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6025 Aluminum vs. 6101A Aluminum

Both 6025 aluminum and 6101A 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 6025 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, % 2.8 to 10
11
Fatigue Strength, MPa 67 to 110
80
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
26
Shear Strength, MPa 110 to 140
130
Tensile Strength: Ultimate (UTS), MPa 190 to 240
220
Tensile Strength: Yield (Proof), MPa 68 to 210
190

Thermal Properties

Latent Heat of Fusion, J/g 410
400
Maximum Temperature: Mechanical, °C 160
160
Melting Completion (Liquidus), °C 650
640
Melting Onset (Solidus), °C 550
630
Specific Heat Capacity, J/kg-K 900
900
Thermal Conductivity, W/m-K 130
200
Thermal Expansion, µm/m-K 23
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 33
55
Electrical Conductivity: Equal Weight (Specific), % IACS 110
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 8.5
8.3
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1160
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 6.0 to 15
24
Resilience: Unit (Modulus of Resilience), kJ/m3 33 to 310
280
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
51
Strength to Weight: Axial, points 19 to 24
23
Strength to Weight: Bending, points 26 to 31
30
Thermal Diffusivity, mm2/s 54
84
Thermal Shock Resistance, points 8.2 to 10
10

Alloy Composition


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Aluminum (Al), % 91.7 to 96.3
97.9 to 99.3
Chromium (Cr), % 0 to 0.2
0
Copper (Cu), % 0.2 to 0.7
0 to 0.050
Iron (Fe), % 0 to 0.7
0 to 0.4
Magnesium (Mg), % 2.1 to 3.0
0.4 to 0.9
Manganese (Mn), % 0.6 to 1.4
0
Silicon (Si), % 0.8 to 1.5
0.3 to 0.7
Titanium (Ti), % 0 to 0.2
0
Zinc (Zn), % 0 to 0.5
0
Residuals, % 0 to 0.15
0 to 0.1