Aerospace Materials: CLAD 2014 PLATE 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 PLATE T62 0.250-0.499 S | 70 | 10.7 | 10.9 | 96 | 121 | 81 | 96 | 57 | 58 | 36 | 62 | 64 | 55 | 57 | 4 | S | T62b | 0.101 | 8 | Platea | 0.33 | AMS-QQ-A-250/3 | 0.250-0.499 |
| CLAD 2014 PLATE T62 0.500-1.000 S | 70 | 10.7 | 10.9 | 96 | 121 | 79 | 94 | 56 | 57 | 36 | 62 | 64 | 54 | 56 | 4 | S | T62b | 0.101 | 6 | Platea | 0.33 | AMS-QQ-A-250/3 | 0.500-1.000c |
| CLAD 2014 PLATE T62 1.001-2.000 S | 70 | 10.7 | 10.9 | 96 | 121 | 79 | 94 | 56 | 56 | 36 | 62 | 64 | 54 | 56 | 4 | S | T62b | 0.101 | 4 | Platea | 0.33 | AMS-QQ-A-250/3 | 1.001-2.000c |
| CLAD 2014 PLATE T62 2.001-2.500 S | 70 | 10.7 | 10.9 | 93 | 118 | 78 | 92 | 55 | 55 | 35 | 60 | 62 | 53 | 55 | 4 | S | T62b | 0.101 | 2 | Platea | 0.33 | AMS-QQ-A-250/3 | 2.001-2.500c |
| CLAD 2014 PLATE T62 2.501-3.000 S | 70 | 10.7 | 10.9 | — | — | — | — | — | — | — | — | 60 | — | 54 | 4 | S | T62b | 0.101 | 2 | Platea | 0.33 | AMS-QQ-A-250/3 | 2.501-3.000c |
| CLAD 2014 PLATE T62 3.001-4.000 S | 70 | 10.7 | 10.9 | — | — | — | — | — | — | — | — | 56 | — | 52 | 4 | S | T62b | 0.101 | 1 | Platea | 0.33 | AMS-QQ-A-250/3 | 3.001-4.000c |
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