EN 1.4913 Stainless Steel vs. Nickel 690
EN 1.4913 stainless steel belongs to the iron alloys classification, while nickel 690 belongs to the nickel alloys. They have a modest 21% 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 EN 1.4913 stainless steel and the bottom bar is nickel 690.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 190 | |
| 200 |
| Elongation at Break, % | 14 to 22 | |
| 3.4 to 34 |
| Fatigue Strength, MPa | 320 to 480 | |
| 180 to 300 |
| Poisson's Ratio | 0.28 | |
| 0.28 |
| Shear Modulus, GPa | 75 | |
| 79 |
| Shear Strength, MPa | 550 to 590 | |
| 420 to 570 |
| Tensile Strength: Ultimate (UTS), MPa | 870 to 980 | |
| 640 to 990 |
| Tensile Strength: Yield (Proof), MPa | 480 to 850 | |
| 250 to 760 |
Thermal Properties
| Latent Heat of Fusion, J/g | 270 | |
| 320 |
| Maximum Temperature: Mechanical, °C | 700 | |
| 1010 |
| Melting Completion (Liquidus), °C | 1460 | |
| 1380 |
| Melting Onset (Solidus), °C | 1410 | |
| 1340 |
| Specific Heat Capacity, J/kg-K | 480 | |
| 470 |
| Thermal Conductivity, W/m-K | 24 | |
| 14 |
| Thermal Expansion, µm/m-K | 11 | |
| 14 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 2.9 | |
| 1.5 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 3.3 | |
| 1.6 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 9.0 | |
| 50 |
| Density, g/cm3 | 7.8 | |
| 8.3 |
| Embodied Carbon, kg CO2/kg material | 2.9 | |
| 8.2 |
| Embodied Energy, MJ/kg | 41 | |
| 120 |
| Embodied Water, L/kg | 97 | |
| 290 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 130 to 160 | |
| 31 to 170 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 600 to 1860 | |
| 160 to 1440 |
| Stiffness to Weight: Axial, points | 14 | |
| 13 |
| Stiffness to Weight: Bending, points | 25 | |
| 24 |
| Strength to Weight: Axial, points | 31 to 35 | |
| 21 to 33 |
| Strength to Weight: Bending, points | 26 to 28 | |
| 20 to 27 |
| Thermal Diffusivity, mm2/s | 6.5 | |
| 3.5 |
| Thermal Shock Resistance, points | 31 to 34 | |
| 16 to 25 |
Alloy Composition
| Aluminum (Al), % | 0 to 0.020 | |
| 0 |
| Boron (B), % | 0 to 0.0015 | |
| 0 |
| Carbon (C), % | 0.17 to 0.23 | |
| 0 to 0.050 |
| Chromium (Cr), % | 10 to 11.5 | |
| 27 to 31 |
| Copper (Cu), % | 0 | |
| 0 to 0.5 |
| Iron (Fe), % | 84.5 to 88.3 | |
| 7.0 to 11 |
| Manganese (Mn), % | 0.4 to 0.9 | |
| 0 to 0.5 |
| Molybdenum (Mo), % | 0.5 to 0.8 | |
| 0 |
| Nickel (Ni), % | 0.2 to 0.6 | |
| 58 to 66 |
| Niobium (Nb), % | 0.25 to 0.55 | |
| 0 |
| Nitrogen (N), % | 0.050 to 0.1 | |
| 0 |
| Phosphorus (P), % | 0 to 0.025 | |
| 0 |
| Silicon (Si), % | 0 to 0.5 | |
| 0 to 0.5 |
| Sulfur (S), % | 0 to 0.015 | |
| 0 to 0.015 |
| Vanadium (V), % | 0.1 to 0.3 | |
| 0 |