1
Dimension(s) for this product
- Across Flats: 1.0625 "
Product Details, Specifications, and Technical Information
1-1/16 inch Aluminum Hex 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 |
| Max Length | 144 |
| Across Flats | 1.0625 |
| Alloy | 7075 |
| Temper | T7351 |
| Production Method | Cold Finished |
| Material | Aluminum |
| Shape | Bar-Hex |
| MTR Availability | Yes |
| RoHS | Yes |
| REACH | Yes |
| Custom Cut Warehouse | 1 |
| Weight/Lineal Foot | ||
| 1.2 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 |
| 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 |
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