AISI 205 Stainless Steel vs. Grade 20 Titanium
AISI 205 stainless steel belongs to the iron alloys classification, while grade 20 titanium belongs to the titanium alloys. There are 25 material properties with values for both materials. Properties with values for just one material (5, in this case) are not shown.
For each property being compared, the top bar is AISI 205 stainless steel and the bottom bar is grade 20 titanium.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 120 |
| Elongation at Break, % | 11 to 51 | |
| 5.7 to 17 |
| Fatigue Strength, MPa | 410 to 640 | |
| 550 to 630 |
| Poisson's Ratio | 0.28 | |
| 0.32 |
| Shear Modulus, GPa | 77 | |
| 47 |
| Shear Strength, MPa | 560 to 850 | |
| 560 to 740 |
| Tensile Strength: Ultimate (UTS), MPa | 800 to 1430 | |
| 900 to 1270 |
| Tensile Strength: Yield (Proof), MPa | 450 to 1100 | |
| 850 to 1190 |
Thermal Properties
| Latent Heat of Fusion, J/g | 280 | |
| 400 |
| Maximum Temperature: Mechanical, °C | 880 | |
| 370 |
| Melting Completion (Liquidus), °C | 1380 | |
| 1660 |
| Melting Onset (Solidus), °C | 1340 | |
| 1600 |
| Specific Heat Capacity, J/kg-K | 480 | |
| 520 |
| Thermal Expansion, µm/m-K | 18 | |
| 9.6 |
Otherwise Unclassified Properties
| Density, g/cm3 | 7.6 | |
| 5.0 |
| Embodied Carbon, kg CO2/kg material | 2.6 | |
| 52 |
| Embodied Energy, MJ/kg | 37 | |
| 860 |
| Embodied Water, L/kg | 150 | |
| 350 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 150 to 430 | |
| 71 to 150 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 510 to 3060 | |
| 2940 to 5760 |
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 26 | |
| 33 |
| Strength to Weight: Axial, points | 29 to 52 | |
| 50 to 70 |
| Strength to Weight: Bending, points | 25 to 37 | |
| 41 to 52 |
| Thermal Shock Resistance, points | 16 to 29 | |
| 55 to 77 |
Alloy Composition
Deprecated: Automatic conversion of false to array is deprecated in /home/public/compare.php on line 460
| Aluminum (Al), % | 0 | |
| 3.0 to 4.0 |
| Carbon (C), % | 0.12 to 0.25 | |
| 0 to 0.050 |
| Chromium (Cr), % | 16.5 to 18.5 | |
| 5.5 to 6.5 |
| Hydrogen (H), % | 0 | |
| 0 to 0.020 |
| Iron (Fe), % | 62.6 to 68.1 | |
| 0 to 0.3 |
| Manganese (Mn), % | 14 to 15.5 | |
| 0 |
| Molybdenum (Mo), % | 0 | |
| 3.5 to 4.5 |
| Nickel (Ni), % | 1.0 to 1.7 | |
| 0 |
| Nitrogen (N), % | 0.32 to 0.4 | |
| 0 to 0.030 |
| Oxygen (O), % | 0 | |
| 0 to 0.12 |
| Palladium (Pd), % | 0 | |
| 0.040 to 0.080 |
| Phosphorus (P), % | 0 to 0.060 | |
| 0 |
| Silicon (Si), % | 0 to 1.0 | |
| 0 |
| Sulfur (S), % | 0 to 0.030 | |
| 0 |
| Titanium (Ti), % | 0 | |
| 71 to 77 |
| Vanadium (V), % | 0 | |
| 7.5 to 8.5 |
| Zirconium (Zr), % | 0 | |
| 3.5 to 4.5 |
| Residuals, % | 0 | |
| 0 to 0.4 |