % | 0 to 0.14 | |
| 0 |
| Chromium (Cr), % | 26 to 30 | |
| 0.050 to 0.25 |
| Cobalt (Co), % | 57.7 to 68.7 | |
| 0 |
| Copper (Cu), % | 0 | |
| 0.3 to 0.8 |
| Iron (Fe), % | 0 to 0.75 | |
| 0 to 0.5 |
| Lanthanum (La), % | 0.030 to 0.2 | |
| 0 |
| Magnesium (Mg), % | 0 | |
| 0.7 to 1.1 |
| Manganese (Mn), % | 0 to 1.0 | |
| 0.3 to 0.9 |
| 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 | |
| 0.7 to 1.1 |
| Titanium (Ti), % | 0 | |
| 0 to 0.2 |
| Zinc (Zn), % | 0 | |
| 0 to 0.2 |
| Zirconium (Zr), % | 0 | |
| 0 to 0.2 |
| Residuals, % | 0 | |
| 0 to 0.15 |