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7050
Aluminum 7050 Product Guide
Applications | Aluminum 7050-T7451 Specifications | Mechanical and Chemical Data
Overview
7050 Aluminum is similar to the other popular 7000 series aluminum alloy 7075, however it is less quench sensitive. This allows the alloy to maintain strength properties over time better than other high strength alloys, especially in thick sections. 7050 T7451 also displays better corrosion resistance, exfoliation resistance, and toughness than standard high strength alloys making it very popular in the aerospace industry where it is used for bulkheads, fuselages, and wing skins.
Common Trade Names
UNS A97050, ISO AlZn6CuMgZr, AA7050-T7451, Al7050-T7451
Other Resources
Safety Data Sheet | Weight Calculator | Mill Test Reports
Products
Applications
- Aerospace Structural Parts
- Spacecraft
Aluminum 7050 Specifications
AMS | 4050 |
Mechanical Information T7451 | ||||
Density | Ultimate Tensile Strength | Yield Tensile Strength | Fatigue Strength | |
---|---|---|---|---|
Imperial | 0.102 lb/in3 | 76,000 psi | 68,000 psi | 23,000/21,800 psi |
Metric | 2.83 g/cc | 527/462 MPa | 503/386 MPa | 200 MPa |
Mechanical Information T7451 | ||||
Modulus of Elasticity | Shear Modulus | Shear Strength | Melting Point | |
---|---|---|---|---|
Imperial | 10,400 ksi | 3,900 ksi | 44,000 psi | 910-1165 F |
Metric | 71.7 GPa | 26.9 GPa | 303 MPa | 488-629 C |
Mechanical Information T7451 | ||||
Electrical Conductivity | Hardness Rockwell/Brinell | Elongation at break percentage | Poissons Ratio | Machinability Percentage |
---|---|---|---|---|
35% IACS | B84 | 10% at .5" dia. | 0.33 | 70 |
Chemistry Information
|
|
Element |
Percentage |
Al | - |
Si | 0.12 |
Fe | 0.15 |
Cu | 2 - 2.6 |
Mn | 0.1 |
Cr | 0.04 |
Mg | 1.9 - 2.6 |
Zn | 5.7 - 6.7 |
Zr | 0.08 - 0.15 |
Ti | 0.06 |