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6110 Aluminum vs. 6101A Aluminum

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

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Electrical Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition


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