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Product Details, Specifications, and Technical Information

Aluminum Cold Finish Rectangle Bar 7075-T6 has high strength, light weight, good fatigue resistance, average corrosion resistance, and average machinability. 7075, one of the strongest aluminum alloys, was specifically designed for aircraft frames and offers strength slightly superior to steel while maintaining the light weight of aluminum. It is typically used in aerospace, high-end automotive, and defense applications.

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Dimension Name Specification
Thickness 0.25
Width 2
Max Length 144
MTR Availability Yes
Material Aluminum
Shape Bar-Rectangle
Custom Cut Warehouse 1
Alloy 7075
Temper T6
Production Method Cold Finished
Material Specifications

This material meets the following specs: ASTM -B211, AMS -QQ-A-225/9, AMS -4122

Weight/Lineal Foot
0.62 pounds
Please note that this data is to be used ONLY FOR REFERENCE, NOT FOR DESIGN, and by using it,you agree that any decisions you make regarding materials for your project are at your own discretion.
Mechanical Properties
Property Value
Ultimate Tensile Strength KSI 83
Density g/cm^3 3
Yield Tensile Strength KSI 73
Brinell Hardness 500 kg load 150
Rockwell Hardness B Scale 87
Melting Point °F 890 - 1180
Shear Strength KSI 48
Electrical Conductivity % IACS 33
Machinability % 70
Elongation % in 2 in. 11
Chemistry Information: 7075 Aluminum
Element Percentage
Al 90
Cr 0.18 - 0.28
Cu 1.2 - 2
Fe 0.5 max
Mg 2.1 - 2.9
Mn 0.3 max
Si 0.4 max
Ti 0.2 max
Zn 5.1 - 6.1
Zr+Ti 0.25 max
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