R05252 Alloy vs. Grade 19 Titanium
R05252 alloy belongs to the otherwise unclassified metals classification, while grade 19 titanium belongs to the titanium alloys. There are 18 material properties with values for both materials. Properties with values for just one material (11, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.
For each property being compared, the top bar is R05252 alloy and the bottom bar is grade 19 titanium.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 120 |
| Elongation at Break, % | 23 | |
| 5.6 to 17 |
| Poisson's Ratio | 0.33 | |
| 0.32 |
| Shear Modulus, GPa | 73 | |
| 47 |
| Tensile Strength: Ultimate (UTS), MPa | 310 | |
| 890 to 1300 |
| Tensile Strength: Yield (Proof), MPa | 220 | |
| 870 to 1170 |
Thermal Properties
| Latent Heat of Fusion, J/g | 140 | |
| 400 |
| Specific Heat Capacity, J/kg-K | 140 | |
| 520 |
| Thermal Expansion, µm/m-K | 6.7 | |
| 9.1 |
Otherwise Unclassified Properties
| Density, g/cm3 | 17 | |
| 5.0 |
| Embodied Water, L/kg | 600 | |
| 230 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 63 | |
| 70 to 150 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 120 | |
| 3040 to 5530 |
| Stiffness to Weight: Axial, points | 6.5 | |
| 14 |
| Stiffness to Weight: Bending, points | 12 | |
| 33 |
| Strength to Weight: Axial, points | 5.2 | |
| 49 to 72 |
| Strength to Weight: Bending, points | 6.1 | |
| 41 to 53 |
| Thermal Shock Resistance, points | 17 | |
| 57 to 83 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 3.0 to 4.0 |
| Carbon (C), % | 0 to 0.010 | |
| 0 to 0.050 |
| Chromium (Cr), % | 0 | |
| 5.5 to 6.5 |
| Hydrogen (H), % | 0 to 0.0015 | |
| 0 to 0.020 |
| Iron (Fe), % | 0 to 0.010 | |
| 0 to 0.3 |
| Molybdenum (Mo), % | 0 to 0.020 | |
| 3.5 to 4.5 |
| Nickel (Ni), % | 0 to 0.010 | |
| 0 |
| Niobium (Nb), % | 0 to 0.1 | |
| 0 |
| Nitrogen (N), % | 0 to 0.010 | |
| 0 to 0.030 |
| Oxygen (O), % | 0 to 0.015 | |
| 0 to 0.12 |
| Silicon (Si), % | 0 to 0.0050 | |
| 0 |
| Tantalum (Ta), % | 88.8 to 91 | |
| 0 |
| Titanium (Ti), % | 0 to 0.010 | |
| 71.1 to 77 |
| Tungsten (W), % | 9.0 to 11 | |
| 0 |
| Vanadium (V), % | 0 | |
| 7.5 to 8.5 |
| Zirconium (Zr), % | 0 | |
| 3.5 to 4.5 |
| Residuals, % | 0 | |
| 0 to 0.4 |