Aerospace Materials: 2024-T4 SHEET
-65 to 70
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) | Fbru ksi (ksi) | Fcy ksi (ksi) | Fsu ksi (ksi) | Ftu ksi (ksi) | Fty ksi (ksi) | elongation pct (%) | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|
| 2024-T4 SHEET | -65 | 10.7 | 120 | 42 | 42 | 70 | 48 | 18 | QQ-A-250/5 | 0.010-0.249 in |
| 2024-T4 SHEET | 70 | 10.5 | 118 | 40 | 37 | 62 | 40 | 12 | AMS 4035, AMS-QQ-A-250/4 | 0.010–0.249 in (coiled sheet) |
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