6182 Aluminum vs. Grade 25 Titanium
6182 aluminum belongs to the aluminum alloys classification, while grade 25 titanium belongs to the titanium alloys. There are 29 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 6182 aluminum and the bottom bar is grade 25 titanium.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 70 | |
| 110 |
| Elongation at Break, % | 6.8 to 13 | |
| 11 |
| Fatigue Strength, MPa | 63 to 99 | |
| 550 |
| Poisson's Ratio | 0.33 | |
| 0.32 |
| Shear Modulus, GPa | 26 | |
| 40 |
| Shear Strength, MPa | 140 to 190 | |
| 600 |
| Tensile Strength: Ultimate (UTS), MPa | 230 to 320 | |
| 1000 |
| Tensile Strength: Yield (Proof), MPa | 130 to 270 | |
| 940 |
Thermal Properties
| Latent Heat of Fusion, J/g | 410 | |
| 410 |
| Maximum Temperature: Mechanical, °C | 190 | |
| 340 |
| Melting Completion (Liquidus), °C | 640 | |
| 1610 |
| Melting Onset (Solidus), °C | 600 | |
| 1560 |
| Specific Heat Capacity, J/kg-K | 900 | |
| 560 |
| Thermal Conductivity, W/m-K | 160 | |
| 7.1 |
| Thermal Expansion, µm/m-K | 23 | |
| 9.6 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 40 | |
| 1.0 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 130 | |
| 2.0 |
Otherwise Unclassified Properties
| Density, g/cm3 | 2.7 | |
| 4.5 |
| Embodied Carbon, kg CO2/kg material | 8.4 | |
| 43 |
| Embodied Energy, MJ/kg | 150 | |
| 700 |
| Embodied Water, L/kg | 1170 | |
| 320 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 21 to 26 | |
| 110 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 110 to 520 | |
| 4220 |
| Stiffness to Weight: Axial, points | 14 | |
| 13 |
| Stiffness to Weight: Bending, points | 50 | |
| 35 |
| Strength to Weight: Axial, points | 23 to 32 | |
| 62 |
| Strength to Weight: Bending, points | 30 to 38 | |
| 50 |
| Thermal Diffusivity, mm2/s | 65 | |
| 2.8 |
| Thermal Shock Resistance, points | 10 to 14 | |
| 71 |
Alloy Composition
| Aluminum (Al), % | 95 to 97.9 | |
| 5.5 to 6.8 |
| Carbon (C), % | 0 | |
| 0 to 0.080 |
| Chromium (Cr), % | 0 to 0.25 | |
| 0 |
| Copper (Cu), % | 0 to 0.1 | |
| 0 |
| Hydrogen (H), % | 0 | |
| 0 to 0.013 |
| Iron (Fe), % | 0 to 0.5 | |
| 0 to 0.4 |
| Magnesium (Mg), % | 0.7 to 1.2 | |
| 0 |
| Manganese (Mn), % | 0.5 to 1.0 | |
| 0 |
| Nickel (Ni), % | 0 | |
| 0.3 to 0.8 |
| Nitrogen (N), % | 0 | |
| 0 to 0.050 |
| Oxygen (O), % | 0 | |
| 0 to 0.2 |
| Palladium (Pd), % | 0 | |
| 0.040 to 0.080 |
| Silicon (Si), % | 0.9 to 1.3 | |
| 0 |
| Titanium (Ti), % | 0 to 0.1 | |
| 86.7 to 90.6 |
| Vanadium (V), % | 0 | |
| 3.5 to 4.5 |
| Zinc (Zn), % | 0 to 0.2 | |
| 0 |
| Zirconium (Zr), % | 0.050 to 0.2 | |
| 0 |
| Residuals, % | 0 | |
| 0 to 0.4 |