Aerospace Materials: 6061 EXTRUSION T6
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 (%) | form | poisson ratio | specification |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 6061 EXTRUSION T6 ANY A T3 6 2 0g C4 | 70 | 9.9 | 10.1 | 64 | 82 | 54 | 60 | 34 | 35 | 26 | 38 | 37 | 35 | 33 | 3.8 | A | T6, T6510, and T6511 | 0.098 | 10 | Extruded rod, bar, and shapes | 0.33 | AMS 4150, AMS 4173 & AMS-QQ-A-200/8 |
| 6061 EXTRUSION T6 ANY A T3 6 2 0g C6 | 70 | 9.9 | 10.1 | 52 | 69 | 42 | 50 | 34 | 30 | 19 | 38 | 33 | 35 | 28 | 3.8 | A | T6, T6510, and T6511 | 0.098 | 10 | Extruded rod, bar, and shapes | 0.33 | AMS 4150, AMS 4173 & AMS-QQ-A-200/8 |
| 6061 EXTRUSION T6 ANY B T3 6 2 0g C5 | 70 | 9.9 | 10.1 | 69 | 88 | 58 | 65 | 37 | 38 | 28 | 41 | 40 | 38 | 36 | 3.8 | B | T6, T6510, and T6511 | 0.098 | — | Extruded rod, bar, and shapes | 0.33 | AMS 4150, AMS 4173 & AMS-QQ-A-200/8 |
| 6061 EXTRUSION T6 ANY B T3 6 2 0g C7 | 70 | 9.9 | 10.1 | 57 | 74 | 46 | 55 | 37 | 33 | 21 | 41 | 35 | 38 | 31 | 3.8 | B | T6, T6510, and T6511 | 0.098 | — | Extruded rod, bar, and shapes | 0.33 | AMS 4150, AMS 4173 & AMS-QQ-A-200/8 |
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