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Aluminum 5083-O
Categories: Metal; Nonferrous Metal; Aluminum Alloy; 5000 Series Aluminum Alloy

Material Notes: This alloy has very good corrosion resistance (susceptible to deterioration after prolonged exposure to elevated temperatures) and moderate strength. Its weldability is a plus. It finds uses in transportation, pressure vessels, cryogenics, towers and drilling rigs, gas/oil piping, ordnance, and armor plate.

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: UNS A95083; ISO AlMg4.5Mn; Aluminium 5083-O; AA5083-O; Al5083-O
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Physical PropertiesMetricEnglishComments
Density 2.66 g/cc0.0961 lb/in³AA; Typical
 
Mechanical PropertiesMetricEnglishComments
Hardness, Brinell 7777500 kg load with 10 mm ball. Calculated value.
Hardness, Knoop 100100Converted from Brinell Hardness Value
Hardness, Vickers 8787Converted from Brinell Hardness Value
Tensile Strength, Ultimate 290 MPa42000 psiAA; Typical
 41.0 MPa
@Temperature 370 °C
5950 psi
@Temperature 698 °F
 75.0 MPa
@Temperature 315 °C
10900 psi
@Temperature 599 °F
 115 MPa
@Temperature 260 °C
16700 psi
@Temperature 500 °F
 150 MPa
@Temperature 205 °C
21800 psi
@Temperature 401 °F
 215 MPa
@Temperature 150 °C
31200 psi
@Temperature 302 °F
 275 MPa
@Temperature 100 °C
39900 psi
@Temperature 212 °F
 290 MPa
@Temperature -30.0 °C
42100 psi
@Temperature -22.0 °F
 290 MPa
@Temperature 25.0 °C
42100 psi
@Temperature 77.0 °F
 295 MPa
@Temperature -80.0 °C
42800 psi
@Temperature -112 °F
 405 MPa
@Temperature -195 °C
58700 psi
@Temperature -319 °F
 >= 250 MPa
@Thickness 177.8 - 203 mm
>= 36300 psi
@Thickness 7.001 - 8.00 in
 >= 255 MPa
@Thickness 127.0 - 178 mm
>= 37000 psi
@Thickness 5.001 - 7.00 in
 >= 260 MPa
@Thickness 76.23 - 127 mm
>= 37700 psi
@Thickness 3.001 - 5.00 in
 270 - 345 MPa
@Thickness 38.13 - 76.2 mm
39200 - 50000 psi
@Thickness 1.501 - 3.00 in
 275 - 350 MPa
@Thickness 1.30 - 38.1 mm
39900 - 50800 psi
@Thickness 0.0510 - 1.50 in
Tensile Strength, Yield 145 MPa21000 psiAA; Typical
 >= 95.0 MPa
@Thickness 177.8 - 203 mm
>= 13800 psi
@Thickness 7.001 - 8.00 in
 >= 105 MPa
@Thickness 127.0 - 178 mm
>= 15200 psi
@Thickness 5.001 - 7.00 in
 >= 110 MPa
@Thickness 76.23 - 127 mm
>= 16000 psi
@Thickness 3.001 - 5.00 in
 115 - 200 MPa
@Thickness 38.13 - 76.2 mm
16700 - 29000 psi
@Thickness 1.501 - 3.00 in
 125 - 200 MPa
@Thickness 1.30 - 38.1 mm
18100 - 29000 psi
@Thickness 0.0510 - 1.50 in
 29.0 MPa
@Strain 0.2 %,
Temperature 370 °C
4210 psi
@Strain 0.2 %,
Temperature 698 °F
 50.0 MPa
@Strain 0.2 %,
Temperature 315 °C
7250 psi
@Strain 0.2 %,
Temperature 599 °F
 75.0 MPa
@Strain 0.2 %,
Temperature 260 °C
10900 psi
@Strain 0.2 %,
Temperature 500 °F
 115 MPa
@Strain 0.2 %,
Temperature 205 °C
16700 psi
@Strain 0.2 %,
Temperature 401 °F
 130 MPa
@Strain 0.2 %,
Temperature 150 °C
18900 psi
@Strain 0.2 %,
Temperature 302 °F
 145 MPa
@Strain 0.2 %,
Temperature -80.0 °C
21000 psi
@Strain 0.2 %,
Temperature -112 °F
 145 MPa
@Strain 0.2 %,
Temperature -30.0 °C
21000 psi
@Strain 0.2 %,
Temperature -22.0 °F
 145 MPa
@Strain 0.2 %,
Temperature 25.0 °C
21000 psi
@Strain 0.2 %,
Temperature 77.0 °F
 145 MPa
@Strain 0.2 %,
Temperature 100 °C
21000 psi
@Strain 0.2 %,
Temperature 212 °F
 165 MPa
@Strain 0.2 %,
Temperature -195 °C
23900 psi
@Strain 0.2 %,
Temperature -319 °F
Elongation at Break  25 %
@Temperature 25.0 °C
25 %
@Temperature 77.0 °F
 27 %
@Temperature -30.0 °C
27 %
@Temperature -22.0 °F
 30 %
@Temperature -80.0 °C
30 %
@Temperature -112 °F
 36 %
@Temperature -195 °C
36 %
@Temperature -319 °F
 36 %
@Temperature 100 °C
36 %
@Temperature 212 °F
 50 %
@Temperature 150 °C
50 %
@Temperature 302 °F
 60 %
@Temperature 205 °C
60 %
@Temperature 401 °F
 80 %
@Temperature 260 °C
80 %
@Temperature 500 °F
 110 %
@Temperature 315 °C
110 %
@Temperature 599 °F
 130 %
@Temperature 370 °C
130 %
@Temperature 698 °F
 >= 12 %
@Thickness 177.8 - 203 mm
>= 12 %
@Thickness 7.001 - 8.00 in
 >= 14 %
@Thickness 127.0 - 178 mm
>= 14 %
@Thickness 5.001 - 7.00 in
 14 - 16 %
@Thickness 76.23 - 127 mm
14 - 16 %
@Thickness 3.001 - 5.00 in
 >= 16 %
@Thickness 1.30 - 38.1 mm
>= 16 %
@Thickness 0.0510 - 1.50 in
 >= 16 %
@Thickness 38.13 - 76.2 mm
>= 16 %
@Thickness 1.501 - 3.00 in
 22 %
@Diameter 12.7 mm
22 %
@Diameter 0.500 in
AA; Typical
Modulus of Elasticity 71.0 GPa10300 ksiAA; Typical; Average of tension and compression. Compression modulus is about 2% greater than tensile modulus.
Tensile Modulus 70.3 GPa10200 ksi
Compressive Modulus 71.7 GPa10400 ksi
Notched Tensile Strength 269 MPa39000 psi2.5 cm width x 0.16 cm thick side-notched specimen, Kt = 17.
Ultimate Bearing Strength 552 MPa80100 psiEdge distance/pin diameter = 2.0
Bearing Yield Strength 248 MPa36000 psiEdge distance/pin diameter = 2.0
Poissons Ratio 0.330.33Estimated from trends in similar Al alloys.
Fatigue Strength 150 MPa
@# of Cycles 5.00e+8
21800 psi
@# of Cycles 5.00e+8
unnotched R. R. Moore rotating beam
Machinability 30 %30 %0-100 Scale of Aluminum Alloys
Shear Modulus 26.4 GPa3830 ksi
Shear Strength 172 MPa25000 psiAA; Typical
 
Electrical PropertiesMetricEnglishComments
Electrical Resistivity 0.00000598 ohm-cm
@Temperature 20.0 °C
0.00000598 ohm-cm
@Temperature 68.0 °F
AA; Typical
 
Thermal PropertiesMetricEnglishComments
CTE, linear  22.3 µm/m-°C
@Temperature -50.0 - 20.0 °C
12.4 µin/in-°F
@Temperature -58.0 - 68.0 °F
 23.8 µm/m-°C
@Temperature 20.0 - 100 °C
13.2 µin/in-°F
@Temperature 68.0 - 212 °F
AA; Typical; average over range
 24.2 µm/m-°C
@Temperature 20.0 - 100 °C
13.4 µin/in-°F
@Temperature 68.0 - 212 °F
 25.0 µm/m-°C
@Temperature 20.0 - 200 °C
13.9 µin/in-°F
@Temperature 68.0 - 392 °F
 26.0 µm/m-°C
@Temperature 20.0 - 300 °C
14.4 µin/in-°F
@Temperature 68.0 - 572 °F
Specific Heat Capacity 0.900 J/g-°C0.215 BTU/lb-°F
Thermal Conductivity 117 W/m-K810 BTU-in/hr-ft²-°FAA; Typical at 77°F
Melting Point 590.6 - 638 °C1095 - 1180 °FAA; Typical range based on typical composition for wrought products >= 1/4 in. thickness
Solidus 590.6 °C1095 °FAA; Typical
Liquidus 638 °C1180 °FAA; Typical
 
Processing PropertiesMetricEnglishComments
Annealing Temperature 413 °C775 °Fholding at temperature not required
Hot-Working Temperature 316 - 482 °C600 - 900 °F
 
Component Elements PropertiesMetricEnglishComments
Aluminum, Al 92.4 - 95.6 %92.4 - 95.6 %As remainder
Chromium, Cr 0.05 - 0.25 %0.05 - 0.25 %
Copper, Cu <= 0.10 %<= 0.10 %
Iron, Fe <= 0.40 %<= 0.40 %
Magnesium, Mg 4.0 - 4.9 %4.0 - 4.9 %
Manganese, Mn 0.40 - 1.0 %0.40 - 1.0 %
Other, each <= 0.05 %<= 0.05 %
Other, total <= 0.15 %<= 0.15 %
Silicon, Si <= 0.40 %<= 0.40 %
Titanium, Ti <= 0.15 %<= 0.15 %
Zinc, Zn <= 0.25 %<= 0.25 %

References for this datasheet.

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