5083 Aluminum vs. Grade 9 Titanium
5083 aluminum belongs to the aluminum alloys classification, while grade 9 titanium belongs to the titanium alloys. There are 30 material properties with values for both materials. Properties with values for just one material (4, in this case) are not shown.
For each property being compared, the top bar is 5083 aluminum and the bottom bar is grade 9 titanium.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 68 | |
110 |
Elongation at Break, % | 1.1 to 17 | |
11 to 17 |
Fatigue Strength, MPa | 93 to 190 | |
330 to 480 |
Poisson's Ratio | 0.33 | |
0.32 |
Shear Modulus, GPa | 26 | |
40 |
Shear Strength, MPa | 170 to 220 | |
430 to 580 |
Tensile Strength: Ultimate (UTS), MPa | 290 to 390 | |
700 to 960 |
Tensile Strength: Yield (Proof), MPa | 110 to 340 | |
540 to 830 |
Thermal Properties
Latent Heat of Fusion, J/g | 400 | |
410 |
Maximum Temperature: Mechanical, °C | 190 | |
330 |
Melting Completion (Liquidus), °C | 640 | |
1640 |
Melting Onset (Solidus), °C | 580 | |
1590 |
Specific Heat Capacity, J/kg-K | 900 | |
550 |
Thermal Conductivity, W/m-K | 120 | |
8.1 |
Thermal Expansion, µm/m-K | 24 | |
9.1 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 29 | |
1.4 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 96 | |
2.7 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 9.5 | |
37 |
Density, g/cm3 | 2.7 | |
4.5 |
Embodied Carbon, kg CO2/kg material | 8.9 | |
36 |
Embodied Energy, MJ/kg | 150 | |
580 |
Embodied Water, L/kg | 1170 | |
150 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 4.2 to 42 | |
89 to 110 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 95 to 860 | |
1380 to 3220 |
Stiffness to Weight: Axial, points | 14 | |
13 |
Stiffness to Weight: Bending, points | 50 | |
35 |
Strength to Weight: Axial, points | 29 to 40 | |
43 to 60 |
Strength to Weight: Bending, points | 36 to 44 | |
39 to 48 |
Thermal Diffusivity, mm2/s | 48 | |
3.3 |
Thermal Shock Resistance, points | 12 to 17 | |
52 to 71 |
Alloy Composition
Aluminum (Al), % | 92.4 to 95.6 | |
2.5 to 3.5 |
Carbon (C), % | 0 | |
0 to 0.080 |
Chromium (Cr), % | 0.050 to 0.25 | |
0 |
Copper (Cu), % | 0 to 0.1 | |
0 |
Hydrogen (H), % | 0 | |
0 to 0.015 |
Iron (Fe), % | 0 to 0.4 | |
0 to 0.25 |
Magnesium (Mg), % | 4.0 to 4.9 | |
0 |
Manganese (Mn), % | 0.4 to 1.0 | |
0 |
Nitrogen (N), % | 0 | |
0 to 0.030 |
Oxygen (O), % | 0 | |
0 to 0.15 |
Silicon (Si), % | 0 to 0.4 | |
0 |
Titanium (Ti), % | 0 to 0.15 | |
92.6 to 95.5 |
Vanadium (V), % | 0 | |
2.0 to 3.0 |
Zinc (Zn), % | 0 to 0.25 | |
0 |
Residuals, % | 0 | |
0 to 0.4 |