N06007 Nickel vs. SAE-AISI 9310 Steel
N06007 nickel belongs to the nickel alloys classification, while SAE-AISI 9310 steel belongs to the iron alloys. They have a modest 25% of their average alloy composition in common, which, by itself, doesn't mean much. There are 28 material properties with values for both materials. Properties with values for just one material (4, in this case) are not shown.
For each property being compared, the top bar is N06007 nickel and the bottom bar is SAE-AISI 9310 steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 190 |
| Elongation at Break, % | 38 | |
| 17 to 19 |
| Fatigue Strength, MPa | 330 | |
| 300 to 390 |
| Poisson's Ratio | 0.29 | |
| 0.29 |
| Shear Modulus, GPa | 79 | |
| 73 |
| Shear Strength, MPa | 470 | |
| 510 to 570 |
| Tensile Strength: Ultimate (UTS), MPa | 690 | |
| 820 to 910 |
| Tensile Strength: Yield (Proof), MPa | 260 | |
| 450 to 570 |
Thermal Properties
| Latent Heat of Fusion, J/g | 320 | |
| 250 |
| Maximum Temperature: Mechanical, °C | 990 | |
| 440 |
| Melting Completion (Liquidus), °C | 1340 | |
| 1460 |
| Melting Onset (Solidus), °C | 1260 | |
| 1420 |
| Specific Heat Capacity, J/kg-K | 450 | |
| 470 |
| Thermal Conductivity, W/m-K | 10 | |
| 48 |
| Thermal Expansion, µm/m-K | 14 | |
| 13 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 60 | |
| 4.4 |
| Density, g/cm3 | 8.4 | |
| 7.9 |
| Embodied Carbon, kg CO2/kg material | 10 | |
| 1.8 |
| Embodied Energy, MJ/kg | 140 | |
| 24 |
| Embodied Water, L/kg | 260 | |
| 57 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 200 | |
| 120 to 150 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 170 | |
| 540 to 860 |
| Stiffness to Weight: Axial, points | 13 | |
| 13 |
| Stiffness to Weight: Bending, points | 23 | |
| 24 |
| Strength to Weight: Axial, points | 23 | |
| 29 to 32 |
| Strength to Weight: Bending, points | 21 | |
| 25 to 27 |
| Thermal Diffusivity, mm2/s | 2.7 | |
| 13 |
| Thermal Shock Resistance, points | 18 | |
| 24 to 27 |
Alloy Composition
| Carbon (C), % | 0 to 0.050 | |
| 0.080 to 0.13 |
| Chromium (Cr), % | 21 to 23.5 | |
| 1.0 to 1.4 |
| Cobalt (Co), % | 0 to 2.5 | |
| 0 |
| Copper (Cu), % | 1.5 to 2.5 | |
| 0 |
| Iron (Fe), % | 18 to 21 | |
| 93.8 to 95.2 |
| Manganese (Mn), % | 1.0 to 2.0 | |
| 0.45 to 0.65 |
| Molybdenum (Mo), % | 5.5 to 7.5 | |
| 0.080 to 0.15 |
| Nickel (Ni), % | 36.1 to 51.1 | |
| 3.0 to 3.5 |
| Niobium (Nb), % | 1.8 to 2.5 | |
| 0 |
| Nitrogen (N), % | 0.15 to 0.25 | |
| 0 |
| Phosphorus (P), % | 0 to 0.040 | |
| 0 to 0.015 |
| Silicon (Si), % | 0 to 1.0 | |
| 0.2 to 0.35 |
| Sulfur (S), % | 0 to 0.030 | |
| 0 to 0.012 |
| Tungsten (W), % | 0 to 1.0 | |
| 0 |