| All data is for information only------(Home) | |
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| PRODUCT DATA of AA3004-H32 |
| Material | AA3004-H32 |
| Processing and Assembly | Strain-hardened and stabilized. Applies to products in the magnesium-aluminum class which will age-soften at room temperature after strain-hardening. These products are strainhardened to the desired amount and then subjected to a low temperature thermal operation which results in a improved ductility. The number following this designation indicates the degree of strain-hardening remaining after the stabilization treatment. |
| Chemical Composition | 0.8-1.3Mg, 1-1.5Mn, rem Al |
| EXPERIENCE IN PRACTICE |
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| Development Status | Commercial Product |
| Cost Range | Low |
| Lot Reproducibility | Good |
| Equivalent Designations | A-M1G, AA 3004 |
| Space Experience | Good |
| PHYSICAL PROPERTIES |
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| Crystal Structure | Face centered cubic (fcc) |
| Specific Gravity | 2.72 |
| Magnetic Properties | Nonmagnetic |
| ELASTIC PROPERTIES |
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| Tensile Modulus | 69 GPa |
| Shear Modulus | 25 GPa |
| Poisson Ratio | 0.35 |
| MECHANICAL PROPERTIES |
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| Ultimate Tensile Strength | 193 to 241 MPa |
| Proof Stress (0.2%) | 145 MPa(minimum) |
| Elongation | 6 %(minimum) |
| Fatigue Limit | 103 MPa |
| Hardness | 72 Hv |
| Shear Strength | 117 MPa |
| ELECTRICAL PROPERTIES |
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| Electrical Volume Resistivity | 4.1e-8 ohm.m |
| Electrical Conductivity | 42 %IACS |
| THERMAL PROPERTIES |
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| Thermal Conductivity | 163 W/m.K |
| Specific Heat | 0.893 J/g.K |
| Melting Range | 629 to 654 °C |
| RELEVANT PROPERTIES FOR USE IN SPACE COMMUNITY |
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| General Corrosion Status | No specific corrosion protection required |
| Stress Corrosion Status | High Resistance to SCC: Table 1
Data Quality: Design Data |
| EMF vs SCE | -0.76 V |
| 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 Data Quality: Design Data |