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6101A Aluminum vs. 5182 Aluminum

Both 6101A aluminum and 5182 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 6101A aluminum and the bottom bar is 5182 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
68
Elongation at Break, % 11
1.1 to 12
Fatigue Strength, MPa 80
100 to 130
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
25
Shear Strength, MPa 130
170 to 240
Tensile Strength: Ultimate (UTS), MPa 220
280 to 420
Tensile Strength: Yield (Proof), MPa 190
130 to 360

Thermal Properties

Latent Heat of Fusion, J/g 400
390
Maximum Temperature: Mechanical, °C 160
180
Melting Completion (Liquidus), °C 640
640
Melting Onset (Solidus), °C 630
590
Specific Heat Capacity, J/kg-K 900
900
Thermal Conductivity, W/m-K 200
130
Thermal Expansion, µm/m-K 23
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 55
28
Electrical Conductivity: Equal Weight (Specific), % IACS 180
94

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
9.5
Density, g/cm3 2.7
2.7
Embodied Carbon, kg CO2/kg material 8.3
8.9
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1190
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 24
2.6 to 49
Resilience: Unit (Modulus of Resilience), kJ/m3 280
120 to 950
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 51
51
Strength to Weight: Axial, points 23
29 to 44
Strength to Weight: Bending, points 30
36 to 47
Thermal Diffusivity, mm2/s 84
53
Thermal Shock Resistance, points 10
12 to 19

Alloy Composition


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Aluminum (Al), % 97.9 to 99.3
93.2 to 95.8
Chromium (Cr), % 0
0 to 0.1
Copper (Cu), % 0 to 0.050
0 to 0.15
Iron (Fe), % 0 to 0.4
0 to 0.35
Magnesium (Mg), % 0.4 to 0.9
4.0 to 5.0
Manganese (Mn), % 0
0.2 to 0.5
Silicon (Si), % 0.3 to 0.7
0 to 0.2
Titanium (Ti), % 0
0 to 0.1
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0 to 0.1
0 to 0.15