Aerospace Materials: CLAD 2024 SHEET T42
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 T42 0.008-0.009 A | 70 | 9.5 | 9.7 | 88 | 109 | 60 | 72 | 38 | 37 | 33 | 55 | 55 | 34 | 34 | A | T42a | 0.1 | 10 | Flat sheet and plate | 0.33 | AMS-QQ-A-250/5 | 0.008-0.009 |
| CLAD 2024 SHEET T42 0.008-0.009 B | 70 | 9.5 | 9.7 | 91 | 113 | 61 | 74 | 39 | 38 | 34 | 57 | 57 | 35 | 35 | B | T42a | 0.1 | — | Flat sheet and plate | 0.33 | AMS-QQ-A-250/5 | 0.008-0.009 |
| CLAD 2024 SHEET T42 0.010-0.062 A | 70 | 9.5 | 9.7 | 91 | 113 | 60 | 72 | 38 | 37 | 34 | 57 | 57 | 34 | 34 | A | T42a | 0.1 | — | Flat sheet and plate | 0.33 | AMS-QQ-A-250/5 | 0.010-0.062 |
| CLAD 2024 SHEET T42 0.010-0.062 B | 70 | 9.5 | 9.7 | 94 | 117 | 61 | 74 | 39 | 38 | 35 | 59 | 59 | 35 | 35 | B | T42a | 0.1 | — | Flat sheet and plate | 0.33 | AMS-QQ-A-250/5 | 0.010-0.062 |
| CLAD 2024 SHEET T42 2.001-3.000 S | 70 | 9.5 | 9.7 | — | — | — | — | — | — | — | — | 56 | — | 36 | S | T42a | 0.1 | 4 | Flat sheet and plate | 0.33 | AMS-QQ-A-250/5 | 2.001-3.000b |
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