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 | 0.125 |
Max Width | 48 |
Max Length | 120 |
Alloy | 7075 |
Temper | O |
MTR Availability | Yes |
Material | Aluminum |
Shape | Sheet/Plate |
Surface | Clad |
Custom Cut Warehouse | 1 |
This material meets the following specs: ASTM -B209, AMS -4048
Weight/Lineal Foot | ||
1.84 pounds |
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 |