Aerospace Materials: CLAD 2024 SHEET T72
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) | Ftu ksi LT (ksi) | Fty ksi LT (ksi) | basis | condition | density lb in3 (lb/in^3) | elongation pct LT (%) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| CLAD 2024 SHEET T72 0.010-0.062 S | 70 | 9.5 | 9.7 | 56 | 43 | S | T72a | 0.1 | 5 | Flat sheet and plate | 0.33 | AMS-QQ-A-250/5 | 0.010-0.062 |
| CLAD 2024 SHEET T72 0.063-0.249 S | 70 | 9.5 | 9.7 | 58 | 45 | S | T72a | 0.1 | 5 | Flat sheet and plate | 0.33 | AMS-QQ-A-250/5 | 0.063-0.249 |
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