Aerospace Materials: 6061 PLATE T451
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 LT (ksi) | Fsu ksi (ksi) | Ftu ksi LT (ksi) | Fty ksi LT (ksi) | G Msi (Msi) | basis | condition | density lb in3 (lb/in^3) | elongation pct (%) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 6061 PLATE T451 0.250-2.000 A | 70 | 9.9 | 10.1 | 48 | 63 | 22 | 26 | 16 | 20 | 30 | 16 | 3.8 | A | T451 | 0.098 | — | Plate | 0.33 | AMS 4026 and AMS-QQ-A-250/11 | 0.250-2.000 |
| 6061 PLATE T451 0.250-2.000 B | 70 | 9.9 | 10.1 | 52 | 67 | 25 | 29 | 18 | 21 | 32 | 18 | 3.8 | B | T451 | 0.098 | — | Plate | 0.33 | AMS 4026 and AMS-QQ-A-250/11 | 0.250-2.000 |
| 6061 PLATE T451 2.001-3.000 A | 70 | 9.9 | 10.1 | — | — | — | — | — | — | 30 | 16 | 3.8 | A | T451 | 0.098 | 16 | Plate | 0.33 | AMS 4026 and AMS-QQ-A-250/11 | 2.001-3.000 |
| 6061 PLATE T451 2.001-3.000 B | 70 | 9.9 | 10.1 | — | — | — | — | — | — | 32 | 18 | 3.8 | B | T451 | 0.098 | — | Plate | 0.33 | AMS 4026 and AMS-QQ-A-250/11 | 2.001-3.000 |
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