S36200 Stainless Steel vs. Grade 21 Titanium
S36200 stainless steel belongs to the iron alloys classification, while grade 21 titanium belongs to the titanium alloys. 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 S36200 stainless steel and the bottom bar is grade 21 titanium.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 190 | |
| 140 |
| Elongation at Break, % | 3.4 to 4.6 | |
| 9.0 to 17 |
| Fatigue Strength, MPa | 450 to 570 | |
| 550 to 660 |
| Poisson's Ratio | 0.28 | |
| 0.32 |
| Shear Modulus, GPa | 76 | |
| 51 |
| Shear Strength, MPa | 680 to 810 | |
| 550 to 790 |
| Tensile Strength: Ultimate (UTS), MPa | 1180 to 1410 | |
| 890 to 1340 |
| Tensile Strength: Yield (Proof), MPa | 960 to 1240 | |
| 870 to 1170 |
Thermal Properties
| Latent Heat of Fusion, J/g | 280 | |
| 410 |
| Maximum Temperature: Mechanical, °C | 820 | |
| 310 |
| Melting Completion (Liquidus), °C | 1440 | |
| 1740 |
| Melting Onset (Solidus), °C | 1400 | |
| 1690 |
| Specific Heat Capacity, J/kg-K | 480 | |
| 500 |
| Thermal Conductivity, W/m-K | 16 | |
| 7.5 |
| Thermal Expansion, µm/m-K | 11 | |
| 7.1 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 12 | |
| 60 |
| Density, g/cm3 | 7.8 | |
| 5.4 |
| Embodied Carbon, kg CO2/kg material | 2.8 | |
| 32 |
| Embodied Energy, MJ/kg | 40 | |
| 490 |
| Embodied Water, L/kg | 120 | |
| 180 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 46 to 51 | |
| 110 to 180 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 2380 to 3930 | |
| 2760 to 5010 |
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 25 | |
| 32 |
| Strength to Weight: Axial, points | 42 to 50 | |
| 46 to 69 |
| Strength to Weight: Bending, points | 32 to 36 | |
| 38 to 50 |
| Thermal Diffusivity, mm2/s | 4.3 | |
| 2.8 |
| Thermal Shock Resistance, points | 40 to 48 | |
| 66 to 100 |
Alloy Composition
| Aluminum (Al), % | 0 to 0.1 | |
| 2.5 to 3.5 |
| Carbon (C), % | 0 to 0.050 | |
| 0 to 0.050 |
| Chromium (Cr), % | 14 to 14.5 | |
| 0 |
| Hydrogen (H), % | 0 | |
| 0 to 0.015 |
| Iron (Fe), % | 75.4 to 79.5 | |
| 0 to 0.4 |
| Manganese (Mn), % | 0 to 0.5 | |
| 0 |
| Molybdenum (Mo), % | 0 to 0.3 | |
| 14 to 16 |
| Nickel (Ni), % | 6.5 to 7.0 | |
| 0 |
| Niobium (Nb), % | 0 | |
| 2.2 to 3.2 |
| Nitrogen (N), % | 0 | |
| 0 to 0.030 |
| Oxygen (O), % | 0 | |
| 0 to 0.17 |
| Phosphorus (P), % | 0 to 0.030 | |
| 0 |
| Silicon (Si), % | 0 to 0.3 | |
| 0.15 to 0.25 |
| Sulfur (S), % | 0 to 0.030 | |
| 0 |
| Titanium (Ti), % | 0.6 to 0.9 | |
| 76 to 81.2 |
| Residuals, % | 0 | |
| 0 to 0.4 |