7475 Aluminum vs. Grade 23 Titanium
7475 aluminum belongs to the aluminum alloys classification, while grade 23 titanium belongs to the titanium alloys. There are 30 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 7475 aluminum and the bottom bar is grade 23 titanium.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 70 | |
110 |
Elongation at Break, % | 10 to 12 | |
6.7 to 11 |
Fatigue Strength, MPa | 190 to 210 | |
470 to 500 |
Poisson's Ratio | 0.32 | |
0.32 |
Shear Modulus, GPa | 26 | |
40 |
Shear Strength, MPa | 320 to 350 | |
540 to 570 |
Tensile Strength: Ultimate (UTS), MPa | 530 to 590 | |
930 to 940 |
Tensile Strength: Yield (Proof), MPa | 440 to 520 | |
850 to 870 |
Thermal Properties
Latent Heat of Fusion, J/g | 380 | |
410 |
Maximum Temperature: Mechanical, °C | 180 | |
340 |
Melting Completion (Liquidus), °C | 640 | |
1610 |
Melting Onset (Solidus), °C | 480 | |
1560 |
Specific Heat Capacity, J/kg-K | 870 | |
560 |
Thermal Conductivity, W/m-K | 140 to 160 | |
7.1 |
Thermal Expansion, µm/m-K | 23 | |
9.4 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 33 to 42 | |
1.0 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 98 to 120 | |
2.0 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 10 | |
36 |
Density, g/cm3 | 3.0 | |
4.4 |
Embodied Carbon, kg CO2/kg material | 8.2 | |
38 |
Embodied Energy, MJ/kg | 150 | |
610 |
Embodied Water, L/kg | 1130 | |
200 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 53 to 68 | |
61 to 100 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 1390 to 1920 | |
3430 to 3560 |
Stiffness to Weight: Axial, points | 13 | |
13 |
Stiffness to Weight: Bending, points | 46 | |
35 |
Strength to Weight: Axial, points | 49 to 55 | |
58 to 59 |
Strength to Weight: Bending, points | 48 to 52 | |
48 |
Thermal Diffusivity, mm2/s | 53 to 63 | |
2.9 |
Thermal Shock Resistance, points | 23 to 26 | |
67 to 68 |
Alloy Composition
Aluminum (Al), % | 88.6 to 91.6 | |
5.5 to 6.5 |
Carbon (C), % | 0 | |
0 to 0.080 |
Chromium (Cr), % | 0.18 to 0.25 | |
0 |
Copper (Cu), % | 1.2 to 1.9 | |
0 |
Hydrogen (H), % | 0 | |
0 to 0.013 |
Iron (Fe), % | 0 to 0.12 | |
0 to 0.25 |
Magnesium (Mg), % | 1.9 to 2.6 | |
0 |
Manganese (Mn), % | 0 to 0.060 | |
0 |
Nitrogen (N), % | 0 | |
0 to 0.030 |
Oxygen (O), % | 0 | |
0 to 0.13 |
Silicon (Si), % | 0 to 0.1 | |
0 |
Titanium (Ti), % | 0 to 0.060 | |
88.1 to 91 |
Vanadium (V), % | 0 | |
3.5 to 4.5 |
Zinc (Zn), % | 5.1 to 6.2 | |
0 |
Residuals, % | 0 | |
0 to 0.4 |