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Aluminum Plate 7075-T7351 has high strength, light weight, good fatigue resistance, good 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 | 0.5 |
Max Width | 48 |
Max Length | 120 |
Alloy | 7075 |
Temper | T7351 |
Material | Aluminum |
Shape | Sheet/Plate |
MTR Availability | Yes |
RoHS | Yes |
REACH | Yes |
Custom Cut Warehouse | 1 |
Weight/Lineal Foot | ||
7.35 pounds |
Mechanical Properties | |
Property | Value |
Density g/cm^3 | 3 |
Rockwell Hardness B Scale | 82 |
Yield Tensile Strength KSI | 63 |
Melting Point °F | 890 - 1180 |
Shear Strength KSI | 44 |
Elongation % in 2 in. | 8 |
Machinability % | 70 |
Ultimate Tensile Strength KSI | 73 |
Brinell Hardness 500 kg load | 135 |
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 |