Aerospace Materials: CLAD 2424 SHEET 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) | Fcy ksi LT (ksi) | Fsu ksi (ksi) | Ftu ksi (ksi) | Ftu ksi LT (ksi) | Fty ksi (ksi) | Fty ksi LT (ksi) | basis | condition | elongation pct LT (%) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| CLAD 2424 SHEET T3 0.063-0.128 A | 70 | 10.3 | 10.5 | 94 | 121 | 60 | 70 | 40 | 43 | 41 | 64 | 61 | 46 | 40 | A | T3 | 15 | Sheet | 0.34 | AMS 4270 | 0.063-0.128 |
| CLAD 2424 SHEET T3 0.063-0.128 B | 70 | 10.3 | 10.5 | 98 | 126 | 66 | 77 | 44 | 47 | 43 | 65 | 64 | 49 | 44 | B | T3 | — | Sheet | 0.34 | AMS 4270 | 0.063-0.128 |
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