Nickel 725 vs. EN 1.5510 Steel
Nickel 725 belongs to the nickel alloys classification, while EN 1.5510 steel belongs to the iron alloys. There are 29 material properties with values for both materials. Properties with values for just one material (3, in this case) are not shown.
For each property being compared, the top bar is nickel 725 and the bottom bar is EN 1.5510 steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 190 |
| Elongation at Break, % | 34 | |
| 11 to 21 |
| Fatigue Strength, MPa | 260 | |
| 220 to 330 |
| Poisson's Ratio | 0.29 | |
| 0.29 |
| Reduction in Area, % | 45 | |
| 62 to 72 |
| Shear Modulus, GPa | 78 | |
| 73 |
| Shear Strength, MPa | 580 | |
| 310 to 380 |
| Tensile Strength: Ultimate (UTS), MPa | 860 | |
| 450 to 1600 |
| Tensile Strength: Yield (Proof), MPa | 350 | |
| 310 to 520 |
Thermal Properties
| Latent Heat of Fusion, J/g | 320 | |
| 250 |
| Maximum Temperature: Mechanical, °C | 980 | |
| 400 |
| Melting Completion (Liquidus), °C | 1340 | |
| 1460 |
| Melting Onset (Solidus), °C | 1270 | |
| 1420 |
| Specific Heat Capacity, J/kg-K | 440 | |
| 470 |
| Thermal Expansion, µm/m-K | 13 | |
| 13 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 1.5 | |
| 7.1 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 1.6 | |
| 8.2 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 75 | |
| 1.9 |
| Density, g/cm3 | 8.5 | |
| 7.8 |
| Embodied Carbon, kg CO2/kg material | 13 | |
| 1.4 |
| Embodied Energy, MJ/kg | 190 | |
| 19 |
| Embodied Water, L/kg | 270 | |
| 47 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 240 | |
| 46 to 260 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 300 | |
| 260 to 710 |
| Stiffness to Weight: Axial, points | 13 | |
| 13 |
| Stiffness to Weight: Bending, points | 23 | |
| 24 |
| Strength to Weight: Axial, points | 28 | |
| 16 to 57 |
| Strength to Weight: Bending, points | 24 | |
| 17 to 39 |
| Thermal Shock Resistance, points | 23 | |
| 13 to 47 |
Alloy Composition
| Aluminum (Al), % | 0 to 0.35 | |
| 0 |
| Boron (B), % | 0 | |
| 0.00080 to 0.0050 |
| Carbon (C), % | 0 to 0.030 | |
| 0.25 to 0.3 |
| Chromium (Cr), % | 19 to 22.5 | |
| 0 to 0.3 |
| Copper (Cu), % | 0 | |
| 0 to 0.25 |
| Iron (Fe), % | 2.3 to 15.3 | |
| 97.9 to 99.149 |
| Manganese (Mn), % | 0 to 0.35 | |
| 0.6 to 0.9 |
| Molybdenum (Mo), % | 7.0 to 9.5 | |
| 0 |
| Nickel (Ni), % | 55 to 59 | |
| 0 |
| Niobium (Nb), % | 2.8 to 4.0 | |
| 0 |
| Phosphorus (P), % | 0 to 0.015 | |
| 0 to 0.025 |
| Silicon (Si), % | 0 to 0.2 | |
| 0 to 0.3 |
| Sulfur (S), % | 0 to 0.010 | |
| 0 to 0.025 |
| Titanium (Ti), % | 1.0 to 1.7 | |
| 0 |