50Cr-50Ni Alloy vs. R60901 Alloy
Both 50Cr-50Ni alloy and R60901 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 50Cr-50Ni alloy and the bottom bar is R60901 alloy.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 210 | |
| 98 |
| Elongation at Break, % | 5.7 | |
| 17 to 22 |
| Poisson's Ratio | 0.26 | |
| 0.34 |
| Shear Modulus, GPa | 84 | |
| 37 |
| Tensile Strength: Ultimate (UTS), MPa | 620 | |
| 500 to 580 |
| Tensile Strength: Yield (Proof), MPa | 390 | |
| 350 to 390 |
Thermal Properties
| Latent Heat of Fusion, J/g | 350 | |
| 250 |
| Specific Heat Capacity, J/kg-K | 490 | |
| 270 |
| Thermal Expansion, µm/m-K | 15 | |
| 6.3 |
Otherwise Unclassified Properties
| Density, g/cm3 | 8.0 | |
| 6.6 |
| Embodied Water, L/kg | 350 | |
| 270 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 31 | |
| 88 to 100 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 350 | |
| 640 to 760 |
| Stiffness to Weight: Axial, points | 15 | |
| 8.3 |
| Stiffness to Weight: Bending, points | 25 | |
| 23 |
| Strength to Weight: Axial, points | 21 | |
| 21 to 25 |
| Strength to Weight: Bending, points | 20 | |
| 21 to 24 |
| Thermal Shock Resistance, points | 14 | |
| 58 to 67 |
Alloy Composition
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| Aluminum (Al), % | 0 to 0.25 | |
| 0 |
| Carbon (C), % | 0 to 0.1 | |
| 0 |
| Chromium (Cr), % | 48 to 52 | |
| 0 |
| Iron (Fe), % | 0 to 1.0 | |
| 0 |
| Manganese (Mn), % | 0 to 0.3 | |
| 0 |
| Nickel (Ni), % | 44.5 to 52 | |
| 0 |
| Niobium (Nb), % | 0 | |
| 2.4 to 2.8 |
| Nitrogen (N), % | 0 to 0.3 | |
| 0 |
| Phosphorus (P), % | 0 to 0.020 | |
| 0 |
| Silicon (Si), % | 0 to 1.0 | |
| 0 |
| Sulfur (S), % | 0 to 0.020 | |
| 0 |
| Titanium (Ti), % | 0 to 0.5 | |
| 0 |
| Zirconium (Zr), % | 0 | |
| 96.8 to 97.5 |
| Residuals, % | 0 | |
| 0 to 0.29 |