R60802 Alloy vs. C66900 Brass
R60802 alloy belongs to the otherwise unclassified metals classification, while C66900 brass belongs to the copper alloys. There are 18 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 R60802 alloy and the bottom bar is C66900 brass.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 98 | |
| 120 |
| Elongation at Break, % | 22 | |
| 1.1 to 26 |
| Poisson's Ratio | 0.34 | |
| 0.32 |
| Shear Modulus, GPa | 36 | |
| 45 |
| Tensile Strength: Ultimate (UTS), MPa | 430 | |
| 460 to 770 |
| Tensile Strength: Yield (Proof), MPa | 270 | |
| 330 to 760 |
Thermal Properties
| Latent Heat of Fusion, J/g | 250 | |
| 190 |
| Specific Heat Capacity, J/kg-K | 270 | |
| 400 |
| Thermal Expansion, µm/m-K | 6.0 | |
| 20 |
Otherwise Unclassified Properties
| Density, g/cm3 | 6.5 | |
| 8.2 |
| Embodied Water, L/kg | 290 | |
| 310 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 85 | |
| 4.6 to 200 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 380 | |
| 460 to 2450 |
| Stiffness to Weight: Axial, points | 8.3 | |
| 8.1 |
| Stiffness to Weight: Bending, points | 23 | |
| 20 |
| Strength to Weight: Axial, points | 18 | |
| 15 to 26 |
| Strength to Weight: Bending, points | 19 | |
| 16 to 23 |
| Thermal Shock Resistance, points | 53 | |
| 14 to 23 |
Alloy Composition
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| Chromium (Cr), % | 0.050 to 0.15 | |
| 0 |
| Copper (Cu), % | 0 | |
| 62.5 to 64.5 |
| Iron (Fe), % | 0.070 to 0.2 | |
| 0 to 0.25 |
| Lead (Pb), % | 0 | |
| 0 to 0.050 |
| Manganese (Mn), % | 0 | |
| 11.5 to 12.5 |
| Nickel (Ni), % | 0.030 to 0.080 | |
| 0 |
| Tin (Sn), % | 1.2 to 1.7 | |
| 0 |
| Zinc (Zn), % | 0 | |
| 22.5 to 26 |
| Zirconium (Zr), % | 97.8 to 98.7 | |
| 0 |
| Residuals, % | 0 to 0.11 | |
| 0 to 0.2 |