R30075 Cobalt vs. Grade 5 Titanium
R30075 cobalt belongs to the cobalt alloys classification, while grade 5 titanium belongs to the titanium alloys. There are 28 material properties with values for both materials. Properties with values for just one material (4, in this case) are not shown.
For each property being compared, the top bar is R30075 cobalt and the bottom bar is grade 5 titanium.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 210 to 250 | |
| 110 |
| Elongation at Break, % | 12 | |
| 8.6 to 11 |
| Fatigue Strength, MPa | 250 to 840 | |
| 530 to 630 |
| Poisson's Ratio | 0.29 | |
| 0.32 |
| Reduction in Area, % | 20 | |
| 21 to 25 |
| Shear Modulus, GPa | 82 to 98 | |
| 40 |
| Tensile Strength: Ultimate (UTS), MPa | 780 to 1280 | |
| 1000 to 1190 |
| Tensile Strength: Yield (Proof), MPa | 480 to 840 | |
| 910 to 1110 |
Thermal Properties
| Latent Heat of Fusion, J/g | 320 | |
| 410 |
| Melting Completion (Liquidus), °C | 1360 | |
| 1610 |
| Melting Onset (Solidus), °C | 1290 | |
| 1650 |
| Specific Heat Capacity, J/kg-K | 450 | |
| 560 |
| Thermal Conductivity, W/m-K | 13 | |
| 6.8 |
| Thermal Expansion, µm/m-K | 12 | |
| 8.9 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 2.0 | |
| 1.0 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 2.1 | |
| 2.0 |
Otherwise Unclassified Properties
| Density, g/cm3 | 8.4 | |
| 4.4 |
| Embodied Carbon, kg CO2/kg material | 8.1 | |
| 38 |
| Embodied Energy, MJ/kg | 110 | |
| 610 |
| Embodied Water, L/kg | 530 | |
| 200 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 84 to 140 | |
| 100 to 110 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 560 to 1410 | |
| 3980 to 5880 |
| Stiffness to Weight: Axial, points | 14 to 17 | |
| 13 |
| Stiffness to Weight: Bending, points | 24 to 25 | |
| 35 |
| Strength to Weight: Axial, points | 26 to 42 | |
| 62 to 75 |
| Strength to Weight: Bending, points | 22 to 31 | |
| 50 to 56 |
| Thermal Diffusivity, mm2/s | 3.5 | |
| 2.7 |
| Thermal Shock Resistance, points | 21 to 29 | |
| 76 to 91 |
Alloy Composition
| Aluminum (Al), % | 0 to 0.1 | |
| 5.5 to 6.8 |
| Boron (B), % | 0 to 0.010 | |
| 0 |
| Carbon (C), % | 0 to 0.35 | |
| 0 to 0.080 |
| Chromium (Cr), % | 27 to 30 | |
| 0 |
| Cobalt (Co), % | 58.7 to 68 | |
| 0 |
| Hydrogen (H), % | 0 | |
| 0 to 0.015 |
| Iron (Fe), % | 0 to 0.75 | |
| 0 to 0.4 |
| Manganese (Mn), % | 0 to 1.0 | |
| 0 |
| Molybdenum (Mo), % | 5.0 to 7.0 | |
| 0 |
| Nickel (Ni), % | 0 to 0.5 | |
| 0 |
| Nitrogen (N), % | 0 to 0.25 | |
| 0 to 0.050 |
| Oxygen (O), % | 0 | |
| 0 to 0.2 |
| Phosphorus (P), % | 0 to 0.020 | |
| 0 |
| Silicon (Si), % | 0 to 1.0 | |
| 0 |
| Sulfur (S), % | 0 to 0.010 | |
| 0 |
| Titanium (Ti), % | 0 to 0.1 | |
| 87.4 to 91 |
| Tungsten (W), % | 0 to 0.2 | |
| 0 |
| Vanadium (V), % | 0 | |
| 3.5 to 4.5 |
| Yttrium (Y), % | 0 | |
| 0 to 0.0050 |
| Residuals, % | 0 | |
| 0 to 0.4 |