Aerospace Materials: 2024 SHEET T4
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 | Fbru ksi (ksi) | Fbru ksi 2 (ksi) | Fbry ksi (ksi) | Fbry ksi 2 (ksi) | Fcy ksi (ksi) | Fcy ksi LT (ksi) | Fsu ksi (ksi) | Ftu ksi (ksi) | Ftu ksi LT (ksi) | Fty ksi (ksi) | Fty ksi LT (ksi) | basis | condition | density lb in3 (lb/in^3) | form | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 2024 SHEET T4 0.010-0.249 A | 70 | 93 | 118 | 56 | 64 | 40 | 40 | 37 | 62 | 62 | 40 | 40 | A | T4 | 0.1 | Coiled sheet | AMS-QQ-A-250/4 | 0.010-0.249 |
| 2024 SHEET T4 0.010-0.249 B | 70 | 96 | 122 | 59 | 67 | 42 | 42 | 38 | 64 | 64 | 42 | 42 | B | T4 | 0.1 | Coiled sheet | AMS-QQ-A-250/4 | 0.010-0.249 |
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