R58150 Titanium vs. 6101 Aluminum
R58150 titanium belongs to the titanium alloys classification, while 6101 aluminum belongs to the aluminum alloys. There are 17 material properties with values for both materials. Properties with values for just one material (14, in this case) are not shown.
For each property being compared, the top bar is R58150 titanium and the bottom bar is 6101 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 140 | |
| 68 |
| Elongation at Break, % | 13 | |
| 10 to 25 |
| Poisson's Ratio | 0.32 | |
| 0.33 |
| Shear Modulus, GPa | 52 | |
| 26 |
Thermal Properties
| Latent Heat of Fusion, J/g | 410 | |
| 400 |
| Maximum Temperature: Mechanical, °C | 320 | |
| 160 |
| Melting Completion (Liquidus), °C | 1760 | |
| 650 |
| Melting Onset (Solidus), °C | 1700 | |
| 620 |
| Specific Heat Capacity, J/kg-K | 500 | |
| 900 |
| Thermal Expansion, µm/m-K | 8.4 | |
| 23 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 48 | |
| 9.5 |
| Density, g/cm3 | 5.4 | |
| 2.7 |
| Embodied Carbon, kg CO2/kg material | 31 | |
| 8.3 |
| Embodied Energy, MJ/kg | 480 | |
| 150 |
| Embodied Water, L/kg | 150 | |
| 1190 |
Common Calculations
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 32 | |
| 50 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 97.6 to 99.4 |
| Boron (B), % | 0 | |
| 0 to 0.060 |
| Carbon (C), % | 0 to 0.1 | |
| 0 |
| Chromium (Cr), % | 0 | |
| 0 to 0.030 |
| Copper (Cu), % | 0 | |
| 0 to 0.1 |
| Hydrogen (H), % | 0 to 0.015 | |
| 0 |
| Iron (Fe), % | 0 to 0.1 | |
| 0 to 0.5 |
| Magnesium (Mg), % | 0 | |
| 0.35 to 0.8 |
| Manganese (Mn), % | 0 | |
| 0 to 0.030 |
| Molybdenum (Mo), % | 14 to 16 | |
| 0 |
| Nitrogen (N), % | 0 to 0.050 | |
| 0 |
| Oxygen (O), % | 0 to 0.2 | |
| 0 |
| Silicon (Si), % | 0 | |
| 0.3 to 0.7 |
| Titanium (Ti), % | 83.5 to 86 | |
| 0 |
| Zinc (Zn), % | 0 | |
| 0 to 0.1 |
| Residuals, % | 0 | |
| 0 to 0.1 |