Product Details, Specifications, and Technical Information
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 | 2.5 |
Add-On Services | Guaranteed Precision Saw Cuts Available - Request Quote Today! |
Max Width | 48 |
Max Length | 120 |
Alloy | 7075 |
Temper | T7351 |
MTR Availability | Yes |
Full Length | true |
Material | Aluminum |
Shape | Sheet/Plate |
Custom Cut Warehouse | 1 |
This material meets the following specs: ASTM -B209, AMS -QQ-A-250/12, AMS -4078
Weight/Lineal Foot | ||
36.72 pounds |
Mechanical Properties | |
Property | Value |
Brinell Hardness 500 kg load | 135 |
Rockwell Hardness B Scale | 82 |
Density g/cm^3 | 2 |
Elongation Typical % | 13 |
Melting Point °F | 890 - 1180 |
Modulus of Elasticity KSI x 10^3 | 10 |
Specific Heat BTU/lb-°F (32-212F) | 2 |
Thermal Conductivity BTU-in/hr-ft^2-°F | 1080 |
Shear Strength KSI | 43 |
Tensile Strength KSI | 73 |
Yield Strength KSI | 63 |
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 |