Product Details, Specifications, and Technical Information
Aluminum Sheet 7075-T6 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 | 0.125 |
Max Width | 48 |
Max Length | 120 |
Alloy | 7075 |
Temper | T6 |
Covering | Pvc 1 Side |
MTR Availability | Yes |
Full Length | true |
Material | Aluminum |
Shape | Sheet/Plate |
Custom Cut Warehouse | 1 |
This material meets the following specs: ASTM -B209, AMS -4045, AMS -QQ-A-250/12
Weight/Lineal Foot | ||
1.84 pounds |
Mechanical Properties | |
Property | Value |
Brinell Hardness 500 kg load | 150 |
Rockwell Hardness B Scale | 87 |
Density g/cm^3 | 2 |
Elongation Typical % | 11 |
Melting Point °F | 890 - 1180 |
Specific Heat BTU/lb-°F (32-212F) | 2 |
Thermal Conductivity BTU-in/hr-ft^2-°F | 900 |
Modulus of Elasticity KSI x 10^3 | 10 |
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 |