SAE-AISI 9310 Steel vs. EN 2.4668 Nickel
SAE-AISI 9310 steel belongs to the iron alloys classification, while EN 2.4668 nickel belongs to the nickel alloys. They have a modest 23% of their average alloy composition in common, which, by itself, doesn't mean much. There are 30 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 SAE-AISI 9310 steel and the bottom bar is EN 2.4668 nickel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 190 | |
| 190 |
| Elongation at Break, % | 17 to 19 | |
| 14 |
| Fatigue Strength, MPa | 300 to 390 | |
| 590 |
| Poisson's Ratio | 0.29 | |
| 0.29 |
| Shear Modulus, GPa | 73 | |
| 75 |
| Shear Strength, MPa | 510 to 570 | |
| 840 |
| Tensile Strength: Ultimate (UTS), MPa | 820 to 910 | |
| 1390 |
| Tensile Strength: Yield (Proof), MPa | 450 to 570 | |
| 1160 |
Thermal Properties
| Latent Heat of Fusion, J/g | 250 | |
| 310 |
| Maximum Temperature: Mechanical, °C | 440 | |
| 980 |
| Melting Completion (Liquidus), °C | 1460 | |
| 1460 |
| Melting Onset (Solidus), °C | 1420 | |
| 1410 |
| Specific Heat Capacity, J/kg-K | 470 | |
| 450 |
| Thermal Conductivity, W/m-K | 48 | |
| 13 |
| Thermal Expansion, µm/m-K | 13 | |
| 13 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 7.7 | |
| 1.4 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 8.9 | |
| 1.5 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 4.4 | |
| 75 |
| Density, g/cm3 | 7.9 | |
| 8.3 |
| Embodied Carbon, kg CO2/kg material | 1.8 | |
| 13 |
| Embodied Energy, MJ/kg | 24 | |
| 190 |
| Embodied Water, L/kg | 57 | |
| 250 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 120 to 150 | |
| 180 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 540 to 860 | |
| 3490 |
| Stiffness to Weight: Axial, points | 13 | |
| 13 |
| Stiffness to Weight: Bending, points | 24 | |
| 23 |
| Strength to Weight: Axial, points | 29 to 32 | |
| 46 |
| Strength to Weight: Bending, points | 25 to 27 | |
| 33 |
| Thermal Diffusivity, mm2/s | 13 | |
| 3.5 |
| Thermal Shock Resistance, points | 24 to 27 | |
| 40 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 0.3 to 0.7 |
| Boron (B), % | 0 | |
| 0.0020 to 0.0060 |
| Carbon (C), % | 0.080 to 0.13 | |
| 0.020 to 0.080 |
| Chromium (Cr), % | 1.0 to 1.4 | |
| 17 to 21 |
| Cobalt (Co), % | 0 | |
| 0 to 1.0 |
| Copper (Cu), % | 0 | |
| 0 to 0.3 |
| Iron (Fe), % | 93.8 to 95.2 | |
| 11.2 to 24.6 |
| Manganese (Mn), % | 0.45 to 0.65 | |
| 0 to 0.35 |
| Molybdenum (Mo), % | 0.080 to 0.15 | |
| 2.8 to 3.3 |
| Nickel (Ni), % | 3.0 to 3.5 | |
| 50 to 55 |
| Niobium (Nb), % | 0 | |
| 4.7 to 5.5 |
| Phosphorus (P), % | 0 to 0.015 | |
| 0 to 0.015 |
| Silicon (Si), % | 0.2 to 0.35 | |
| 0 to 0.35 |
| Sulfur (S), % | 0 to 0.012 | |
| 0 to 0.015 |
| Titanium (Ti), % | 0 | |
| 0.6 to 1.2 |