Grade 21 Titanium vs. EN 1.0434 Steel
Grade 21 titanium belongs to the titanium alloys classification, while EN 1.0434 steel belongs to the iron alloys. There are 29 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 21 titanium and the bottom bar is EN 1.0434 steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 140 | |
| 190 |
| Elongation at Break, % | 9.0 to 17 | |
| 12 to 28 |
| Fatigue Strength, MPa | 550 to 660 | |
| 190 to 300 |
| Poisson's Ratio | 0.32 | |
| 0.29 |
| Reduction in Area, % | 22 | |
| 64 to 74 |
| Shear Modulus, GPa | 51 | |
| 73 |
| Shear Strength, MPa | 550 to 790 | |
| 280 to 330 |
| Tensile Strength: Ultimate (UTS), MPa | 890 to 1340 | |
| 390 to 540 |
| Tensile Strength: Yield (Proof), MPa | 870 to 1170 | |
| 250 to 450 |
Thermal Properties
| Latent Heat of Fusion, J/g | 410 | |
| 250 |
| Maximum Temperature: Mechanical, °C | 310 | |
| 400 |
| Melting Completion (Liquidus), °C | 1740 | |
| 1460 |
| Melting Onset (Solidus), °C | 1690 | |
| 1420 |
| Specific Heat Capacity, J/kg-K | 500 | |
| 470 |
| Thermal Conductivity, W/m-K | 7.5 | |
| 52 |
| Thermal Expansion, µm/m-K | 7.1 | |
| 12 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 60 | |
| 1.8 |
| Density, g/cm3 | 5.4 | |
| 7.9 |
| Embodied Carbon, kg CO2/kg material | 32 | |
| 1.4 |
| Embodied Energy, MJ/kg | 490 | |
| 18 |
| Embodied Water, L/kg | 180 | |
| 46 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 110 to 180 | |
| 39 to 140 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 2760 to 5010 | |
| 170 to 540 |
| Stiffness to Weight: Axial, points | 14 | |
| 13 |
| Stiffness to Weight: Bending, points | 32 | |
| 24 |
| Strength to Weight: Axial, points | 46 to 69 | |
| 14 to 19 |
| Strength to Weight: Bending, points | 38 to 50 | |
| 15 to 19 |
| Thermal Diffusivity, mm2/s | 2.8 | |
| 14 |
| Thermal Shock Resistance, points | 66 to 100 | |
| 12 to 17 |
Alloy Composition
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| Aluminum (Al), % | 2.5 to 3.5 | |
| 0.020 to 0.060 |
| Carbon (C), % | 0 to 0.050 | |
| 0.15 to 0.19 |
| Hydrogen (H), % | 0 to 0.015 | |
| 0 |
| Iron (Fe), % | 0 to 0.4 | |
| 98.8 to 99.18 |
| Manganese (Mn), % | 0 | |
| 0.65 to 0.85 |
| 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 0.025 |
| Silicon (Si), % | 0.15 to 0.25 | |
| 0 to 0.1 |
| Sulfur (S), % | 0 | |
| 0 to 0.025 |
| Titanium (Ti), % | 76 to 81.2 | |
| 0 |
| Residuals, % | 0 to 0.4 | |
| 0 |