AISI 205 Stainless Steel vs. S36200 Stainless Steel
Both AISI 205 stainless steel and S36200 stainless steel are iron alloys. They have 81% of their average alloy composition in common. There are 28 material properties with values for both materials. Properties with values for just one material (6, in this case) are not shown.
For each property being compared, the top bar is AISI 205 stainless steel and the bottom bar is S36200 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 190 |
| Elongation at Break, % | 11 to 51 | |
| 3.4 to 4.6 |
| Fatigue Strength, MPa | 410 to 640 | |
| 450 to 570 |
| Poisson's Ratio | 0.28 | |
| 0.28 |
| Shear Modulus, GPa | 77 | |
| 76 |
| Shear Strength, MPa | 560 to 850 | |
| 680 to 810 |
| Tensile Strength: Ultimate (UTS), MPa | 800 to 1430 | |
| 1180 to 1410 |
| Tensile Strength: Yield (Proof), MPa | 450 to 1100 | |
| 960 to 1240 |
Thermal Properties
| Latent Heat of Fusion, J/g | 280 | |
| 280 |
| Maximum Temperature: Corrosion, °C | 410 | |
| 530 |
| Maximum Temperature: Mechanical, °C | 880 | |
| 820 |
| Melting Completion (Liquidus), °C | 1380 | |
| 1440 |
| Melting Onset (Solidus), °C | 1340 | |
| 1400 |
| Specific Heat Capacity, J/kg-K | 480 | |
| 480 |
| Thermal Expansion, µm/m-K | 18 | |
| 11 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 11 | |
| 12 |
| Density, g/cm3 | 7.6 | |
| 7.8 |
| Embodied Carbon, kg CO2/kg material | 2.6 | |
| 2.8 |
| Embodied Energy, MJ/kg | 37 | |
| 40 |
| Embodied Water, L/kg | 150 | |
| 120 |
Common Calculations
| PREN (Pitting Resistance) | 23 | |
| 15 |
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 150 to 430 | |
| 46 to 51 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 510 to 3060 | |
| 2380 to 3930 |
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 26 | |
| 25 |
| Strength to Weight: Axial, points | 29 to 52 | |
| 42 to 50 |
| Strength to Weight: Bending, points | 25 to 37 | |
| 32 to 36 |
| Thermal Shock Resistance, points | 16 to 29 | |
| 40 to 48 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 0 to 0.1 |
| Carbon (C), % | 0.12 to 0.25 | |
| 0 to 0.050 |
| Chromium (Cr), % | 16.5 to 18.5 | |
| 14 to 14.5 |
| Iron (Fe), % | 62.6 to 68.1 | |
| 75.4 to 79.5 |
| Manganese (Mn), % | 14 to 15.5 | |
| 0 to 0.5 |
| Molybdenum (Mo), % | 0 | |
| 0 to 0.3 |
| Nickel (Ni), % | 1.0 to 1.7 | |
| 6.5 to 7.0 |
| Nitrogen (N), % | 0.32 to 0.4 | |
| 0 |
| Phosphorus (P), % | 0 to 0.060 | |
| 0 to 0.030 |
| Silicon (Si), % | 0 to 1.0 | |
| 0 to 0.3 |
| Sulfur (S), % | 0 to 0.030 | |
| 0 to 0.030 |
| Titanium (Ti), % | 0 | |
| 0.6 to 0.9 |