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PRODUCT DATA of AA2024-T6, T62 |
Material | AA2024-T6, T62 |
Product Type | rod, bar, extrusion, plate |
Chemical Composition | 4.5% Cu, 1.5% Mg, 0.6% Mn, Rem. Al |
Name of Manufacturer | Corus |
EXPERIENCE IN PRACTICE |
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Development Status | Commercial Product |
Cost Range | Very Low |
Equivalent Designations | Aluminium-Copper Alloy (ISO AlCu4Mg1), BS L97, BS L98, AFNOR A-U4G1, DIN 1725, AA 2024 |
Space Experience | Good |
PHYSICAL PROPERTIES |
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Crystal Structure | Face centered cubic (fcc) |
Specific Gravity | 2.77 |
Magnetic Properties | Nonmagnetic |
MECHANICAL PROPERTIES |
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Ultimate Tensile Strength | 427 to 441 MPa Data Quality: Limited Laboratory testing |
Proof Stress (0.2%) | 345 MPa Data Quality: Limited Laboratory testing |
Elongation | 5 % Data Quality: Limited Laboratory testing |
THERMAL PROPERTIES |
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Temperature Range | 160 °C(maximum) |
RELEVANT PROPERTIES FOR USE IN SPACE COMMUNITY |
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General Corrosion Status | Requires specific corrosion protection |
Stress Corrosion Status | Moderate Resistance to SCC: Table 2 Remark: acc. to ECSS-Q-ST-70-36C. Requires Stress corrosion evalution form Test: ECSS-Q-70-37C: Data Quality: Design Data |
EMF vs SCE | -0.62 V |
Bimetallic Corrosion | Can be used in a non-controlled environment with: Al+alloys, Cd, Sn-Pb alloys, Sn, Pb Can be used in a clean room environment with: as above and Mg, Ni, Monel, Inconel, Ni-Mo alloys, 300 series SS, 400 series SS, Ti and Ti alloys, Zn, Be Needs specific measures: All others Test: ECSS-Q-ST-70C Rev.1 table 5.1: Data Quality: Design Data |
FLUID SYSTEMS COMPATIBILITY |
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Gaseous Oxygen (GOX) | Meets the mechanical impact requirements. No batch test required |
Liquid Oxygen (LOX) | Meets the mechanical impact requirements. No batch test required. |
Nitrogen Tetroxide (N2O4) | SCC susceptibility is low and no fluid decomposition |
Hydrazine (HDZE) | SCC susceptibility is low and no fluid decomposition |
SPECIAL RECOMMENDATIONS |
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Special Recommendations | For precipitation hardened parts, heating above the precipitation temperature may result in susceptibility to intergranular and stress corrosion. · The room-temperature aged conditions may become susceptible to intergranular corrosion if the alloy is heated above 65°C. |