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Aluminum 6061-T4; 6061-T451
Categories: Metal; Nonferrous Metal; Aluminum Alloy; 6000 Series Aluminum Alloy

Material Notes: Information provided by Alcoa 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.

Uses: 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.

Data points with the AA note have been provided by the Aluminum Association, Inc. and are NOT FOR DESIGN.

Composition Notes:
Composition information provided by the Aluminum Association and is not for design.

Key Words: al6061, AD-33 (Russia); AA6061-T451; AA6061-T4, UNS A96061; ISO AlMg1SiCu; Aluminum 6061-T451; Aluminium 6061-T4; Aluminium 6061-T451; Al6061-T4
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Physical PropertiesMetricEnglishComments
Density 2.70 g/cc0.0975 lb/in³AA; Typical
 
Mechanical PropertiesMetricEnglishComments
Hardness, Brinell 6565AA; Typical; 500 g load; 10 mm ball
Hardness, Knoop 8888Converted from Brinell Hardness Value
Hardness, Vickers 7575Converted from Brinell Hardness Value
Tensile Strength, Ultimate 241 MPa35000 psiAA; Typical
Tensile Strength, Yield 145 MPa21000 psiAA; Typical
Elongation at Break 22 %
@Thickness 1.59 mm
22 %
@Thickness 0.0625 in
AA; Typical
 25 %
@Diameter 12.7 mm
25 %
@Diameter 0.500 in
AA; Typical
Modulus of Elasticity 68.9 GPa10000 ksiAA; Typical; Average of tension and compression. Compression modulus is about 2% greater than tensile modulus.
Poissons Ratio 0.330.33Estimated from trends in similar Al alloys.
Fatigue Strength 96.5 MPa
@# of Cycles 5.00e+8
14000 psi
@# of Cycles 5.00e+8
completely reversed stress; RR Moore machine/specimen
Machinability 50 %50 %0-100 Scale of Aluminum Alloys
Shear Modulus 26.0 GPa3770 ksiEstimated from similar Al alloys.
Shear Strength 165 MPa24000 psiAA; Typical
 
Electrical PropertiesMetricEnglishComments
Electrical Resistivity 0.00000432 ohm-cm
@Temperature 20.0 °C
0.00000432 ohm-cm
@Temperature 68.0 °F
AA; Typical
 
Thermal PropertiesMetricEnglishComments
CTE, linear  23.6 µm/m-°C
@Temperature 20.0 - 100 °C
13.1 µin/in-°F
@Temperature 68.0 - 212 °F
AA; Typical; average over range
 25.2 µm/m-°C
@Temperature 20.0 - 300 °C
14.0 µin/in-°F
@Temperature 68.0 - 572 °F
Specific Heat Capacity 0.896 J/g-°C0.214 BTU/lb-°F
Thermal Conductivity 154 W/m-K1070 BTU-in/hr-ft²-°FAA; Typical at 77°F
Melting Point 582 - 651.7 °C1080 - 1205 °FAA; Typical range based on typical composition for wrought products >= 1/4 in. thickness. Eutectic melting can be eliminated by homogenization.
Solidus 582 °C1080 °FAA; Typical
Liquidus 651.7 °C1205 °FAA; Typical
 
Processing PropertiesMetricEnglishComments
Solution Temperature 529 °C985 °F
Aging Temperature 160 °C320 °FRolled or drawn products; hold at temperature for 18 hr
 177 °C350 °FExtrusions or forgings; hold at temperature for 8 hr
 
Component Elements PropertiesMetricEnglishComments
Aluminum, Al 95.8 - 98.6 %95.8 - 98.6 %As remainder
Chromium, Cr 0.04 - 0.35 %0.04 - 0.35 %
Copper, Cu 0.15 - 0.40 %0.15 - 0.40 %
Iron, Fe <= 0.70 %<= 0.70 %
Magnesium, Mg 0.80 - 1.2 %0.80 - 1.2 %
Manganese, Mn <= 0.15 %<= 0.15 %
Other, each <= 0.05 %<= 0.05 %
Other, total <= 0.15 %<= 0.15 %
Silicon, Si 0.40 - 0.80 %0.40 - 0.80 %
Titanium, Ti <= 0.15 %<= 0.15 %
Zinc, Zn <= 0.25 %<= 0.25 %

References for this datasheet.

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