7050 Aluminum vs. Grade 18 Titanium
7050 aluminum belongs to the aluminum alloys classification, while grade 18 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 7050 aluminum and the bottom bar is grade 18 titanium.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 70 | |
110 |
Elongation at Break, % | 2.2 to 12 | |
11 to 17 |
Fatigue Strength, MPa | 130 to 210 | |
330 to 480 |
Poisson's Ratio | 0.32 | |
0.32 |
Shear Modulus, GPa | 26 | |
40 |
Shear Strength, MPa | 280 to 330 | |
420 to 590 |
Tensile Strength: Ultimate (UTS), MPa | 490 to 570 | |
690 to 980 |
Tensile Strength: Yield (Proof), MPa | 390 to 500 | |
540 to 810 |
Thermal Properties
Latent Heat of Fusion, J/g | 370 | |
410 |
Maximum Temperature: Mechanical, °C | 190 | |
330 |
Melting Completion (Liquidus), °C | 630 | |
1640 |
Melting Onset (Solidus), °C | 490 | |
1590 |
Specific Heat Capacity, J/kg-K | 860 | |
550 |
Thermal Conductivity, W/m-K | 140 | |
8.3 |
Thermal Expansion, µm/m-K | 24 | |
9.9 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 35 | |
1.3 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 100 | |
2.7 |
Otherwise Unclassified Properties
Density, g/cm3 | 3.1 | |
4.5 |
Embodied Carbon, kg CO2/kg material | 8.2 | |
41 |
Embodied Energy, MJ/kg | 150 | |
670 |
Embodied Water, L/kg | 1120 | |
270 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 10 to 55 | |
87 to 110 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 1110 to 1760 | |
1380 to 3110 |
Stiffness to Weight: Axial, points | 13 | |
13 |
Stiffness to Weight: Bending, points | 45 | |
35 |
Strength to Weight: Axial, points | 45 to 51 | |
43 to 61 |
Strength to Weight: Bending, points | 45 to 50 | |
39 to 49 |
Thermal Diffusivity, mm2/s | 54 | |
3.4 |
Thermal Shock Resistance, points | 21 to 25 | |
47 to 67 |
Alloy Composition
Aluminum (Al), % | 87.3 to 92.1 | |
2.5 to 3.5 |
Carbon (C), % | 0 | |
0 to 0.080 |
Chromium (Cr), % | 0 to 0.040 | |
0 |
Copper (Cu), % | 2.0 to 2.6 | |
0 |
Hydrogen (H), % | 0 | |
0 to 0.015 |
Iron (Fe), % | 0 to 0.15 | |
0 to 0.25 |
Magnesium (Mg), % | 1.9 to 2.6 | |
0 |
Manganese (Mn), % | 0 to 0.1 | |
0 |
Nitrogen (N), % | 0 | |
0 to 0.030 |
Oxygen (O), % | 0 | |
0 to 0.15 |
Palladium (Pd), % | 0 | |
0.040 to 0.080 |
Silicon (Si), % | 0 to 0.12 | |
0 |
Titanium (Ti), % | 0 to 0.060 | |
92.5 to 95.5 |
Vanadium (V), % | 0 | |
2.0 to 3.0 |
Zinc (Zn), % | 5.7 to 6.7 | |
0 |
Zirconium (Zr), % | 0.080 to 0.15 | |
0 |
Residuals, % | 0 | |
0 to 0.4 |