| All data is for information only------(Home) | |
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| PRODUCT DATA of AA5086-H34 |
| Material | AA5086-H34 |
| Chemical Composition | Al-4Mg-0.5Mn-0.2Cr |
| EXPERIENCE IN PRACTICE |
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| Development Status | Commercial Product |
| Cost Range | Low |
| Lot Reproducibility | Good |
| Equivalent Designations | AlMg4Mn;AlMg4;A-G4MC; A95086;3.3545; L-3322, AA 5086 |
| Space Experience | Good |
| PHYSICAL PROPERTIES |
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| Crystal Structure | Face centered cubic (fcc) |
| Specific Gravity | 2.67 |
| Magnetic Properties | Nonmagnetic |
| ELASTIC PROPERTIES |
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| Tensile Modulus | 71 GPa |
| Shear Modulus | 26.7 GPa |
| MECHANICAL PROPERTIES |
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| Ultimate Tensile Strength | 300 MPa(minimum) |
| Proof Stress (0.2%) | 230 MPa(minimum) |
| Elongation | 8 to 15 % |
| Hardness | 90 Hv |
| ELECTRICAL PROPERTIES |
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| Electrical Volume Resistivity | 5.6e-8 ohm.m |
| Electrical Conductivity | 31 %IACS |
| THERMAL PROPERTIES |
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| Thermal Conductivity | 126 W/m.K |
| Thermal Expansion Coefficient | 23.8 μstrain/°C |
| Specific Heat | 0.9 J/g.K |
| Melting Range | 585 to 640 °C |
| RELEVANT PROPERTIES FOR USE IN SPACE COMMUNITY |
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| General Corrosion Status | No specific corrosion protection required |
| Stress Corrosion Status | Moderate Resistance to SCC: Table 2 Remark: acc. to ECSS-Q-ST-70-36C Data Quality: Design Data |
| EMF vs SCE | -0.77 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 Remark: ECSS-Q-ST-70C Rev.1 table 5.1 Data Quality: Design Data |
| SPECIAL RECOMMENDATIONS |
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| Lessons Learned | The alloy is prohibited for continuous service at temperatures above 66°C because of accelerated aging at elevated temperatures which may increase the susceptibility of the alloy to stress corrosion cracking |