Product Details, Specifications, and Technical Information
Aluminum Round Bar 7075-T7351 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 |
Diameter | 3 |
Max Length | 144 |
MTR Availability | Yes |
Full Length | true |
Material | Aluminum |
Shape | Bar-Round |
Custom Cut Warehouse | 1 |
Alloy | 7075 |
Temper | T7351 |
Production Method | Cold Finished |
This material meets the following specs: ASTM -B211, AMS -QQ-A-225/9, AMS -4124
Weight/Lineal Foot | ||
8.6 pounds |
Mechanical Properties | |
Property | Value |
Density g/cm^3 | 3 |
Yield Tensile Strength KSI | 63 |
Ultimate Tensile Strength KSI | 73 |
Brinell Hardness 500 kg load | 135 |
Rockwell Hardness B Scale | 82 |
Elongation % in 2 in. | 8 |
Melting Point °F | 890 - 1180 |
Shear Strength KSI | 44 |
Machinability % | 70 |
Electrical Conductivity % IACS | 33 |
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 |