S36200 Stainless Steel vs. Grade 5 Titanium
S36200 stainless steel belongs to the iron alloys classification, while grade 5 titanium belongs to the titanium alloys. There are 31 material properties with values for both materials. Properties with values for just one material (3, in this case) are not shown.
For each property being compared, the top bar is S36200 stainless steel and the bottom bar is grade 5 titanium.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 190 | |
| 110 |
| Elongation at Break, % | 3.4 to 4.6 | |
| 8.6 to 11 |
| Fatigue Strength, MPa | 450 to 570 | |
| 530 to 630 |
| Poisson's Ratio | 0.28 | |
| 0.32 |
| Rockwell C Hardness | 25 to 33 | |
| 33 |
| Shear Modulus, GPa | 76 | |
| 40 |
| Shear Strength, MPa | 680 to 810 | |
| 600 to 710 |
| Tensile Strength: Ultimate (UTS), MPa | 1180 to 1410 | |
| 1000 to 1190 |
| Tensile Strength: Yield (Proof), MPa | 960 to 1240 | |
| 910 to 1110 |
Thermal Properties
| Latent Heat of Fusion, J/g | 280 | |
| 410 |
| Maximum Temperature: Mechanical, °C | 820 | |
| 330 |
| Melting Completion (Liquidus), °C | 1440 | |
| 1610 |
| Melting Onset (Solidus), °C | 1400 | |
| 1650 |
| Specific Heat Capacity, J/kg-K | 480 | |
| 560 |
| Thermal Conductivity, W/m-K | 16 | |
| 6.8 |
| Thermal Expansion, µm/m-K | 11 | |
| 8.9 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 2.3 | |
| 1.0 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 2.6 | |
| 2.0 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 12 | |
| 36 |
| Density, g/cm3 | 7.8 | |
| 4.4 |
| Embodied Carbon, kg CO2/kg material | 2.8 | |
| 38 |
| Embodied Energy, MJ/kg | 40 | |
| 610 |
| Embodied Water, L/kg | 120 | |
| 200 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 46 to 51 | |
| 100 to 110 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 2380 to 3930 | |
| 3980 to 5880 |
| Stiffness to Weight: Axial, points | 14 | |
| 13 |
| Stiffness to Weight: Bending, points | 25 | |
| 35 |
| Strength to Weight: Axial, points | 42 to 50 | |
| 62 to 75 |
| Strength to Weight: Bending, points | 32 to 36 | |
| 50 to 56 |
| Thermal Diffusivity, mm2/s | 4.3 | |
| 2.7 |
| Thermal Shock Resistance, points | 40 to 48 | |
| 76 to 91 |
Alloy Composition
| Aluminum (Al), % | 0 to 0.1 | |
| 5.5 to 6.8 |
| Carbon (C), % | 0 to 0.050 | |
| 0 to 0.080 |
| 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 | |
| 0 |
| Nickel (Ni), % | 6.5 to 7.0 | |
| 0 |
| Nitrogen (N), % | 0 | |
| 0 to 0.050 |
| Oxygen (O), % | 0 | |
| 0 to 0.2 |
| Phosphorus (P), % | 0 to 0.030 | |
| 0 |
| Silicon (Si), % | 0 to 0.3 | |
| 0 |
| Sulfur (S), % | 0 to 0.030 | |
| 0 |
| Titanium (Ti), % | 0.6 to 0.9 | |
| 87.4 to 91 |
| Vanadium (V), % | 0 | |
| 3.5 to 4.5 |
| Yttrium (Y), % | 0 | |
| 0 to 0.0050 |
| Residuals, % | 0 | |
| 0 to 0.4 |