R60705 Alloy vs. C12000 Copper
R60705 alloy belongs to the otherwise unclassified metals classification, while C12000 copper belongs to the copper alloys. There are 20 material properties with values for both materials. Properties with values for just one material (12, in this case) are not shown.
For each property being compared, the top bar is R60705 alloy and the bottom bar is C12000 copper.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 98 | |
| 120 |
| Elongation at Break, % | 18 | |
| 2.8 to 50 |
| Poisson's Ratio | 0.34 | |
| 0.34 |
| Shear Modulus, GPa | 37 | |
| 43 |
| Tensile Strength: Ultimate (UTS), MPa | 540 | |
| 230 to 410 |
| Tensile Strength: Yield (Proof), MPa | 430 | |
| 77 to 400 |
Thermal Properties
| Latent Heat of Fusion, J/g | 250 | |
| 210 |
| Specific Heat Capacity, J/kg-K | 270 | |
| 390 |
| Thermal Conductivity, W/m-K | 17 | |
| 390 |
| Thermal Expansion, µm/m-K | 6.3 | |
| 17 |
Otherwise Unclassified Properties
| Density, g/cm3 | 6.7 | |
| 9.0 |
| Embodied Water, L/kg | 450 | |
| 310 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 90 | |
| 10 to 91 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 950 | |
| 25 to 690 |
| Stiffness to Weight: Axial, points | 8.1 | |
| 7.2 |
| Stiffness to Weight: Bending, points | 23 | |
| 18 |
| Strength to Weight: Axial, points | 22 | |
| 7.2 to 13 |
| Strength to Weight: Bending, points | 22 | |
| 9.4 to 14 |
| Thermal Diffusivity, mm2/s | 9.5 | |
| 110 |
| Thermal Shock Resistance, points | 63 | |
| 8.2 to 15 |
Alloy Composition
| Carbon (C), % | 0 to 0.050 | |
| 0 |
| Chromium (Cr), % | 0 to 0.2 | |
| 0 |
| Copper (Cu), % | 0 | |
| 99.9 to 99.996 |
| Hafnium (Hf), % | 0 to 4.5 | |
| 0 |
| Hydrogen (H), % | 0 to 0.0050 | |
| 0 |
| Iron (Fe), % | 0 to 0.2 | |
| 0 |
| Niobium (Nb), % | 2.0 to 3.0 | |
| 0 |
| Nitrogen (N), % | 0 to 0.025 | |
| 0 |
| Oxygen (O), % | 0 to 0.18 | |
| 0 |
| Phosphorus (P), % | 0 | |
| 0.0040 to 0.012 |
| Zirconium (Zr), % | 91 to 98 | |
| 0 |