771.0 Aluminum vs. 852.0 Aluminum
Both 771.0 aluminum and 852.0 aluminum are aluminum alloys. They have a moderately high 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 771.0 aluminum and the bottom bar is 852.0 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
Brinell Hardness | 85 to 120 | |
64 |
Elastic (Young's, Tensile) Modulus, GPa | 70 | |
70 |
Elongation at Break, % | 1.7 to 6.5 | |
3.4 |
Fatigue Strength, MPa | 92 to 180 | |
73 |
Poisson's Ratio | 0.32 | |
0.33 |
Shear Modulus, GPa | 26 | |
26 |
Tensile Strength: Ultimate (UTS), MPa | 250 to 370 | |
200 |
Tensile Strength: Yield (Proof), MPa | 210 to 350 | |
150 |
Thermal Properties
Latent Heat of Fusion, J/g | 380 | |
370 |
Maximum Temperature: Mechanical, °C | 180 | |
190 |
Melting Completion (Liquidus), °C | 630 | |
640 |
Melting Onset (Solidus), °C | 620 | |
210 |
Solidification (Pattern Maker's) Shrinkage, % | 1.6 | |
1.3 |
Specific Heat Capacity, J/kg-K | 870 | |
840 |
Thermal Conductivity, W/m-K | 140 to 150 | |
180 |
Thermal Expansion, µm/m-K | 24 | |
23 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 27 | |
45 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 82 | |
130 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 9.5 | |
15 |
Density, g/cm3 | 3.0 | |
3.2 |
Embodied Carbon, kg CO2/kg material | 8.0 | |
8.5 |
Embodied Energy, MJ/kg | 150 | |
160 |
Embodied Water, L/kg | 1130 | |
1150 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 4.4 to 20 | |
6.2 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 310 to 900 | |
160 |
Stiffness to Weight: Axial, points | 13 | |
12 |
Stiffness to Weight: Bending, points | 46 | |
43 |
Strength to Weight: Axial, points | 23 to 35 | |
17 |
Strength to Weight: Bending, points | 29 to 39 | |
24 |
Thermal Diffusivity, mm2/s | 54 to 58 | |
65 |
Thermal Shock Resistance, points | 11 to 16 | |
8.7 |
Alloy Composition
Aluminum (Al), % | 90.5 to 92.5 | |
86.6 to 91.3 |
Chromium (Cr), % | 0.060 to 0.2 | |
0 |
Copper (Cu), % | 0 to 0.1 | |
1.7 to 2.3 |
Iron (Fe), % | 0 to 0.15 | |
0 to 0.7 |
Magnesium (Mg), % | 0.8 to 1.0 | |
0.6 to 0.9 |
Manganese (Mn), % | 0 to 0.1 | |
0 to 0.1 |
Nickel (Ni), % | 0 | |
0.9 to 1.5 |
Silicon (Si), % | 0 to 0.15 | |
0 to 0.4 |
Tin (Sn), % | 0 | |
5.5 to 7.0 |
Titanium (Ti), % | 0.1 to 0.2 | |
0 to 0.2 |
Zinc (Zn), % | 6.5 to 7.5 | |
0 |
Residuals, % | 0 | |
0 to 0.3 |