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.

Dimension Name | Specification |
Thickness | 0.375 |
Width | 1 |
Max Length | 144 |
Alloy | 7075 |
Temper | T6 |
Production Method | Cold Finish |
MTR Availability | Yes |
Material | Aluminum |
Shape | Bar-Rectangle |
Custom Cut Warehouse | 1 |
This material meets the following specs: ASTM -B211, AMS -QQ-A-225/9, AMS -4122
Weight/Lineal Foot | ||
0.46 pounds |
Mechanical Properties | |
Property | Value |
Brinell Hardness 500 kg load | 150 |
Rockwell Hardness B Scale | 87 |
Melting Point °F | 890 - 1180 |
Modulus of Elasticity KSI x 10^3 | 10 |
Density g/cm^3 | 2 |
Elongation Typical % | 11 |
Specific Heat BTU/lb-°F (32-212F) | 2 |
Thermal Conductivity BTU-in/hr-ft^2-°F | 900 |
Tensile Strength KSI | 83 |
Yield Strength KSI | 73 |
Shear Strength KSI | 48 |
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 |