Hot Rolled EN 1.4618 vs. Hot Worked Nickel 690
Hot rolled EN 1.4618 belongs to the iron alloys classification, while hot worked nickel 690 belongs to the nickel alloys. They have a modest 32% of their average alloy composition in common, which, by itself, doesn't mean much. There are 31 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 hot rolled EN 1.4618 and the bottom bar is hot worked nickel 690.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 200 | |
| 90 |
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 200 |
| Elongation at Break, % | 51 | |
| 28 |
| Fatigue Strength, MPa | 240 | |
| 180 |
| Poisson's Ratio | 0.28 | |
| 0.28 |
| Shear Modulus, GPa | 77 | |
| 79 |
| Shear Strength, MPa | 480 | |
| 430 |
| Tensile Strength: Ultimate (UTS), MPa | 680 | |
| 660 |
| Tensile Strength: Yield (Proof), MPa | 250 | |
| 270 |
Thermal Properties
| Latent Heat of Fusion, J/g | 280 | |
| 320 |
| Maximum Temperature: Mechanical, °C | 900 | |
| 1010 |
| Melting Completion (Liquidus), °C | 1400 | |
| 1380 |
| Melting Onset (Solidus), °C | 1360 | |
| 1340 |
| Specific Heat Capacity, J/kg-K | 480 | |
| 470 |
| Thermal Conductivity, W/m-K | 15 | |
| 14 |
| Thermal Expansion, µm/m-K | 16 | |
| 14 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 2.4 | |
| 1.5 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 2.7 | |
| 1.6 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 13 | |
| 50 |
| Density, g/cm3 | 7.7 | |
| 8.3 |
| Embodied Carbon, kg CO2/kg material | 2.7 | |
| 8.2 |
| Embodied Energy, MJ/kg | 39 | |
| 120 |
| Embodied Water, L/kg | 150 | |
| 290 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 270 | |
| 150 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 160 | |
| 180 |
| Stiffness to Weight: Axial, points | 14 | |
| 13 |
| Stiffness to Weight: Bending, points | 25 | |
| 24 |
| Strength to Weight: Axial, points | 24 | |
| 22 |
| Strength to Weight: Bending, points | 22 | |
| 20 |
| Thermal Diffusivity, mm2/s | 4.0 | |
| 3.5 |
| Thermal Shock Resistance, points | 15 | |
| 17 |
Alloy Composition
| Carbon (C), % | 0 to 0.1 | |
| 0 to 0.050 |
| Chromium (Cr), % | 16.5 to 18.5 | |
| 27 to 31 |
| Copper (Cu), % | 1.0 to 2.5 | |
| 0 to 0.5 |
| Iron (Fe), % | 62.7 to 72.5 | |
| 7.0 to 11 |
| Manganese (Mn), % | 5.5 to 9.5 | |
| 0 to 0.5 |
| Nickel (Ni), % | 4.5 to 5.5 | |
| 58 to 66 |
| Nitrogen (N), % | 0 to 0.15 | |
| 0 |
| Phosphorus (P), % | 0 to 0.070 | |
| 0 |
| Silicon (Si), % | 0 to 1.0 | |
| 0 to 0.5 |
| Sulfur (S), % | 0 to 0.010 | |
| 0 to 0.015 |