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PRODUCT DATA of AA5456-H112 |
Material | AA5456-H112 |
Processing and Assembly | Applies to products that may acquire some strain hardening during working at elevated temperature and for which there are mechanical property limits. |
Chemical Composition | Al-5.1Mg-0.8Mn-0.12Cr |
EXPERIENCE IN PRACTICE |
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Development Status | Commercial Product |
Cost Range | Low |
Equivalent Designations | AA 5456 |
Space Experience | Good |
PHYSICAL PROPERTIES |
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Crystal Structure | Face centered cubic (fcc) |
Specific Gravity | 2.65 |
Magnetic Properties | Nonmagnetic |
ELASTIC PROPERTIES |
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Shear Modulus | 27.1 GPa |
Poisson Ratio | 0.33 |
MECHANICAL PROPERTIES |
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Ultimate Tensile Strength | 283 MPa |
Proof Stress (0.2%) | 124 MPa |
Elongation | 12 % |
Hardness | 70 HB |
ELECTRICAL PROPERTIES |
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Electrical Volume Resistivity | 5.9e-8 ohm.m |
THERMAL PROPERTIES |
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Temperature Range | 66 °C(maximum) |
Thermal Conductivity | 117 W/m.K |
Thermal Expansion Coefficient | 23.9 µstrain/°C |
Specific Heat | 0.963 J/g.K |
Melting Range | 571 to 638 °C |
RELEVANT PROPERTIES FOR USE IN SPACE COMMUNITY |
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EMF vs SCE | -0.79 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 Remark: ECSS-Q-ST-70C Rev.1 table 5.1 Data Quality: Design Data All others |
SPECIAL RECOMMENDATIONS |
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Lessons Learned | The alloy is not recommended 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 |