Aerospace Materials: C355 0 CASTING UNK 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 | density lb in3 (lb/in^3) | elongation pct (%) | form | poisson ratio | specification |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| C355 0 CASTING UNK ANY S SC2 | 70 | 10.1 | 10.3 | 88 | 88 | 58 | 58 | 33 | 28 | 44 | 33 | 3.85 | S | T6 | 2 | 0.098 | 3 | Casting | 0.33 | AMS-A-21180 |
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