Aerospace Materials: 6061 PLATE 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) | 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 T42 0.250-1.000 S | 70 | 9.9 | 10.1 | 30 | 14 | 3.8 | S | T42a | 0.098 | 18 | Plate | 0.33 | AMS-QQ-A-250/11 | 0.250-1.000 |
| 6061 PLATE T42 1.001-3.000 S | 70 | 9.9 | 10.1 | 30 | 14 | 3.8 | S | T42a | 0.098 | 16 | Plate | 0.33 | AMS-QQ-A-250/11 | 1.001-3.000 |
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