S36200 Stainless Steel vs. S45500 Stainless Steel
Both S36200 stainless steel and S45500 stainless steel are iron alloys. They have a very high 95% of their average alloy composition in common. There are 28 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 S36200 stainless steel and the bottom bar is S45500 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 190 | |
| 190 |
| Elongation at Break, % | 3.4 to 4.6 | |
| 3.4 to 11 |
| Fatigue Strength, MPa | 450 to 570 | |
| 570 to 890 |
| Poisson's Ratio | 0.28 | |
| 0.28 |
| Rockwell C Hardness | 25 to 33 | |
| 32 to 54 |
| Shear Modulus, GPa | 76 | |
| 75 |
| Shear Strength, MPa | 680 to 810 | |
| 790 to 1090 |
| Tensile Strength: Ultimate (UTS), MPa | 1180 to 1410 | |
| 1370 to 1850 |
| Tensile Strength: Yield (Proof), MPa | 960 to 1240 | |
| 1240 to 1700 |
Thermal Properties
| Latent Heat of Fusion, J/g | 280 | |
| 270 |
| Maximum Temperature: Corrosion, °C | 530 | |
| 620 |
| Maximum Temperature: Mechanical, °C | 820 | |
| 760 |
| Melting Completion (Liquidus), °C | 1440 | |
| 1440 |
| Melting Onset (Solidus), °C | 1400 | |
| 1400 |
| Specific Heat Capacity, J/kg-K | 480 | |
| 470 |
| Thermal Expansion, µm/m-K | 11 | |
| 11 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 12 | |
| 17 |
| Density, g/cm3 | 7.8 | |
| 7.9 |
| Embodied Carbon, kg CO2/kg material | 2.8 | |
| 3.8 |
| Embodied Energy, MJ/kg | 40 | |
| 57 |
| Embodied Water, L/kg | 120 | |
| 120 |
Common Calculations
| PREN (Pitting Resistance) | 15 | |
| 13 |
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 46 to 51 | |
| 45 to 190 |
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 25 | |
| 24 |
| Strength to Weight: Axial, points | 42 to 50 | |
| 48 to 65 |
| Strength to Weight: Bending, points | 32 to 36 | |
| 35 to 42 |
| Thermal Shock Resistance, points | 40 to 48 | |
| 48 to 64 |
Alloy Composition
| Aluminum (Al), % | 0 to 0.1 | |
| 0 |
| Carbon (C), % | 0 to 0.050 | |
| 0 to 0.050 |
| Chromium (Cr), % | 14 to 14.5 | |
| 11 to 12.5 |
| Copper (Cu), % | 0 | |
| 1.5 to 2.5 |
| Iron (Fe), % | 75.4 to 79.5 | |
| 71.5 to 79.2 |
| Manganese (Mn), % | 0 to 0.5 | |
| 0 to 0.5 |
| Molybdenum (Mo), % | 0 to 0.3 | |
| 0 to 0.5 |
| Nickel (Ni), % | 6.5 to 7.0 | |
| 7.5 to 9.5 |
| Niobium (Nb), % | 0 | |
| 0 to 0.5 |
| Phosphorus (P), % | 0 to 0.030 | |
| 0 to 0.040 |
| Silicon (Si), % | 0 to 0.3 | |
| 0 to 0.5 |
| Sulfur (S), % | 0 to 0.030 | |
| 0 to 0.030 |
| Tantalum (Ta), % | 0 | |
| 0 to 0.5 |
| Titanium (Ti), % | 0.6 to 0.9 | |
| 0.8 to 1.4 |