C66200 Brass vs. Grade 5 Titanium
C66200 brass belongs to the copper alloys classification, while grade 5 titanium belongs to the titanium 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 C66200 brass and the bottom bar is grade 5 titanium.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 110 | |
| 110 |
| Elongation at Break, % | 8.0 to 15 | |
| 8.6 to 11 |
| Poisson's Ratio | 0.33 | |
| 0.32 |
| Shear Modulus, GPa | 42 | |
| 40 |
| Shear Strength, MPa | 270 to 300 | |
| 600 to 710 |
| Tensile Strength: Ultimate (UTS), MPa | 450 to 520 | |
| 1000 to 1190 |
| Tensile Strength: Yield (Proof), MPa | 410 to 480 | |
| 910 to 1110 |
Thermal Properties
| Latent Heat of Fusion, J/g | 200 | |
| 410 |
| Maximum Temperature: Mechanical, °C | 180 | |
| 330 |
| Melting Completion (Liquidus), °C | 1070 | |
| 1610 |
| Melting Onset (Solidus), °C | 1030 | |
| 1650 |
| Specific Heat Capacity, J/kg-K | 390 | |
| 560 |
| Thermal Conductivity, W/m-K | 150 | |
| 6.8 |
| Thermal Expansion, µm/m-K | 18 | |
| 8.9 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 35 | |
| 1.0 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 36 | |
| 2.0 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 29 | |
| 36 |
| Density, g/cm3 | 8.7 | |
| 4.4 |
| Embodied Carbon, kg CO2/kg material | 2.7 | |
| 38 |
| Embodied Energy, MJ/kg | 43 | |
| 610 |
| Embodied Water, L/kg | 320 | |
| 200 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 40 to 66 | |
| 100 to 110 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 760 to 1030 | |
| 3980 to 5880 |
| Stiffness to Weight: Axial, points | 7.2 | |
| 13 |
| Stiffness to Weight: Bending, points | 19 | |
| 35 |
| Strength to Weight: Axial, points | 14 to 17 | |
| 62 to 75 |
| Strength to Weight: Bending, points | 15 to 16 | |
| 50 to 56 |
| Thermal Diffusivity, mm2/s | 45 | |
| 2.7 |
| Thermal Shock Resistance, points | 16 to 18 | |
| 76 to 91 |
Alloy Composition
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| Aluminum (Al), % | 0 | |
| 5.5 to 6.8 |
| Carbon (C), % | 0 | |
| 0 to 0.080 |
| Copper (Cu), % | 86.6 to 91 | |
| 0 |
| Hydrogen (H), % | 0 | |
| 0 to 0.015 |
| Iron (Fe), % | 0 to 0.050 | |
| 0 to 0.4 |
| Lead (Pb), % | 0 to 0.050 | |
| 0 |
| Nickel (Ni), % | 0.3 to 1.0 | |
| 0 |
| Nitrogen (N), % | 0 | |
| 0 to 0.050 |
| Oxygen (O), % | 0 | |
| 0 to 0.2 |
| Phosphorus (P), % | 0.050 to 0.2 | |
| 0 |
| Tin (Sn), % | 0.2 to 0.7 | |
| 0 |
| Titanium (Ti), % | 0 | |
| 87.4 to 91 |
| Vanadium (V), % | 0 | |
| 3.5 to 4.5 |
| Yttrium (Y), % | 0 | |
| 0 to 0.0050 |
| Zinc (Zn), % | 6.5 to 12.9 | |
| 0 |
| Residuals, % | 0 to 0.5 | |
| 0 to 0.4 |