Grade 23 Titanium vs. S35500 Stainless Steel
Grade 23 titanium belongs to the titanium alloys classification, while S35500 stainless steel belongs to the iron 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 grade 23 titanium and the bottom bar is S35500 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 110 | |
| 200 |
| Elongation at Break, % | 6.7 to 11 | |
| 14 |
| Fatigue Strength, MPa | 470 to 500 | |
| 690 to 730 |
| Poisson's Ratio | 0.32 | |
| 0.28 |
| Rockwell C Hardness | 32 | |
| 33 to 42 |
| Shear Modulus, GPa | 40 | |
| 78 |
| Shear Strength, MPa | 540 to 570 | |
| 810 to 910 |
| Tensile Strength: Ultimate (UTS), MPa | 930 to 940 | |
| 1330 to 1490 |
| Tensile Strength: Yield (Proof), MPa | 850 to 870 | |
| 1200 to 1280 |
Thermal Properties
| Latent Heat of Fusion, J/g | 410 | |
| 280 |
| Maximum Temperature: Mechanical, °C | 340 | |
| 870 |
| Melting Completion (Liquidus), °C | 1610 | |
| 1460 |
| Melting Onset (Solidus), °C | 1560 | |
| 1420 |
| Specific Heat Capacity, J/kg-K | 560 | |
| 470 |
| Thermal Conductivity, W/m-K | 7.1 | |
| 16 |
| Thermal Expansion, µm/m-K | 9.4 | |
| 11 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 1.0 | |
| 2.2 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 2.0 | |
| 2.5 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 36 | |
| 16 |
| Density, g/cm3 | 4.4 | |
| 7.8 |
| Embodied Carbon, kg CO2/kg material | 38 | |
| 3.5 |
| Embodied Energy, MJ/kg | 610 | |
| 47 |
| Embodied Water, L/kg | 200 | |
| 130 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 61 to 100 | |
| 180 to 190 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 3430 to 3560 | |
| 3610 to 4100 |
| Stiffness to Weight: Axial, points | 13 | |
| 14 |
| Stiffness to Weight: Bending, points | 35 | |
| 25 |
| Strength to Weight: Axial, points | 58 to 59 | |
| 47 to 53 |
| Strength to Weight: Bending, points | 48 | |
| 34 to 37 |
| Thermal Diffusivity, mm2/s | 2.9 | |
| 4.4 |
| Thermal Shock Resistance, points | 67 to 68 | |
| 44 to 49 |
Alloy Composition
| Aluminum (Al), % | 5.5 to 6.5 | |
| 0 |
| Carbon (C), % | 0 to 0.080 | |
| 0.1 to 0.15 |
| Chromium (Cr), % | 0 | |
| 15 to 16 |
| Hydrogen (H), % | 0 to 0.013 | |
| 0 |
| Iron (Fe), % | 0 to 0.25 | |
| 73.2 to 77.7 |
| Manganese (Mn), % | 0 | |
| 0.5 to 1.3 |
| Molybdenum (Mo), % | 0 | |
| 2.5 to 3.2 |
| Nickel (Ni), % | 0 | |
| 4.0 to 5.0 |
| Niobium (Nb), % | 0 | |
| 0.1 to 0.5 |
| Nitrogen (N), % | 0 to 0.030 | |
| 0.070 to 0.13 |
| Oxygen (O), % | 0 to 0.13 | |
| 0 |
| Phosphorus (P), % | 0 | |
| 0 to 0.040 |
| Silicon (Si), % | 0 | |
| 0 to 0.5 |
| Sulfur (S), % | 0 | |
| 0 to 0.030 |
| Titanium (Ti), % | 88.1 to 91 | |
| 0 |
| Vanadium (V), % | 3.5 to 4.5 | |
| 0 |
| Residuals, % | 0 to 0.4 | |
| 0 |