Grade 21 Titanium vs. SAE-AISI 6150 Steel
Grade 21 titanium belongs to the titanium alloys classification, while SAE-AISI 6150 steel belongs to the iron alloys. There are 28 material properties with values for both materials. Properties with values for just one material (4, in this case) are not shown.
For each property being compared, the top bar is grade 21 titanium and the bottom bar is SAE-AISI 6150 steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 140 | |
| 190 |
| Elongation at Break, % | 9.0 to 17 | |
| 15 to 23 |
| Fatigue Strength, MPa | 550 to 660 | |
| 300 to 750 |
| Poisson's Ratio | 0.32 | |
| 0.29 |
| Shear Modulus, GPa | 51 | |
| 73 |
| Shear Strength, MPa | 550 to 790 | |
| 400 to 730 |
| Tensile Strength: Ultimate (UTS), MPa | 890 to 1340 | |
| 630 to 1200 |
| Tensile Strength: Yield (Proof), MPa | 870 to 1170 | |
| 420 to 1160 |
Thermal Properties
| Latent Heat of Fusion, J/g | 410 | |
| 250 |
| Maximum Temperature: Mechanical, °C | 310 | |
| 420 |
| Melting Completion (Liquidus), °C | 1740 | |
| 1460 |
| Melting Onset (Solidus), °C | 1690 | |
| 1410 |
| Specific Heat Capacity, J/kg-K | 500 | |
| 470 |
| Thermal Conductivity, W/m-K | 7.5 | |
| 46 |
| Thermal Expansion, µm/m-K | 7.1 | |
| 12 to 13 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 60 | |
| 2.3 |
| Density, g/cm3 | 5.4 | |
| 7.8 |
| Embodied Carbon, kg CO2/kg material | 32 | |
| 2.0 |
| Embodied Energy, MJ/kg | 490 | |
| 28 |
| Embodied Water, L/kg | 180 | |
| 51 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 110 to 180 | |
| 130 to 180 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 2760 to 5010 | |
| 460 to 3590 |
| Stiffness to Weight: Axial, points | 14 | |
| 13 |
| Stiffness to Weight: Bending, points | 32 | |
| 24 |
| Strength to Weight: Axial, points | 46 to 69 | |
| 22 to 43 |
| Strength to Weight: Bending, points | 38 to 50 | |
| 21 to 32 |
| Thermal Diffusivity, mm2/s | 2.8 | |
| 13 |
| Thermal Shock Resistance, points | 66 to 100 | |
| 20 to 38 |
Alloy Composition
| Aluminum (Al), % | 2.5 to 3.5 | |
| 0 |
| Carbon (C), % | 0 to 0.050 | |
| 0.48 to 0.53 |
| Chromium (Cr), % | 0 | |
| 0.8 to 1.1 |
| Hydrogen (H), % | 0 to 0.015 | |
| 0 |
| Iron (Fe), % | 0 to 0.4 | |
| 96.7 to 97.7 |
| Manganese (Mn), % | 0 | |
| 0.7 to 0.9 |
| Molybdenum (Mo), % | 14 to 16 | |
| 0 |
| Niobium (Nb), % | 2.2 to 3.2 | |
| 0 |
| Nitrogen (N), % | 0 to 0.030 | |
| 0 |
| Oxygen (O), % | 0 to 0.17 | |
| 0 |
| Phosphorus (P), % | 0 | |
| 0 to 0.035 |
| Silicon (Si), % | 0.15 to 0.25 | |
| 0.15 to 0.35 |
| Sulfur (S), % | 0 | |
| 0 to 0.040 |
| Titanium (Ti), % | 76 to 81.2 | |
| 0 |
| Vanadium (V), % | 0 | |
| 0.15 to 0.3 |
| Residuals, % | 0 to 0.4 | |
| 0 |