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1435 Aluminum vs. 6110 Aluminum

Both 1435 aluminum and 6110 aluminum are aluminum alloys. They have a very high 97% of their average alloy composition in common.

For each property being compared, the top bar is 1435 aluminum and the bottom bar is 6110 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
70
Elongation at Break, % 4.1 to 32
2.2
Fatigue Strength, MPa 27 to 49
120
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
26
Shear Strength, MPa 54 to 87
290
Tensile Strength: Ultimate (UTS), MPa 81 to 150
500
Tensile Strength: Yield (Proof), MPa 23 to 130
500

Thermal Properties

Latent Heat of Fusion, J/g 400
410
Maximum Temperature: Mechanical, °C 170
170
Melting Completion (Liquidus), °C 650
640
Melting Onset (Solidus), °C 640
600
Specific Heat Capacity, J/kg-K 900
900
Thermal Conductivity, W/m-K 230
170
Thermal Expansion, µm/m-K 23
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 60
42
Electrical Conductivity: Equal Weight (Specific), % IACS 200
140

Otherwise Unclassified Properties

Base Metal Price, % relative 9.0
9.5
Density, g/cm3 2.7
2.8
Embodied Carbon, kg CO2/kg material 8.2
8.2
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1190
1170

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 5.0 to 20
11
Resilience: Unit (Modulus of Resilience), kJ/m3 3.8 to 110
1770
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
50
Strength to Weight: Axial, points 8.3 to 15
51
Strength to Weight: Bending, points 15 to 23
51
Thermal Diffusivity, mm2/s 93
67
Thermal Shock Resistance, points 3.6 to 6.7
22

Alloy Composition


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Aluminum (Al), % 99.35 to 99.7
94.4 to 98.4
Chromium (Cr), % 0
0.040 to 0.25
Copper (Cu), % 0 to 0.020
0.2 to 0.7
Iron (Fe), % 0.3 to 0.5
0 to 0.8
Magnesium (Mg), % 0 to 0.050
0.5 to 1.1
Manganese (Mn), % 0 to 0.050
0.2 to 0.7
Silicon (Si), % 0 to 0.15
0.7 to 1.5
Titanium (Ti), % 0 to 0.030
0 to 0.15
Zinc (Zn), % 0 to 0.1
0 to 0.3
Residuals, % 0
0 to 0.15