| All data is for information only------(<---links) | |
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| PRODUCT DATA of AA7175-T736 | 
| Material | AA7175-T736 | 
| General Information | 7175 is a high strength, heat treatable, forging alloy. It has an excellent combination of toughness and strength, similar to 7075 alloy except that the 7175 version has superior toughness and tensile strength. | 
| Processing and Assembly | Solution heat treated and then artificially overaged (between T73 and T76 (now T74) | 
| Precautions | data from ASM. Not for design | 
| Chemical Composition | Al-5.6Zn-2.5Mg-1.6Cu-0.23Cr | 
| EXPERIENCE IN PRACTICE | 
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| Development Status | Commercial Product | 
| Equivalent Designations | AA 7175 | 
| Space Experience | Good | 
| PHYSICAL PROPERTIES | 
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| Crystal Structure | Face centered cubic (fcc) | 
| Magnetic Properties | Nonmagnetic | 
| ELASTIC PROPERTIES | 
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| Tensile Modulus | 72 GPa | 
| Poisson Ratio | 0.33 | 
| RELEVANT PROPERTIES FOR USE IN SPACE COMMUNITY | 
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| 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 | 
| Machinability | The alloy is machinable. However no specific comments are available. Consult the supplier. | 
| Aging | This is an age hardenable alloy. | 
| SPECIAL RECOMMENDATIONS | 
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| Lessons Learned | In some cases where the Zn content is at the high end of the composition range, this alloy responds poorly to black anodising. |