C35600 Brass vs. R58150 Titanium
C35600 brass belongs to the copper alloys classification, while R58150 titanium belongs to the titanium 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 C35600 brass and the bottom bar is R58150 titanium.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 100 | |
| 140 |
| Poisson's Ratio | 0.31 | |
| 0.32 |
| Shear Modulus, GPa | 39 | |
| 52 |
| Tensile Strength: Ultimate (UTS), MPa | 340 to 650 | |
| 770 |
Thermal Properties
| Latent Heat of Fusion, J/g | 170 | |
| 410 |
| Maximum Temperature: Mechanical, °C | 120 | |
| 320 |
| Melting Completion (Liquidus), °C | 900 | |
| 1760 |
| Melting Onset (Solidus), °C | 890 | |
| 1700 |
| Specific Heat Capacity, J/kg-K | 380 | |
| 500 |
| Thermal Expansion, µm/m-K | 21 | |
| 8.4 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 23 | |
| 48 |
| Density, g/cm3 | 8.1 | |
| 5.4 |
| Embodied Carbon, kg CO2/kg material | 2.6 | |
| 31 |
| Embodied Energy, MJ/kg | 45 | |
| 480 |
| Embodied Water, L/kg | 320 | |
| 150 |
Common Calculations
| Stiffness to Weight: Axial, points | 7.0 | |
| 14 |
| Stiffness to Weight: Bending, points | 19 | |
| 32 |
| Strength to Weight: Axial, points | 11 to 22 | |
| 40 |
| Strength to Weight: Bending, points | 13 to 21 | |
| 35 |
| Thermal Shock Resistance, points | 11 to 22 | |
| 48 |
Alloy Composition
| Carbon (C), % | 0 | |
| 0 to 0.1 |
| Copper (Cu), % | 60 to 63 | |
| 0 |
| Hydrogen (H), % | 0 | |
| 0 to 0.015 |
| Iron (Fe), % | 0 to 0.1 | |
| 0 to 0.1 |
| Lead (Pb), % | 2.0 to 3.0 | |
| 0 |
| Molybdenum (Mo), % | 0 | |
| 14 to 16 |
| Nitrogen (N), % | 0 | |
| 0 to 0.050 |
| Oxygen (O), % | 0 | |
| 0 to 0.2 |
| Titanium (Ti), % | 0 | |
| 83.5 to 86 |
| Zinc (Zn), % | 33.4 to 38 | |
| 0 |
| Residuals, % | 0 to 0.5 | |
| 0 |