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Aluminum 6063-T6

Material Notes: From the fabrication of pipes through architectural extrusions to transportation parts, the usage of Aluminum is diverse. The data marked with AA notes were provided by the Aluminum Association, Inc., and are for information only; they were not made for design purposes.

Composition Notes: The Aluminum Association enables composition details for reference use only, and those details can’t be relied on for design implementation.

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Specifications for Aluminum 6063-T6

This table presents an overview of the material’s composition which includes its physical, mechanical, electrical, thermal, processing and component elements properties.

PropertyMetric ValueEnglish ValueComments
Physical Properties
Density2.70 g/cc0.0975 lb/in³AA; Typical
Mechanical Properties
Hardness, Brinell7373AA; Typical; 500 g load; 10 mm ball
Hardness, Knoop9696Converted from Brinell Hardness Value
Hardness, Vickers8383Converted from Brinell Hardness Value
Tensile Strength, Ultimate241 MPa35000 psiAA; Typical
Tensile Strength, Yield214 MPa31000 psiAA; Typical
Elongation at Break15% - 105%15% - 105%Varies with temperature
Modulus of Elasticity68.9 GPa10000 ksiAA; Typical; Average of tension and compression
Ultimate Bearing Strength434 MPa62900 psiEdge distance/pin diameter = 2.0
Bearing Yield Strength276 MPa40000 psiEdge distance/pin diameter = 2.0
Poisson's Ratio0.330.33
Fatigue Strength68.9 MPa10000 psi@# of Cycles 5.00e+8, completely reversed stress
Machinability50%50%0-100 Scale of Aluminum Alloys
Shear Modulus25.8 GPa3740 ksi
Shear Strength152 MPa22000 psiAA; Typical
Electrical Properties
Electrical Resistivity0.00000332 ohm-cm0.00000332 ohm-cmAA; Typical
Thermal Properties
CTE, linear21.8 - 25.6 µm/m-°C12.1 - 14.2 µin/in-°FVaries with temperature range
Specific Heat Capacity0.900 J/g-°C0.215 BTU/lb-°F
Thermal Conductivity200 W/m-K1390 BTU-in/hr-ft²-°FAA; Typical at 77°F
Melting Point616 - 654 °C1140 - 1210 °FAA; Typical range based on typical composition
Solidus616 °C1140 °FAA; Typical
Liquidus654 °C1210 °FAA; Typical
Processing Properties
Annealing Temperature413 °C775 °FHold at temperature for 2 to 3 hr; cool at 50°F per hour from 775 to 500°F
Solution Temperature521 °C970 °F
Aging Temperature177 °C350 °FHold at temperature for 8 hr
Component Elements Properties
Aluminum, Al<= 97.5%<= 97.5%As remainder
Chromium, Cr<= 0.10%<= 0.10%
Copper, Cu<= 0.10%<= 0.10%
Iron, Fe<= 0.35%<= 0.35%
Magnesium, Mg0.45 - 0.90%0.45 - 0.90%
Manganese, Mn<= 0.10%<= 0.10%
Other, each<= 0.05%<= 0.05%
Other, total<= 0.15%<= 0.15%
Silicon, Si0.20 - 0.60%0.20 - 0.60%
Titanium, Ti<= 0.10%<= 0.10%
Zinc, Zn<= 0.10%<= 0.10%
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