H01 C23400 Brass vs. H01 C41500 Brass
Both H01 C23400 brass and H01 C41500 brass are copper alloys. Both are furnished in the H01 (quarter hard) temper. They have 90% of their average alloy composition in common. There are 24 material properties with values for both materials. Properties with values for just one material (7, in this case) are not shown.
For each property being compared, the top bar is H01 C23400 brass and the bottom bar is H01 C41500 brass.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 110 | |
| 110 |
| Poisson's Ratio | 0.32 | |
| 0.33 |
| Rockwell B Hardness | 52 | |
| 62 |
| Rockwell Superficial 30T Hardness | 51 | |
| 58 |
| Shear Modulus, GPa | 42 | |
| 42 |
| Tensile Strength: Ultimate (UTS), MPa | 370 | |
| 340 |
Thermal Properties
| Latent Heat of Fusion, J/g | 190 | |
| 200 |
| Maximum Temperature: Mechanical, °C | 160 | |
| 180 |
| Melting Completion (Liquidus), °C | 970 | |
| 1030 |
| Melting Onset (Solidus), °C | 930 | |
| 1010 |
| Specific Heat Capacity, J/kg-K | 390 | |
| 380 |
| Thermal Conductivity, W/m-K | 120 | |
| 120 |
| Thermal Expansion, µm/m-K | 19 | |
| 18 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 27 | |
| 30 |
| Density, g/cm3 | 8.5 | |
| 8.7 |
| Embodied Carbon, kg CO2/kg material | 2.6 | |
| 2.8 |
| Embodied Energy, MJ/kg | 43 | |
| 45 |
| Embodied Water, L/kg | 320 | |
| 330 |
Common Calculations
| Stiffness to Weight: Axial, points | 7.2 | |
| 7.1 |
| Stiffness to Weight: Bending, points | 19 | |
| 18 |
| Strength to Weight: Axial, points | 12 | |
| 11 |
| Strength to Weight: Bending, points | 13 | |
| 12 |
| Thermal Diffusivity, mm2/s | 36 | |
| 37 |
| Thermal Shock Resistance, points | 12 | |
| 12 |
Alloy Composition
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| Copper (Cu), % | 81 to 84 | |
| 89 to 93 |
| Iron (Fe), % | 0 to 0.050 | |
| 0 to 0.050 |
| Lead (Pb), % | 0 to 0.050 | |
| 0 to 0.1 |
| Tin (Sn), % | 0 | |
| 1.5 to 2.2 |
| Zinc (Zn), % | 15.7 to 19 | |
| 4.2 to 9.5 |
| Residuals, % | 0 to 0.2 | |
| 0 to 0.5 |