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6025 Aluminum vs. 5070 Aluminum

Both 6025 aluminum and 5070 aluminum are aluminum alloys. They have a very high 98% of their average alloy composition in common.

For each property being compared, the top bar is 6025 aluminum and the bottom bar is 5070 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
68
Elongation at Break, % 2.8 to 10
20
Fatigue Strength, MPa 67 to 110
150
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
26
Shear Strength, MPa 110 to 140
190
Tensile Strength: Ultimate (UTS), MPa 190 to 240
300
Tensile Strength: Yield (Proof), MPa 68 to 210
140

Thermal Properties

Latent Heat of Fusion, J/g 410
390
Maximum Temperature: Mechanical, °C 160
190
Melting Completion (Liquidus), °C 650
640
Melting Onset (Solidus), °C 550
550
Specific Heat Capacity, J/kg-K 900
900
Thermal Conductivity, W/m-K 130
130
Thermal Expansion, µm/m-K 23
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 33
31
Electrical Conductivity: Equal Weight (Specific), % IACS 110
100

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
9.5
Density, g/cm3 2.8
2.7
Embodied Carbon, kg CO2/kg material 8.5
8.8
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1160
1170

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 6.0 to 15
51
Resilience: Unit (Modulus of Resilience), kJ/m3 33 to 310
150
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
50
Strength to Weight: Axial, points 19 to 24
31
Strength to Weight: Bending, points 26 to 31
37
Thermal Diffusivity, mm2/s 54
53
Thermal Shock Resistance, points 8.2 to 10
14

Alloy Composition

Aluminum (Al), % 91.7 to 96.3
92.4 to 95.7
Chromium (Cr), % 0 to 0.2
0 to 0.3
Copper (Cu), % 0.2 to 0.7
0 to 0.25
Iron (Fe), % 0 to 0.7
0 to 0.4
Magnesium (Mg), % 2.1 to 3.0
3.5 to 4.5
Manganese (Mn), % 0.6 to 1.4
0.4 to 0.8
Silicon (Si), % 0.8 to 1.5
0 to 0.25
Titanium (Ti), % 0 to 0.2
0 to 0.15
Zinc (Zn), % 0 to 0.5
0.4 to 0.8
Residuals, % 0
0 to 0.15