| All data is for information only------(<---links) | |
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| PRODUCT DATA of AA4032-T6 |
| Material | AA4032-T6 |
| General Information | Superior wear resistance, eliminated the need for hard coat anodizing. High strength, low thermal expansion |
| Precautions | Typical T6 data from the Aluminium Association (AA). Not for design |
| Chemical Composition | Al-0.9Cu-1.1Mg-0.9Ni-12Si |
| EXPERIENCE IN PRACTICE |
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| Development Status | Commercial Product |
| Cost Range | Low |
| Equivalent Designations | UNS A94032; 4032-T6 |
| PHYSICAL PROPERTIES |
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| Crystal Structure | Face centered cubic (fcc) |
| Specific Gravity | 2.68 |
| Magnetic Properties | Nonmagnetic |
| ELASTIC PROPERTIES |
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| Tensile Modulus | 78.6 GPa |
| Shear Modulus | 26 GPa |
| Poisson Ratio | 0.34 |
| ELECTRICAL PROPERTIES |
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| Electrical Volume Resistivity | 4.99e-8 ohm.m |
| THERMAL PROPERTIES |
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| Thermal Conductivity | 138 W/m.K |
| Thermal Expansion Coefficient | 19.4 µstrain/°C |
| Melting Range | 532 to 571 °C |
| Specific Heat | 0.85 J/g.K |
| RELEVANT PROPERTIES FOR USE IN SPACE COMMUNITY |
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| Stress Corrosion Status | Moderate Resistance to SCC: Table 2 Remark: Requires Stress corrosion evaluation form |
| 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 |