ASTM B522 Class I vs. Grade 29 Titanium
ASTM B522 class I belongs to the otherwise unclassified metals classification, while grade 29 titanium belongs to the titanium alloys. There are 22 material properties with values for both materials. Properties with values for just one material (10, 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 ASTM B522 class I and the bottom bar is grade 29 titanium.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 96 | |
| 110 |
| Elongation at Break, % | 1.1 to 29 | |
| 6.8 to 11 |
| Poisson's Ratio | 0.41 | |
| 0.32 |
| Shear Modulus, GPa | 34 | |
| 40 |
| Shear Strength, MPa | 180 to 280 | |
| 550 to 560 |
| Tensile Strength: Ultimate (UTS), MPa | 280 to 490 | |
| 930 to 940 |
| Tensile Strength: Yield (Proof), MPa | 120 to 210 | |
| 850 to 870 |
Thermal Properties
| Latent Heat of Fusion, J/g | 77 | |
| 410 |
| Melting Completion (Liquidus), °C | 1030 | |
| 1610 |
| Melting Onset (Solidus), °C | 1030 | |
| 1560 |
| Specific Heat Capacity, J/kg-K | 160 | |
| 560 |
| Thermal Expansion, µm/m-K | 15 | |
| 9.3 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 11 | |
| 1.0 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 5.8 | |
| 2.0 |
Otherwise Unclassified Properties
| Density, g/cm3 | 17 | |
| 4.5 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 4.5 to 64 | |
| 62 to 100 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 75 to 230 | |
| 3420 to 3540 |
| Stiffness to Weight: Axial, points | 3.1 | |
| 13 |
| Stiffness to Weight: Bending, points | 8.9 | |
| 35 |
| Strength to Weight: Axial, points | 4.4 to 7.8 | |
| 58 to 59 |
| Strength to Weight: Bending, points | 5.5 to 8.0 | |
| 47 to 48 |
| Thermal Shock Resistance, points | 13 to 24 | |
| 68 to 69 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 5.5 to 6.5 |
| Carbon (C), % | 0 | |
| 0 to 0.080 |
| Gold (Au), % | 68 to 70 | |
| 0 |
| Hydrogen (H), % | 0 | |
| 0 to 0.015 |
| Iron (Fe), % | 0 | |
| 0 to 0.25 |
| Nitrogen (N), % | 0 | |
| 0 to 0.030 |
| Oxygen (O), % | 0 | |
| 0 to 0.13 |
| Platinum (Pt), % | 5.0 to 7.0 | |
| 0 |
| Ruthenium (Ru), % | 0 | |
| 0.080 to 0.14 |
| Silver (Ag), % | 23.5 to 26.5 | |
| 0 |
| Titanium (Ti), % | 0 | |
| 88 to 90.9 |
| Vanadium (V), % | 0 | |
| 3.5 to 4.5 |
| Residuals, % | 0 | |
| 0 to 0.4 |