EN 1.4869 Casting Alloy vs. Grade 19 Titanium
EN 1.4869 casting alloy belongs to the nickel alloys classification, while grade 19 titanium belongs to the titanium alloys. There are 27 material properties with values for both materials. Properties with values for just one material (2, in this case) are not shown.
For each property being compared, the top bar is EN 1.4869 casting alloy and the bottom bar is grade 19 titanium.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 210 | |
| 120 |
| Elongation at Break, % | 5.7 | |
| 5.6 to 17 |
| Fatigue Strength, MPa | 130 | |
| 550 to 620 |
| Poisson's Ratio | 0.28 | |
| 0.32 |
| Shear Modulus, GPa | 80 | |
| 47 |
| Tensile Strength: Ultimate (UTS), MPa | 540 | |
| 890 to 1300 |
| Tensile Strength: Yield (Proof), MPa | 310 | |
| 870 to 1170 |
Thermal Properties
| Latent Heat of Fusion, J/g | 330 | |
| 400 |
| Maximum Temperature: Mechanical, °C | 1200 | |
| 370 |
| Melting Completion (Liquidus), °C | 1450 | |
| 1660 |
| Melting Onset (Solidus), °C | 1390 | |
| 1600 |
| Specific Heat Capacity, J/kg-K | 460 | |
| 520 |
| Thermal Conductivity, W/m-K | 10 | |
| 6.2 |
| Thermal Expansion, µm/m-K | 13 | |
| 9.1 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 70 | |
| 45 |
| Density, g/cm3 | 8.5 | |
| 5.0 |
| Embodied Carbon, kg CO2/kg material | 7.7 | |
| 47 |
| Embodied Energy, MJ/kg | 110 | |
| 760 |
| Embodied Water, L/kg | 300 | |
| 230 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 26 | |
| 70 to 150 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 230 | |
| 3040 to 5530 |
| Stiffness to Weight: Axial, points | 13 | |
| 14 |
| Stiffness to Weight: Bending, points | 23 | |
| 33 |
| Strength to Weight: Axial, points | 18 | |
| 49 to 72 |
| Strength to Weight: Bending, points | 17 | |
| 41 to 53 |
| Thermal Diffusivity, mm2/s | 2.6 | |
| 2.4 |
| Thermal Shock Resistance, points | 14 | |
| 57 to 83 |
Alloy Composition
Deprecated: Automatic conversion of false to array is deprecated in /home/public/compare.php on line 460
| Aluminum (Al), % | 0 | |
| 3.0 to 4.0 |
| Carbon (C), % | 0.45 to 0.55 | |
| 0 to 0.050 |
| Chromium (Cr), % | 24 to 26 | |
| 5.5 to 6.5 |
| Cobalt (Co), % | 14 to 16 | |
| 0 |
| Hydrogen (H), % | 0 | |
| 0 to 0.020 |
| Iron (Fe), % | 11.4 to 23.6 | |
| 0 to 0.3 |
| Manganese (Mn), % | 0 to 1.0 | |
| 0 |
| Molybdenum (Mo), % | 0 | |
| 3.5 to 4.5 |
| Nickel (Ni), % | 33 to 37 | |
| 0 |
| Nitrogen (N), % | 0 | |
| 0 to 0.030 |
| Oxygen (O), % | 0 | |
| 0 to 0.12 |
| Phosphorus (P), % | 0 to 0.040 | |
| 0 |
| Silicon (Si), % | 1.0 to 2.0 | |
| 0 |
| Sulfur (S), % | 0 to 0.030 | |
| 0 |
| Titanium (Ti), % | 0 | |
| 71.1 to 77 |
| Tungsten (W), % | 4.0 to 6.0 | |
| 0 |
| Vanadium (V), % | 0 | |
| 7.5 to 8.5 |
| Zirconium (Zr), % | 0 | |
| 3.5 to 4.5 |
| Residuals, % | 0 | |
| 0 to 0.4 |