R30155 Cobalt vs. ASTM A182 Grade F6b
Both R30155 cobalt and ASTM A182 grade F6b are iron alloys. They have 46% of their average alloy composition in common. There are 32 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 R30155 cobalt and the bottom bar is ASTM A182 grade F6b.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 220 | |
| 260 |
| Elastic (Young's, Tensile) Modulus, GPa | 210 | |
| 190 |
| Elongation at Break, % | 34 | |
| 18 |
| Fatigue Strength, MPa | 310 | |
| 440 |
| Poisson's Ratio | 0.29 | |
| 0.28 |
| Reduction in Area, % | 34 | |
| 51 |
| Shear Modulus, GPa | 81 | |
| 76 |
| Shear Strength, MPa | 570 | |
| 530 |
| Tensile Strength: Ultimate (UTS), MPa | 850 | |
| 850 |
| Tensile Strength: Yield (Proof), MPa | 390 | |
| 710 |
Thermal Properties
| Latent Heat of Fusion, J/g | 300 | |
| 280 |
| Maximum Temperature: Corrosion, °C | 570 | |
| 390 |
| Maximum Temperature: Mechanical, °C | 1100 | |
| 750 |
| Melting Completion (Liquidus), °C | 1470 | |
| 1450 |
| Melting Onset (Solidus), °C | 1420 | |
| 1400 |
| Specific Heat Capacity, J/kg-K | 450 | |
| 480 |
| Thermal Conductivity, W/m-K | 12 | |
| 25 |
| Thermal Expansion, µm/m-K | 14 | |
| 10 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 80 | |
| 8.0 |
| Density, g/cm3 | 8.5 | |
| 7.8 |
| Embodied Carbon, kg CO2/kg material | 9.7 | |
| 2.2 |
| Embodied Energy, MJ/kg | 150 | |
| 30 |
| Embodied Water, L/kg | 300 | |
| 100 |
Common Calculations
| PREN (Pitting Resistance) | 37 | |
| 14 |
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 230 | |
| 140 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 370 | |
| 1280 |
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 23 | |
| 25 |
| Strength to Weight: Axial, points | 28 | |
| 30 |
| Strength to Weight: Bending, points | 24 | |
| 26 |
| Thermal Diffusivity, mm2/s | 3.2 | |
| 6.7 |
| Thermal Shock Resistance, points | 21 | |
| 31 |
Alloy Composition
| Carbon (C), % | 0.080 to 0.16 | |
| 0 to 0.15 |
| Chromium (Cr), % | 20 to 22.5 | |
| 11.5 to 13.5 |
| Cobalt (Co), % | 18.5 to 21 | |
| 0 |
| Copper (Cu), % | 0 | |
| 0 to 0.5 |
| Iron (Fe), % | 24.3 to 36.2 | |
| 81.2 to 87.1 |
| Manganese (Mn), % | 1.0 to 2.0 | |
| 0 to 1.0 |
| Molybdenum (Mo), % | 2.5 to 3.5 | |
| 0.4 to 0.6 |
| Nickel (Ni), % | 19 to 21 | |
| 1.0 to 2.0 |
| Niobium (Nb), % | 0.75 to 1.3 | |
| 0 |
| Nitrogen (N), % | 0 to 0.2 | |
| 0 |
| Phosphorus (P), % | 0 to 0.040 | |
| 0 to 0.020 |
| Silicon (Si), % | 0 to 1.0 | |
| 0 to 1.0 |
| Sulfur (S), % | 0 to 0.030 | |
| 0 to 0.020 |
| Tantalum (Ta), % | 0.75 to 1.3 | |
| 0 |
| Tungsten (W), % | 2.0 to 3.0 | |
| 0 |