Annealed SAE-AISI M62 vs. Annealed Nickel 600
Annealed SAE-AISI M62 belongs to the iron alloys classification, while annealed nickel 600 belongs to the nickel alloys. There are 19 material properties with values for both materials. Properties with values for just one material (15, in this case) are not shown.
For each property being compared, the top bar is annealed SAE-AISI M62 and the bottom bar is annealed nickel 600.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 190 |
| Poisson's Ratio | 0.29 | |
| 0.29 |
| Shear Modulus, GPa | 79 | |
| 75 |
| Tensile Strength: Ultimate (UTS), MPa | 830 | |
| 650 |
Thermal Properties
| Latent Heat of Fusion, J/g | 260 | |
| 310 |
| Melting Completion (Liquidus), °C | 1650 | |
| 1410 |
| Melting Onset (Solidus), °C | 1600 | |
| 1350 |
| Specific Heat Capacity, J/kg-K | 430 | |
| 460 |
| Thermal Expansion, µm/m-K | 12 | |
| 13 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 30 | |
| 55 |
| Density, g/cm3 | 8.5 | |
| 8.5 |
| Embodied Carbon, kg CO2/kg material | 10 | |
| 9.0 |
| Embodied Energy, MJ/kg | 150 | |
| 130 |
| Embodied Water, L/kg | 110 | |
| 250 |
Common Calculations
| Stiffness to Weight: Axial, points | 13 | |
| 13 |
| Stiffness to Weight: Bending, points | 23 | |
| 23 |
| Strength to Weight: Axial, points | 27 | |
| 21 |
| Strength to Weight: Bending, points | 23 | |
| 20 |
| Thermal Shock Resistance, points | 24 | |
| 19 |
Alloy Composition
| Carbon (C), % | 1.3 to 1.4 | |
| 0 to 0.15 |
| Chromium (Cr), % | 3.5 to 4.0 | |
| 14 to 17 |
| Copper (Cu), % | 0 to 0.25 | |
| 0 to 0.5 |
| Iron (Fe), % | 73.6 to 77.4 | |
| 6.0 to 10 |
| Manganese (Mn), % | 0.15 to 0.4 | |
| 0 to 1.0 |
| Molybdenum (Mo), % | 10 to 11 | |
| 0 |
| Nickel (Ni), % | 0 to 0.3 | |
| 72 to 80 |
| Phosphorus (P), % | 0 to 0.030 | |
| 0 |
| Silicon (Si), % | 0.15 to 0.4 | |
| 0 to 0.5 |
| Sulfur (S), % | 0 to 0.030 | |
| 0 to 0.015 |
| Tungsten (W), % | 5.8 to 6.5 | |
| 0 |
| Vanadium (V), % | 1.8 to 2.1 | |
| 0 |