7075 Aluminum vs. A360.0 Aluminum
Both 7075 aluminum and A360.0 aluminum are aluminum alloys. They have 90% of their average alloy composition in common. There are 31 material properties with values for both materials. Properties with values for just one material (1, in this case) are not shown.
For each property being compared, the top bar is 7075 aluminum and the bottom bar is A360.0 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 70 | |
72 |
Elongation at Break, % | 1.8 to 12 | |
1.6 to 5.0 |
Fatigue Strength, MPa | 110 to 190 | |
82 to 150 |
Poisson's Ratio | 0.32 | |
0.33 |
Shear Modulus, GPa | 26 | |
27 |
Shear Strength, MPa | 150 to 340 | |
180 |
Tensile Strength: Ultimate (UTS), MPa | 240 to 590 | |
180 to 320 |
Tensile Strength: Yield (Proof), MPa | 120 to 510 | |
170 to 260 |
Thermal Properties
Latent Heat of Fusion, J/g | 380 | |
530 |
Maximum Temperature: Mechanical, °C | 200 | |
170 |
Melting Completion (Liquidus), °C | 640 | |
680 |
Melting Onset (Solidus), °C | 480 | |
590 |
Specific Heat Capacity, J/kg-K | 870 | |
900 |
Thermal Conductivity, W/m-K | 130 | |
110 |
Thermal Expansion, µm/m-K | 23 | |
21 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 33 | |
30 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 98 | |
100 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 10 | |
9.5 |
Calomel Potential, mV | -750 | |
-700 |
Density, g/cm3 | 3.0 | |
2.6 |
Embodied Carbon, kg CO2/kg material | 8.3 | |
7.8 |
Embodied Energy, MJ/kg | 150 | |
150 |
Embodied Water, L/kg | 1120 | |
1070 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 7.8 to 44 | |
4.6 to 13 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 110 to 1870 | |
190 to 470 |
Stiffness to Weight: Axial, points | 13 | |
15 |
Stiffness to Weight: Bending, points | 46 | |
53 |
Strength to Weight: Axial, points | 22 to 54 | |
19 to 34 |
Strength to Weight: Bending, points | 28 to 52 | |
27 to 39 |
Thermal Diffusivity, mm2/s | 50 | |
48 |
Thermal Shock Resistance, points | 10 to 25 | |
8.5 to 15 |
Alloy Composition
Aluminum (Al), % | 86.9 to 91.4 | |
85.8 to 90.6 |
Chromium (Cr), % | 0.18 to 0.28 | |
0 |
Copper (Cu), % | 1.2 to 2.0 | |
0 to 0.6 |
Iron (Fe), % | 0 to 0.5 | |
0 to 1.3 |
Magnesium (Mg), % | 2.1 to 2.9 | |
0.4 to 0.6 |
Manganese (Mn), % | 0 to 0.3 | |
0 to 0.35 |
Nickel (Ni), % | 0 | |
0 to 0.5 |
Silicon (Si), % | 0 to 0.4 | |
9.0 to 10 |
Tin (Sn), % | 0 | |
0 to 0.15 |
Titanium (Ti), % | 0 to 0.2 | |
0 |
Zinc (Zn), % | 5.1 to 6.1 | |
0 to 0.5 |
Zirconium (Zr), % | 0 to 0.25 | |
0 |
Residuals, % | 0 | |
0 to 0.25 |