Aluminum 7075-T6 is a high-strength aluminum alloy with zinc as its primary alloying element. It has the highest strength-to-weight ratio of common aluminum alloys and is extensively used in aerospace structural applications where strength is critical.
70/100
±0.005 mm
Aluminum Alloys
| Property | Value |
|---|---|
| Tensile Strength | 572 MPa (83 ksi) |
| Yield Strength | 503 MPa (73 ksi) |
| Hardness | 150 HB |
| Density | 2.81 g/cm³ |
| Machinability Rating | 70/100 |
| Thermal Conductivity | 130 W/m·K |
| Melting Point | 477–635 °C |
| Tolerance | ±0.005 mm |
Aircraft structures
Gears
Shafts
High-stress fittings
Missile parts
Rock climbing equipment
Tolerance: ±0.005 mm (±0.0002")
View Details →Tolerance: ±0.005 mm (±0.0002")
View Details →Tolerance: ±0.005 mm
View Details →Tolerance: ±0.005 mm
View Details →Tolerance: ±0.01 mm (prototype standard)
View Details →Tolerance: ±0.005 mm (finished)
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