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6101A Aluminum vs. 5070 Aluminum

Both 6101A aluminum and 5070 aluminum are aluminum alloys. They have a very high 95% of their average alloy composition in common.

For each property being compared, the top bar is 6101A aluminum and the bottom bar is 5070 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
68
Elongation at Break, % 11
20
Fatigue Strength, MPa 80
150
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
26
Shear Strength, MPa 130
190
Tensile Strength: Ultimate (UTS), MPa 220
300
Tensile Strength: Yield (Proof), MPa 190
140

Thermal Properties

Latent Heat of Fusion, J/g 400
390
Maximum Temperature: Mechanical, °C 160
190
Melting Completion (Liquidus), °C 640
640
Melting Onset (Solidus), °C 630
550
Specific Heat Capacity, J/kg-K 900
900
Thermal Conductivity, W/m-K 200
130
Thermal Expansion, µm/m-K 23
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 55
31
Electrical Conductivity: Equal Weight (Specific), % IACS 180
100

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
9.5
Density, g/cm3 2.7
2.7
Embodied Carbon, kg CO2/kg material 8.3
8.8
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1190
1170

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 24
51
Resilience: Unit (Modulus of Resilience), kJ/m3 280
150
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 51
50
Strength to Weight: Axial, points 23
31
Strength to Weight: Bending, points 30
37
Thermal Diffusivity, mm2/s 84
53
Thermal Shock Resistance, points 10
14

Alloy Composition


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Aluminum (Al), % 97.9 to 99.3
92.4 to 95.7
Chromium (Cr), % 0
0 to 0.3
Copper (Cu), % 0 to 0.050
0 to 0.25
Iron (Fe), % 0 to 0.4
0 to 0.4
Magnesium (Mg), % 0.4 to 0.9
3.5 to 4.5
Manganese (Mn), % 0
0.4 to 0.8
Silicon (Si), % 0.3 to 0.7
0 to 0.25
Titanium (Ti), % 0
0 to 0.15
Zinc (Zn), % 0
0.4 to 0.8
Residuals, % 0 to 0.1
0 to 0.15