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6101A Aluminum vs. 5088 Aluminum

Both 6101A aluminum and 5088 aluminum are aluminum alloys. They have a moderately high 95% of their average alloy composition in common.

For each property being compared, the top bar is 6101A aluminum and the bottom bar is 5088 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
68
Elongation at Break, % 11
29
Fatigue Strength, MPa 80
180
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
25
Shear Strength, MPa 130
200
Tensile Strength: Ultimate (UTS), MPa 220
310
Tensile Strength: Yield (Proof), MPa 190
150

Thermal Properties

Latent Heat of Fusion, J/g 400
390
Maximum Temperature: Mechanical, °C 160
200
Melting Completion (Liquidus), °C 640
640
Melting Onset (Solidus), °C 630
540
Specific Heat Capacity, J/kg-K 900
900
Thermal Conductivity, W/m-K 200
120
Thermal Expansion, µm/m-K 23
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 55
29
Electrical Conductivity: Equal Weight (Specific), % IACS 180
98

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
9.0
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1190
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 24
76
Resilience: Unit (Modulus of Resilience), kJ/m3 280
170
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 51
50
Strength to Weight: Axial, points 23
32
Strength to Weight: Bending, points 30
38
Thermal Diffusivity, mm2/s 84
51
Thermal Shock Resistance, points 10
14

Alloy Composition


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Aluminum (Al), % 97.9 to 99.3
92.4 to 94.8
Chromium (Cr), % 0
0 to 0.15
Copper (Cu), % 0 to 0.050
0 to 0.25
Iron (Fe), % 0 to 0.4
0.1 to 0.35
Magnesium (Mg), % 0.4 to 0.9
4.7 to 5.5
Manganese (Mn), % 0
0.2 to 0.5
Silicon (Si), % 0.3 to 0.7
0 to 0.2
Zinc (Zn), % 0
0.2 to 0.4
Zirconium (Zr), % 0
0 to 0.15
Residuals, % 0 to 0.1
0 to 0.15