Product Details, Specifications, and Technical Information
Aluminum Sheet 7075 O Temper Clad has high strength after heat treatment, light weight, good fatigue resistance, excellent 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.
HEAT TREATMENT IS NECESSARY TO PROVIDE STRENGTH, AS O TEMPER IS EXTREMELY SOFT

Dimension Name | Specification |
Thickness | 0.071 |
Max Width | 48 |
Max Length | 120 |
Alloy | 7075 |
Temper | O |
MTR Availability | Yes |
Material | Aluminum |
Shape | Sheet/Plate |
Surface | Clad |
Custom Cut Warehouse | 1 |
Weight/Lineal Foot | ||
1.05 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 |
Brinell Hardness 500 kg load | 60 |
Rockwell Hardness B Scale | 17 |
Density g/cm^3 | 2 |
Elongation Typical % | 10 min |
Melting Point °F | 890 - 1175 |
Modulus of Elasticity KSI x 10^3 | 10 |
Specific Heat BTU/lb-°F (32-212F) | 2 |
Tensile Strength KSI | 39 max |
Thermal Conductivity BTU-in/hr-ft^2-°F | 1200 |
Yield Strength KSI | 21 max |
Shear Strength KSI | 22 |
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 |