5657 Aluminum vs. 771.0 Aluminum
Both 5657 aluminum and 771.0 aluminum are aluminum alloys. They have a moderately high 93% of their average alloy composition in common. 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 5657 aluminum and the bottom bar is 771.0 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
Brinell Hardness | 40 to 50 | |
85 to 120 |
Elastic (Young's, Tensile) Modulus, GPa | 68 | |
70 |
Elongation at Break, % | 6.6 to 15 | |
1.7 to 6.5 |
Fatigue Strength, MPa | 74 to 88 | |
92 to 180 |
Poisson's Ratio | 0.33 | |
0.32 |
Shear Modulus, GPa | 26 | |
26 |
Tensile Strength: Ultimate (UTS), MPa | 150 to 200 | |
250 to 370 |
Tensile Strength: Yield (Proof), MPa | 140 to 170 | |
210 to 350 |
Thermal Properties
Latent Heat of Fusion, J/g | 400 | |
380 |
Maximum Temperature: Mechanical, °C | 180 | |
180 |
Melting Completion (Liquidus), °C | 660 | |
630 |
Melting Onset (Solidus), °C | 640 | |
620 |
Specific Heat Capacity, J/kg-K | 900 | |
870 |
Thermal Conductivity, W/m-K | 210 | |
140 to 150 |
Thermal Expansion, µm/m-K | 24 | |
24 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 54 | |
27 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 180 | |
82 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 9.5 | |
9.5 |
Density, g/cm3 | 2.7 | |
3.0 |
Embodied Carbon, kg CO2/kg material | 8.4 | |
8.0 |
Embodied Energy, MJ/kg | 160 | |
150 |
Embodied Water, L/kg | 1200 | |
1130 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 9.7 to 27 | |
4.4 to 20 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 140 to 200 | |
310 to 900 |
Stiffness to Weight: Axial, points | 14 | |
13 |
Stiffness to Weight: Bending, points | 50 | |
46 |
Strength to Weight: Axial, points | 15 to 20 | |
23 to 35 |
Strength to Weight: Bending, points | 23 to 28 | |
29 to 39 |
Thermal Diffusivity, mm2/s | 84 | |
54 to 58 |
Thermal Shock Resistance, points | 6.7 to 8.6 | |
11 to 16 |
Alloy Composition
Aluminum (Al), % | 98.5 to 99.4 | |
90.5 to 92.5 |
Chromium (Cr), % | 0 | |
0.060 to 0.2 |
Copper (Cu), % | 0 to 0.1 | |
0 to 0.1 |
Gallium (Ga), % | 0 to 0.030 | |
0 |
Iron (Fe), % | 0 to 0.1 | |
0 to 0.15 |
Magnesium (Mg), % | 0.6 to 1.0 | |
0.8 to 1.0 |
Manganese (Mn), % | 0 to 0.030 | |
0 to 0.1 |
Silicon (Si), % | 0 to 0.080 | |
0 to 0.15 |
Titanium (Ti), % | 0 | |
0.1 to 0.2 |
Vanadium (V), % | 0 to 0.050 | |
0 |
Zinc (Zn), % | 0 to 0.050 | |
6.5 to 7.5 |
Residuals, % | 0 | |
0 to 0.15 |