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6106 Aluminum vs. 6025 Aluminum

Both 6106 aluminum and 6025 aluminum are aluminum alloys. They have a very high 96% of their average alloy composition in common.

For each property being compared, the top bar is 6106 aluminum and the bottom bar is 6025 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
70
Elongation at Break, % 9.1
2.8 to 10
Fatigue Strength, MPa 88
67 to 110
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
26
Shear Strength, MPa 170
110 to 140
Tensile Strength: Ultimate (UTS), MPa 290
190 to 240
Tensile Strength: Yield (Proof), MPa 220
68 to 210

Thermal Properties

Latent Heat of Fusion, J/g 400
410
Maximum Temperature: Mechanical, °C 160
160
Melting Completion (Liquidus), °C 660
650
Melting Onset (Solidus), °C 610
550
Specific Heat Capacity, J/kg-K 900
900
Thermal Conductivity, W/m-K 190
130
Thermal Expansion, µm/m-K 23
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 49
33
Electrical Conductivity: Equal Weight (Specific), % IACS 160
110

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
8.5
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1190
1160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 24
6.0 to 15
Resilience: Unit (Modulus of Resilience), kJ/m3 370
33 to 310
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
50
Strength to Weight: Axial, points 29
19 to 24
Strength to Weight: Bending, points 35
26 to 31
Thermal Diffusivity, mm2/s 78
54
Thermal Shock Resistance, points 13
8.2 to 10

Alloy Composition

Aluminum (Al), % 97.2 to 99.3
91.7 to 96.3
Chromium (Cr), % 0 to 0.2
0 to 0.2
Copper (Cu), % 0 to 0.25
0.2 to 0.7
Iron (Fe), % 0 to 0.35
0 to 0.7
Magnesium (Mg), % 0.4 to 0.8
2.1 to 3.0
Manganese (Mn), % 0.050 to 0.2
0.6 to 1.4
Silicon (Si), % 0.3 to 0.6
0.8 to 1.5
Titanium (Ti), % 0 to 0.1
0 to 0.2
Zinc (Zn), % 0 to 0.15
0 to 0.5
Residuals, % 0
0 to 0.15