Aerospace Materials: 2024 TUBE T3
Aerospace material mechanical properties and design allowables at ambient, elevated, and cryogenic temperatures per MMPDS-11 (Metallic Materials Properties Development and Standardization). Covers primary structural alloys: aluminum (2024-T3, 7075-T6, 6061-T6, 2219-T87), titanium (Ti-6Al-4V), nickel superalloys (Inconel 718), and steels (300M, 4130, 4340).
| material id | temp f | E Msi (Msi) | Ec Msi (Msi) | Fbru ksi (ksi) | Fbru ksi 2 (ksi) | Fbry ksi (ksi) | Fbry ksi 2 (ksi) | Fcy ksi (ksi) | Fsu ksi (ksi) | Ftu ksi (ksi) | Fty ksi (ksi) | G Msi (Msi) | basis | condition | density lb in3 (lb/in^3) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 2024 TUBE T3 0.018-0.500 A | 70 | 10.5 | 10.7 | 96 | 122 | 59 | 67 | 42 | 39 | 64 | 42 | 4 | A | T3 | 0.1 | Drawn tubing | 0.33 | AMS 4086 and WW-T-700/3 | 0.018-0.500 |
| 2024 TUBE T3 0.018-0.500 B | 70 | 10.5 | 10.7 | 99 | 126 | 63 | 72 | 45 | 40 | 66 | 45 | 4 | B | T3 | 0.1 | Drawn tubing | 0.33 | AMS 4086 and WW-T-700/3 | 0.018-0.500 |
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