Grade 35 Titanium vs. C63200 Bronze
Grade 35 titanium belongs to the titanium alloys classification, while C63200 bronze belongs to the copper alloys. There are 29 material properties with values for both materials. Properties with values for just one material (3, in this case) are not shown.
For each property being compared, the top bar is grade 35 titanium and the bottom bar is C63200 bronze.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 110 | |
| 120 |
| Elongation at Break, % | 5.6 | |
| 17 to 18 |
| Poisson's Ratio | 0.32 | |
| 0.34 |
| Shear Modulus, GPa | 41 | |
| 44 |
| Shear Strength, MPa | 580 | |
| 390 to 440 |
| Tensile Strength: Ultimate (UTS), MPa | 1000 | |
| 640 to 710 |
| Tensile Strength: Yield (Proof), MPa | 630 | |
| 310 to 350 |
Thermal Properties
| Latent Heat of Fusion, J/g | 420 | |
| 230 |
| Maximum Temperature: Mechanical, °C | 320 | |
| 230 |
| Melting Completion (Liquidus), °C | 1630 | |
| 1060 |
| Melting Onset (Solidus), °C | 1580 | |
| 1040 |
| Specific Heat Capacity, J/kg-K | 550 | |
| 440 |
| Thermal Conductivity, W/m-K | 7.4 | |
| 35 |
| Thermal Expansion, µm/m-K | 9.3 | |
| 18 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 1.1 | |
| 7.0 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 2.2 | |
| 7.6 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 37 | |
| 29 |
| Density, g/cm3 | 4.6 | |
| 8.3 |
| Embodied Carbon, kg CO2/kg material | 33 | |
| 3.4 |
| Embodied Energy, MJ/kg | 530 | |
| 55 |
| Embodied Water, L/kg | 170 | |
| 380 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 49 | |
| 95 to 99 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 1830 | |
| 400 to 510 |
| Stiffness to Weight: Axial, points | 13 | |
| 7.9 |
| Stiffness to Weight: Bending, points | 35 | |
| 20 |
| Strength to Weight: Axial, points | 61 | |
| 21 to 24 |
| Strength to Weight: Bending, points | 49 | |
| 20 to 21 |
| Thermal Diffusivity, mm2/s | 3.0 | |
| 9.6 |
| Thermal Shock Resistance, points | 70 | |
| 22 to 24 |
Alloy Composition
| Aluminum (Al), % | 4.0 to 5.0 | |
| 8.7 to 9.5 |
| Carbon (C), % | 0 to 0.080 | |
| 0 |
| Copper (Cu), % | 0 | |
| 78.8 to 82.6 |
| Hydrogen (H), % | 0 to 0.015 | |
| 0 |
| Iron (Fe), % | 0.2 to 0.8 | |
| 3.5 to 4.3 |
| Lead (Pb), % | 0 | |
| 0 to 0.020 |
| Manganese (Mn), % | 0 | |
| 1.2 to 2.0 |
| Molybdenum (Mo), % | 1.5 to 2.5 | |
| 0 |
| Nickel (Ni), % | 0 | |
| 4.0 to 4.8 |
| Nitrogen (N), % | 0 to 0.050 | |
| 0 |
| Oxygen (O), % | 0 to 0.25 | |
| 0 |
| Silicon (Si), % | 0.2 to 0.4 | |
| 0 to 0.1 |
| Titanium (Ti), % | 88.4 to 93 | |
| 0 |
| Vanadium (V), % | 1.1 to 2.1 | |
| 0 |
| Residuals, % | 0 | |
| 0 to 0.5 |