EN 1.1158 Steel vs. Grade 16 Titanium
EN 1.1158 steel belongs to the iron alloys classification, while grade 16 titanium belongs to the titanium alloys. There are 29 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 EN 1.1158 steel and the bottom bar is grade 16 titanium.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 190 | |
| 110 |
| Elongation at Break, % | 23 to 24 | |
| 23 |
| Fatigue Strength, MPa | 170 to 220 | |
| 240 |
| Poisson's Ratio | 0.29 | |
| 0.32 |
| Shear Modulus, GPa | 73 | |
| 38 |
| Shear Strength, MPa | 300 to 320 | |
| 250 |
| Tensile Strength: Ultimate (UTS), MPa | 470 to 500 | |
| 400 |
| Tensile Strength: Yield (Proof), MPa | 240 to 310 | |
| 340 |
Thermal Properties
| Latent Heat of Fusion, J/g | 250 | |
| 420 |
| Maximum Temperature: Mechanical, °C | 400 | |
| 320 |
| Melting Completion (Liquidus), °C | 1460 | |
| 1660 |
| Melting Onset (Solidus), °C | 1420 | |
| 1610 |
| Specific Heat Capacity, J/kg-K | 470 | |
| 540 |
| Thermal Conductivity, W/m-K | 49 | |
| 22 |
| Thermal Expansion, µm/m-K | 12 | |
| 9.2 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 7.2 | |
| 3.6 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 8.2 | |
| 7.2 |
Otherwise Unclassified Properties
| Density, g/cm3 | 7.8 | |
| 4.5 |
| Embodied Carbon, kg CO2/kg material | 1.4 | |
| 36 |
| Embodied Energy, MJ/kg | 19 | |
| 600 |
| Embodied Water, L/kg | 47 | |
| 230 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 89 to 110 | |
| 86 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 150 to 250 | |
| 550 |
| Stiffness to Weight: Axial, points | 13 | |
| 13 |
| Stiffness to Weight: Bending, points | 24 | |
| 35 |
| Strength to Weight: Axial, points | 17 to 18 | |
| 25 |
| Strength to Weight: Bending, points | 17 to 18 | |
| 27 |
| Thermal Diffusivity, mm2/s | 13 | |
| 8.9 |
| Thermal Shock Resistance, points | 15 to 16 | |
| 29 |
Alloy Composition
| Carbon (C), % | 0.22 to 0.29 | |
| 0 to 0.080 |
| Chromium (Cr), % | 0 to 0.4 | |
| 0 |
| Hydrogen (H), % | 0 | |
| 0 to 0.015 |
| Iron (Fe), % | 97.6 to 99.38 | |
| 0 to 0.3 |
| Manganese (Mn), % | 0.4 to 0.7 | |
| 0 |
| Molybdenum (Mo), % | 0 to 0.1 | |
| 0 |
| Nickel (Ni), % | 0 to 0.4 | |
| 0 |
| Nitrogen (N), % | 0 | |
| 0 to 0.030 |
| Oxygen (O), % | 0 | |
| 0 to 0.25 |
| Palladium (Pd), % | 0 | |
| 0.040 to 0.080 |
| Phosphorus (P), % | 0 to 0.035 | |
| 0 |
| Silicon (Si), % | 0 to 0.4 | |
| 0 |
| Sulfur (S), % | 0 to 0.035 | |
| 0 |
| Titanium (Ti), % | 0 | |
| 98.8 to 99.96 |
| Residuals, % | 0 | |
| 0 to 0.4 |