AWS E320LR vs. Nickel 890
AWS E320LR belongs to the iron alloys classification, while nickel 890 belongs to the nickel alloys. They have 83% of their average alloy composition in common. There are 20 material properties with values for both materials. Properties with values for just one material (7, in this case) are not shown.
For each property being compared, the top bar is AWS E320LR and the bottom bar is nickel 890.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 200 |
| Elongation at Break, % | 34 | |
| 39 |
| Poisson's Ratio | 0.28 | |
| 0.28 |
| Shear Modulus, GPa | 77 | |
| 78 |
| Tensile Strength: Ultimate (UTS), MPa | 580 | |
| 590 |
Thermal Properties
| Latent Heat of Fusion, J/g | 300 | |
| 330 |
| Melting Completion (Liquidus), °C | 1410 | |
| 1390 |
| Melting Onset (Solidus), °C | 1360 | |
| 1340 |
| Specific Heat Capacity, J/kg-K | 460 | |
| 480 |
| Thermal Expansion, µm/m-K | 14 | |
| 14 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 36 | |
| 47 |
| Density, g/cm3 | 8.2 | |
| 8.1 |
| Embodied Carbon, kg CO2/kg material | 6.2 | |
| 8.2 |
| Embodied Energy, MJ/kg | 87 | |
| 120 |
| Embodied Water, L/kg | 220 | |
| 250 |
Common Calculations
| Stiffness to Weight: Axial, points | 13 | |
| 14 |
| Stiffness to Weight: Bending, points | 24 | |
| 24 |
| Strength to Weight: Axial, points | 20 | |
| 20 |
| Strength to Weight: Bending, points | 19 | |
| 19 |
| Thermal Shock Resistance, points | 15 | |
| 15 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 0.050 to 0.6 |
| Carbon (C), % | 0 to 0.030 | |
| 0.060 to 0.14 |
| Chromium (Cr), % | 19 to 21 | |
| 23.5 to 28.5 |
| Copper (Cu), % | 3.0 to 4.0 | |
| 0 to 0.75 |
| Iron (Fe), % | 32.7 to 42.5 | |
| 17.3 to 33.9 |
| Manganese (Mn), % | 1.5 to 2.5 | |
| 0 to 1.5 |
| Molybdenum (Mo), % | 2.0 to 3.0 | |
| 1.0 to 2.0 |
| Nickel (Ni), % | 32 to 36 | |
| 40 to 45 |
| Niobium (Nb), % | 0 to 0.4 | |
| 0.2 to 1.0 |
| Phosphorus (P), % | 0 to 0.020 | |
| 0 |
| Silicon (Si), % | 0 to 0.3 | |
| 1.0 to 2.0 |
| Sulfur (S), % | 0 to 0.015 | |
| 0 to 0.015 |
| Tantalum (Ta), % | 0 | |
| 0.1 to 0.6 |
| Titanium (Ti), % | 0 | |
| 0.15 to 0.6 |