N06007 Nickel vs. EN 1.7386 Steel
N06007 nickel belongs to the nickel alloys classification, while EN 1.7386 steel belongs to the iron alloys. They have a modest 31% 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 (5, in this case) are not shown.
For each property being compared, the top bar is N06007 nickel and the bottom bar is EN 1.7386 steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 190 |
| Elongation at Break, % | 38 | |
| 18 to 21 |
| Fatigue Strength, MPa | 330 | |
| 170 to 290 |
| Poisson's Ratio | 0.29 | |
| 0.28 |
| Shear Modulus, GPa | 79 | |
| 75 |
| Shear Strength, MPa | 470 | |
| 340 to 410 |
| Tensile Strength: Ultimate (UTS), MPa | 690 | |
| 550 to 670 |
| Tensile Strength: Yield (Proof), MPa | 260 | |
| 240 to 440 |
Thermal Properties
| Latent Heat of Fusion, J/g | 320 | |
| 270 |
| Maximum Temperature: Mechanical, °C | 990 | |
| 600 |
| Melting Completion (Liquidus), °C | 1340 | |
| 1450 |
| Melting Onset (Solidus), °C | 1260 | |
| 1410 |
| Specific Heat Capacity, J/kg-K | 450 | |
| 480 |
| Thermal Conductivity, W/m-K | 10 | |
| 26 |
| Thermal Expansion, µm/m-K | 14 | |
| 13 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 60 | |
| 6.5 |
| Density, g/cm3 | 8.4 | |
| 7.8 |
| Embodied Carbon, kg CO2/kg material | 10 | |
| 2.0 |
| Embodied Energy, MJ/kg | 140 | |
| 28 |
| Embodied Water, L/kg | 260 | |
| 88 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 200 | |
| 92 to 110 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 170 | |
| 150 to 490 |
| Stiffness to Weight: Axial, points | 13 | |
| 14 |
| Stiffness to Weight: Bending, points | 23 | |
| 25 |
| Strength to Weight: Axial, points | 23 | |
| 20 to 24 |
| Strength to Weight: Bending, points | 21 | |
| 19 to 22 |
| Thermal Diffusivity, mm2/s | 2.7 | |
| 6.9 |
| Thermal Shock Resistance, points | 18 | |
| 15 to 18 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 0 to 0.040 |
| Carbon (C), % | 0 to 0.050 | |
| 0.080 to 0.15 |
| Chromium (Cr), % | 21 to 23.5 | |
| 8.0 to 10 |
| Cobalt (Co), % | 0 to 2.5 | |
| 0 |
| Copper (Cu), % | 1.5 to 2.5 | |
| 0 to 0.3 |
| Iron (Fe), % | 18 to 21 | |
| 86.8 to 90.5 |
| Manganese (Mn), % | 1.0 to 2.0 | |
| 0.3 to 0.6 |
| Molybdenum (Mo), % | 5.5 to 7.5 | |
| 0.9 to 1.1 |
| Nickel (Ni), % | 36.1 to 51.1 | |
| 0 |
| Niobium (Nb), % | 1.8 to 2.5 | |
| 0 |
| Nitrogen (N), % | 0.15 to 0.25 | |
| 0 |
| Phosphorus (P), % | 0 to 0.040 | |
| 0 to 0.025 |
| Silicon (Si), % | 0 to 1.0 | |
| 0.25 to 1.0 |
| Sulfur (S), % | 0 to 0.030 | |
| 0 to 0.010 |
| Tungsten (W), % | 0 to 1.0 | |
| 0 |