Aerospace Materials: 7049 EXTRUSION T73511
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) | Ftu ksi LT (ksi) | Ftu ksi ST (ksi) | Fty ksi (ksi) | Fty ksi LT (ksi) | Fty ksi ST (ksi) | G Msi (Msi) | basis | condition | density lb in3 (lb/in^3) | elongation pct (%) | elongation pct LT (%) | elongation pct ST (%) | form | poisson ratio | specification |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 7049 EXTRUSION T73511 ANY S T3 7 3 0e C1 | 70 | 10.5 | 11 | 110 | 144 | 85 | 105 | 65 | 40 | 74 | 70 | — | 64 | 60 | — | 4 | S | T73511 | 0.103 | 7 | 5 | — | Extrusion | 0.33 | AMS 4157 and AMS 4343 |
| 7049 EXTRUSION T73511 ANY S T3 7 3 0e C2 | 70 | 10.5 | 11 | 110 | 144 | 85 | 105 | 65 | 40 | 74 | 70 | 70 | 64 | 60 | 60 | 4 | S | T73511 | 0.103 | 7 | 5 | 5 | Extrusion | 0.33 | AMS 4157 and AMS 4343 |
| 7049 EXTRUSION T73511 ANY S T3 7 3 0e C3 | 70 | 10.5 | 11 | 107 | 140 | 83 | 101 | 63 | 39 | 72 | 68 | 68 | 62 | 58 | 58 | 4 | S | T73511 | 0.103 | 7 | 5 | 5 | Extrusion | 0.33 | AMS 4157 and AMS 4343 |
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