Aluminum 6061-T6; 6061-T651
Subcategory: 6000 Series Aluminum Alloy; Aluminum Alloy; Metal; Nonferrous Metal
Close Analogs: Composition Notes: Aluminum content reported is calculated as remainder. Composition information provided by the Aluminum Association and is not for design.
Key Words: al6061, UNS A96061; ISO AlMg1SiCu; Aluminium 6061-T6, AD-33 (Russia); AA6061-T6; 6061T6, UNS A96061; ISO AlMg1SiCu; Aluminium 6061-T651, AD-33 (Russia); AA6061-T651
Component | Wt. % |  | | Al | 95.8 - 98.6 | | Cr | 0.04 - 0.35 | | Cu | 0.15 - 0.4 | | Fe | Max 0.7 | |
| Component | Wt. % |  | | Mg | 0.8 - 1.2 | | Mn | Max 0.15 | | Other, each | Max 0.05 | | Other, total | Max 0.15 | |
| Component | Wt. % |  | | Si | 0.4 - 0.8 | | Ti | Max 0.15 | | Zn | Max 0.25 | |
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Material Notes: Information provided by Alcoa, Starmet and the references. General 6061 characteristics and uses: Excellent joining characteristics, good acceptance of applied coatings. Combines relatively high strength, good workability, and high resistance to corrosion; widely available. The T8 and T9 tempers offer better chipping characteristics over the T6 temper. Applications: Aircraft fittings, camera lens mounts, couplings, marines fittings and hardware, electrical fittings and connectors, decorative or misc. hardware, hinge pins, magneto parts, brake pistons, hydraulic pistons, appliance fittings, valves and valve parts; bike frames. Data points with the AA note have been provided by the Aluminum Association, Inc. and are NOT FOR DESIGN.
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Physical Properties | Original Value | Comments |
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Density | 2.7 g/cc | AA; Typical |
Mechanical Properties |
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Hardness, Brinell | 95 | AA; Typical; 500 g load; 10 mm ball |
Hardness, Knoop | 120 | Converted from Brinell Hardness Value |
Hardness, Rockwell A | 40 | Converted from Brinell Hardness Value |
Hardness, Rockwell B | 60 | Converted from Brinell Hardness Value |
Hardness, Vickers | 107 | Converted from Brinell Hardness Value |
Ultimate Tensile Strength | 45 ksi | AA; Typical |
Tensile Yield Strength | 40 ksi | AA; Typical |
Elongation at Break | 12 % | AA; Typical; 1/16 in. (1.6 mm) Thickness |
Elongation at Break | 17 % | AA; Typical; 1/2 in. (12.7 mm) Diameter |
Modulus of Elasticity | 10000 ksi | AA; Typical; Average of tension and compression. Compression modulus is about 2% greater than tensile modulus. |
Notched Tensile Strength | 324 MPa | 2.5 cm width x 0.16 cm thick side-notched specimen, Kt = 17. |
Ultimate Bearing Strength | 607 MPa | Edge distance/pin diameter = 2.0 |
Bearing Yield Strength | 386 MPa | Edge distance/pin diameter = 2.0 |
Poisson's Ratio | 0.33 | Estimated from trends in similar Al alloys. |
Fatigue Strength | 14000 psi | AA; 500,000,000 cycles completely reversed stress; RR Moore machine/specimen |
Fracture Toughness | 29 MPa-m½ | KIC; TL orientation. |
Machinability | 50 % | 0-100 Scale of Aluminum Alloys |
Shear Modulus | 26 GPa | Estimated from similar Al alloys. |
Shear Strength | 30 ksi | AA; Typical |
Electrical Properties |
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Electrical Resistivity | 24 ohm-cir-mil/ft | AA; Typical at 68°F |
Thermal Properties |
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CTE, linear 68°F | 13.1 µin/in-°F | AA; Typical; Average over 68-212°F range. |
CTE, linear 250°C | 25.2 µm/m-°C | Estimated from trends in similar Al alloys. 20-300°C. |
Specific Heat Capacity | 0.896 J/g-°C | |
Thermal Conductivity | 1160 BTU-in/hr-ft²-°F | AA; Typical at 77°F |
Melting Point | 1080 - 1205 °F | AA; Typical range based on typical composition for wrought products 1/4 inch thickness or greater; Eutectic melting can be completely eliminated by homogenization. |
Solidus | 1080 °F | AA; Typical |
Liquidus | 1205 °F | AA; Typical |
Processing Properties |
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Solution Temperature | 985 °F | |
Aging Temperature | 320 °F | Rolled or drawn products; hold at temperature for 18 hr |
Aging Temperature | 350 °F | Extrusions or forgings; hold at temperature for 8 hr |
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References for this datasheet.
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