Aerospace Materials: 6061 FORGING T6 and T652
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) | Fsu ksi (ksi) | Ftu ksi (ksi) | Fty ksi (ksi) | G Msi (Msi) | basis | condition | density lb in3 (lb/in^3) | elongation pct (%) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 6061 FORGING T6 AND T652 4.000 S | 70 | 9.9 | 10.1 | 61 | 76 | 54 | 61 | 36 | 25 | 38 | 35 | 3.8 | S | T6 and T652 | 0.098 | 7 | Die forging | 0.33 | AMS 4127, MIL-A-22771, and QQ-A-367 | 4.000a |
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