Aerospace Materials: CLAD 2024 SHEET T851
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 | density lb in3 (lb/in^3) | elongation pct LT (%) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| CLAD 2024 SHEET T851 0.250-0.499 A | 70 | 10.2 | 10.4 | 99 | 127 | 83 | 98 | 56 | 57 | 37 | 65 | 65 | 56 | 56 | A | T851a | 0.1 | 5 | Flat sheet and plate | 0.33 | AMS-QQ-A-250/5 | 0.250-0.499 |
| CLAD 2024 SHEET T851 0.250-0.499 B | 70 | 10.2 | 10.4 | 100 | 129 | 86 | 101 | 58 | 59 | 37 | 66 | 66 | 58 | 58 | B | T851a | 0.1 | — | Flat sheet and plate | 0.33 | AMS-QQ-A-250/5 | 0.250-0.499 |
| CLAD 2024 SHEET T851 0.500-1.000 S | 70 | 10.2 | 10.4 | 96 | 123 | 83 | 98 | 56 | 56 | 36 | 63 | 63 | 56 | 56 | S | T851a | 0.1 | 5 | Flat sheet and plate | 0.33 | AMS-QQ-A-250/5 | 0.500-1.000b |
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