7075 T6 Aluminum, High Strength

Much stronger than 5052 and 6061 aluminum, 7075 was developed for use in aircraft frames. 7075 is not formable, and tends to spring back when bent, unlike both 6061 and 5052.

Common Uses
Common use 1 - Longer name example here
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Common use 2
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Common use 3 - Medium length
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Available Sheet Thicknesses

101 Copper
0.024" (24 Ga.)
In stock
Viewspecs
Material Details
Thickness
0.020”
Thickness Tolerance
+/- 0.025”
Material
Copper
Type
Copper
Alloy
Copper 101, H00 to H01 temper
Finish
Mill Finish
Protective Film
None
Supported Services
Tapping
Countersinking
Deburring
Bending
Bead Blasting
Brushed Surface Graining
Powder Coating
Design Rules
Maximum Part Size
35.500" x 11.500"
Minimum Part Size (length or width)
0.100"
Min Recommended Hole Size
0.100"
Min Hole Size
0.100"
Min Recommended Channel Width
0.100"
Min Recommended Wall Thickness
0.100"
Max Recommended Aspect Ratio
0.100"
Kerf (Laser Cut Width)
0.100"
Material Properties
*Note: Physical and mechanical properties are not guaranteed. They are intended only as a basis for comparison and not for design purposes.
Tensile Strength (Ultimate)
26 ksi
Tensile Strength (Yield)
6 ksi
Brinell Hardness
55 kgf / mm^2
Elongation at Break
20%
Bend Parameters
Glossary of terms
View our guide about ordering bent metal parts
View Guide
K-Factor
0.313"
Minimum Flange Support
Angle
0.039"
0.039"
0.039"
0.039"
Full name
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Jan 11, 2050
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Full name
Company name
14
Team name
Jan 11, 2050
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Full name
Company name
14
Team name
Jan 11, 2050
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0.024" (24 Ga.)
0.024" (24 Ga.)
0.024" (24 Ga.)