All data is for information only------(Home) | |
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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 |
MECHANICAL PROPERTIES |
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Ultimate Tensile Strength | 379 MPa |
Proof Stress (0.2%) | 317 Mpa |
Elongation | 9 % |
Fatigue Limit | 110 MPa @5x10^8 cycles |
Hardness | 75 HRb |
Shear Strength | 262 MPa |
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 |
Specific Heat | 0.85 J/g.K |
Melting Range | 532 to 571 °C |
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 |