All data is for information only------(Home) | |
---|---|
PRODUCT DATA of AA7050-T76 |
Material | AA7050-T76 |
General Information | Aluminium-Zinc-Copper-magnesium Alloy which has a good combination of strength, fracture toughness and corrosion resistance |
Processing and Assembly | Solution heat treated and then artificially overaged in order to achieve a good exfoliation corrosion resistance |
Product Type | sheet |
Chemical Composition | Al-6.2Zn-2.25Mg-2.3Cu-0.12Zr |
EXPERIENCE IN PRACTICE |
---|
Development Status | Commercial Product |
Equivalent Designations | AA 7050, UNS A97050 |
PHYSICAL PROPERTIES |
---|
Crystal Structure | Face centered cubic (fcc) |
Magnetic Properties | Nonmagnetic |
ELASTIC PROPERTIES |
---|
Tensile Modulus | 70.3 GPa |
Shear Modulus | 26.9 GPa |
MECHANICAL PROPERTIES |
---|
Ultimate Tensile Strength | 566 to 569 MPa |
Proof Stress (0.2%) | 526 to 527 MPa |
Elongation | 10 to 10.9 % |
Shear Strength | 345 to 359 MPa |
RELEVANT PROPERTIES FOR USE IN SPACE COMMUNITY |
---|
General Corrosion Status | Requires specific corrosion protection |
Stress Corrosion Status | Moderate Resistance to SCC: Table 2 Remark: Requires Stress corrosion evaluation form Data Quality: Design Data |
Bimetallic Corrosion | Can be used in a non-controlled environment: Al alloys, Cd Can be used in a clean room environment: Mg, Sn-Pb alloys (all), Sn, Pb, Zn, Be Needs specific measures: All others Test:ECSS-Q-ST-70C Rev.1 Table 5.1 Data Quality: Design Data |
SPECIAL RECOMMENDATIONS |
---|
Lessons Learned | In some cases, this alloy responds poorly to black anodising. |