EN 1.0456 Steel vs. Grade C-6 Titanium
EN 1.0456 steel belongs to the iron alloys classification, while grade C-6 titanium belongs to the titanium alloys. There are 30 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 EN 1.0456 steel and the bottom bar is grade C-6 titanium.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 120 to 130 | |
| 290 |
| Elastic (Young's, Tensile) Modulus, GPa | 190 | |
| 100 |
| Elongation at Break, % | 24 to 26 | |
| 9.0 |
| Fatigue Strength, MPa | 210 to 220 | |
| 460 |
| Poisson's Ratio | 0.29 | |
| 0.32 |
| Shear Modulus, GPa | 73 | |
| 39 |
| Tensile Strength: Ultimate (UTS), MPa | 420 to 450 | |
| 890 |
| Tensile Strength: Yield (Proof), MPa | 290 to 300 | |
| 830 |
Thermal Properties
| Latent Heat of Fusion, J/g | 250 | |
| 410 |
| Maximum Temperature: Mechanical, °C | 400 | |
| 310 |
| Melting Completion (Liquidus), °C | 1460 | |
| 1580 |
| Melting Onset (Solidus), °C | 1420 | |
| 1530 |
| Specific Heat Capacity, J/kg-K | 470 | |
| 550 |
| Thermal Conductivity, W/m-K | 48 | |
| 7.8 |
| Thermal Expansion, µm/m-K | 12 | |
| 9.8 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 7.3 | |
| 1.2 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 8.4 | |
| 2.5 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 2.2 | |
| 36 |
| Density, g/cm3 | 7.8 | |
| 4.5 |
| Embodied Carbon, kg CO2/kg material | 1.5 | |
| 30 |
| Embodied Energy, MJ/kg | 20 | |
| 480 |
| Embodied Water, L/kg | 49 | |
| 190 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 93 to 99 | |
| 78 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 220 to 230 | |
| 3300 |
| Stiffness to Weight: Axial, points | 13 | |
| 13 |
| Stiffness to Weight: Bending, points | 24 | |
| 35 |
| Strength to Weight: Axial, points | 15 to 16 | |
| 55 |
| Strength to Weight: Bending, points | 16 to 17 | |
| 46 |
| Thermal Diffusivity, mm2/s | 13 | |
| 3.2 |
| Thermal Shock Resistance, points | 13 to 14 | |
| 63 |
Alloy Composition
| Aluminum (Al), % | 0.020 to 0.060 | |
| 4.0 to 6.0 |
| Carbon (C), % | 0 to 0.2 | |
| 0 to 0.1 |
| Chromium (Cr), % | 0 to 0.3 | |
| 0 |
| Copper (Cu), % | 0 to 0.35 | |
| 0 |
| Hydrogen (H), % | 0 | |
| 0 to 0.015 |
| Iron (Fe), % | 96.7 to 99.48 | |
| 0 to 0.5 |
| Manganese (Mn), % | 0.5 to 1.4 | |
| 0 |
| Molybdenum (Mo), % | 0 to 0.1 | |
| 0 |
| Nickel (Ni), % | 0 to 0.3 | |
| 0 to 0.050 |
| Niobium (Nb), % | 0 to 0.050 | |
| 0 |
| Nitrogen (N), % | 0 to 0.015 | |
| 0 |
| Oxygen (O), % | 0 | |
| 0 to 0.2 |
| Phosphorus (P), % | 0 to 0.035 | |
| 0 |
| Silicon (Si), % | 0 to 0.4 | |
| 0 |
| Sulfur (S), % | 0 to 0.030 | |
| 0 |
| Tin (Sn), % | 0 | |
| 2.0 to 3.0 |
| Titanium (Ti), % | 0 to 0.030 | |
| 89.7 to 94 |
| Vanadium (V), % | 0 to 0.050 | |
| 0 |
| Residuals, % | 0 | |
| 0 to 0.4 |