R58150 Titanium vs. C26800 Brass
R58150 titanium belongs to the titanium alloys classification, while C26800 brass belongs to the copper alloys. There are 20 material properties with values for both materials. Properties with values for just one material (13, in this case) are not shown.
For each property being compared, the top bar is R58150 titanium and the bottom bar is C26800 brass.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 140 | |
| 110 |
| Poisson's Ratio | 0.32 | |
| 0.31 |
| Shear Modulus, GPa | 52 | |
| 40 |
| Tensile Strength: Ultimate (UTS), MPa | 770 | |
| 310 to 650 |
Thermal Properties
| Latent Heat of Fusion, J/g | 410 | |
| 180 |
| Maximum Temperature: Mechanical, °C | 320 | |
| 130 |
| Melting Completion (Liquidus), °C | 1760 | |
| 930 |
| Melting Onset (Solidus), °C | 1700 | |
| 900 |
| Specific Heat Capacity, J/kg-K | 500 | |
| 390 |
| Thermal Expansion, µm/m-K | 8.4 | |
| 20 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 48 | |
| 24 |
| Density, g/cm3 | 5.4 | |
| 8.1 |
| Embodied Carbon, kg CO2/kg material | 31 | |
| 2.7 |
| Embodied Energy, MJ/kg | 480 | |
| 45 |
| Embodied Water, L/kg | 150 | |
| 320 |
Common Calculations
| Stiffness to Weight: Axial, points | 14 | |
| 7.2 |
| Stiffness to Weight: Bending, points | 32 | |
| 19 |
| Strength to Weight: Axial, points | 40 | |
| 11 to 22 |
| Strength to Weight: Bending, points | 35 | |
| 13 to 21 |
| Thermal Shock Resistance, points | 48 | |
| 10 to 22 |
Alloy Composition
| Carbon (C), % | 0 to 0.1 | |
| 0 |
| Copper (Cu), % | 0 | |
| 64 to 68.5 |
| Hydrogen (H), % | 0 to 0.015 | |
| 0 |
| Iron (Fe), % | 0 to 0.1 | |
| 0 to 0.050 |
| Lead (Pb), % | 0 | |
| 0 to 0.15 |
| Molybdenum (Mo), % | 14 to 16 | |
| 0 |
| Nitrogen (N), % | 0 to 0.050 | |
| 0 |
| Oxygen (O), % | 0 to 0.2 | |
| 0 |
| Titanium (Ti), % | 83.5 to 86 | |
| 0 |
| Zinc (Zn), % | 0 | |
| 31 to 36 |
| Residuals, % | 0 | |
| 0 to 0.3 |