R60804 Alloy vs. 50Cr-50Ni Alloy
Both R60804 alloy and 50Cr-50Ni alloy are otherwise unclassified metals. There are 18 material properties with values for both materials. Properties with values for just one material (5, in this case) are not shown.
For each property being compared, the top bar is R60804 alloy and the bottom bar is 50Cr-50Ni alloy.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 98 | |
| 210 |
| Elongation at Break, % | 22 | |
| 5.7 |
| Poisson's Ratio | 0.34 | |
| 0.26 |
| Shear Modulus, GPa | 36 | |
| 84 |
| Tensile Strength: Ultimate (UTS), MPa | 430 | |
| 620 |
| Tensile Strength: Yield (Proof), MPa | 270 | |
| 390 |
Thermal Properties
| Latent Heat of Fusion, J/g | 250 | |
| 350 |
| Specific Heat Capacity, J/kg-K | 270 | |
| 490 |
| Thermal Expansion, µm/m-K | 6.0 | |
| 15 |
Otherwise Unclassified Properties
| Density, g/cm3 | 6.5 | |
| 8.0 |
| Embodied Water, L/kg | 290 | |
| 350 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 85 | |
| 31 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 380 | |
| 350 |
| Stiffness to Weight: Axial, points | 8.3 | |
| 15 |
| Stiffness to Weight: Bending, points | 23 | |
| 25 |
| Strength to Weight: Axial, points | 18 | |
| 21 |
| Strength to Weight: Bending, points | 19 | |
| 20 |
| Thermal Shock Resistance, points | 53 | |
| 14 |
Alloy Composition
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| Aluminum (Al), % | 0 | |
| 0 to 0.25 |
| Carbon (C), % | 0 | |
| 0 to 0.1 |
| Chromium (Cr), % | 0.070 to 0.13 | |
| 48 to 52 |
| Iron (Fe), % | 0.18 to 0.24 | |
| 0 to 1.0 |
| Manganese (Mn), % | 0 | |
| 0 to 0.3 |
| Nickel (Ni), % | 0 | |
| 44.5 to 52 |
| Nitrogen (N), % | 0 | |
| 0 to 0.3 |
| Phosphorus (P), % | 0 | |
| 0 to 0.020 |
| Silicon (Si), % | 0 | |
| 0 to 1.0 |
| Sulfur (S), % | 0 | |
| 0 to 0.020 |
| Tin (Sn), % | 1.2 to 1.7 | |
| 0 |
| Titanium (Ti), % | 0 | |
| 0 to 0.5 |
| Zirconium (Zr), % | 97.8 to 98.6 | |
| 0 |
| Residuals, % | 0 to 0.12 | |
| 0 |