Aerospace Materials: A201 0 CASTING T7 ANY S SC2
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 | casting location | casting strength class | condition | density lb in3 (lb/in^3) | elongation pct (%) | form | poisson ratio | specification |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| A201 0 CASTING T7 ANY S SC2 | 70 | 10.3 | 10.7 | 122 | 122 | 87 | 87 | 51 | 36 | 60 | 50 | 4 | S | Designated area | 2 | T7 | 0.101 | 5 | Casting | 0.33 | AMS-A-21180 |
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