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6101A Aluminum vs. 6110 Aluminum

Both 6101A aluminum and 6110 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 6101A aluminum and the bottom bar is 6110 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
70
Elongation at Break, % 11
2.2
Fatigue Strength, MPa 80
120
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
26
Shear Strength, MPa 130
290
Tensile Strength: Ultimate (UTS), MPa 220
500
Tensile Strength: Yield (Proof), MPa 190
500

Thermal Properties

Latent Heat of Fusion, J/g 400
410
Maximum Temperature: Mechanical, °C 160
170
Melting Completion (Liquidus), °C 640
640
Melting Onset (Solidus), °C 630
600
Specific Heat Capacity, J/kg-K 900
900
Thermal Conductivity, W/m-K 200
170
Thermal Expansion, µm/m-K 23
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 55
42
Electrical Conductivity: Equal Weight (Specific), % IACS 180
140

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
9.5
Density, g/cm3 2.7
2.8
Embodied Carbon, kg CO2/kg material 8.3
8.2
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1190
1170

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 24
11
Resilience: Unit (Modulus of Resilience), kJ/m3 280
1770
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 51
50
Strength to Weight: Axial, points 23
51
Strength to Weight: Bending, points 30
51
Thermal Diffusivity, mm2/s 84
67
Thermal Shock Resistance, points 10
22

Alloy Composition


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Aluminum (Al), % 97.9 to 99.3
94.4 to 98.4
Chromium (Cr), % 0
0.040 to 0.25
Copper (Cu), % 0 to 0.050
0.2 to 0.7
Iron (Fe), % 0 to 0.4
0 to 0.8
Magnesium (Mg), % 0.4 to 0.9
0.5 to 1.1
Manganese (Mn), % 0
0.2 to 0.7
Silicon (Si), % 0.3 to 0.7
0.7 to 1.5
Titanium (Ti), % 0
0 to 0.15
Zinc (Zn), % 0
0 to 0.3
Residuals, % 0 to 0.1
0 to 0.15