Aerospace Materials: CLAD 2014 SHEET T62
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) | G Msi (Msi) | basis | condition | density lb in3 (lb/in^3) | elongation pct LT (%) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| CLAD 2014 SHEET T62 0.020-0.039 A | 70 | 10.7 | 10.9 | 93 | 117 | 76 | 86 | 54 | 55 | 37 | 62 | 61 | 54 | 53 | 4 | A | T62b | 0.101 | 7 | Sheet | 0.33 | AMS-QQ-A-250/3 | 0.020-0.039 |
| CLAD 2014 SHEET T62 0.020-0.039 B | 70 | 10.7 | 10.9 | 96 | 121 | 78 | 89 | 56 | 57 | 38 | 64 | 63 | 56 | 55 | 4 | B | T62b | 0.101 | — | Sheet | 0.33 | AMS-QQ-A-250/3 | 0.020-0.039 |
| CLAD 2014 SHEET T62 0.040-0.249 A | 70 | 10.7 | 10.9 | 97 | 123 | 80 | 91 | 57 | 58 | 39 | 65 | 64 | 57 | 56 | 4 | A | T62b | 0.101 | 8 | Sheet | 0.33 | AMS-QQ-A-250/3 | 0.040-0.249 |
| CLAD 2014 SHEET T62 0.040-0.249 B | 70 | 10.7 | 10.9 | 100 | 127 | 83 | 94 | 59 | 60 | 40 | 67 | 66 | 59 | 58 | 4 | B | T62b | 0.101 | — | Sheet | 0.33 | AMS-QQ-A-250/3 | 0.040-0.249 |
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