Aerospace Materials: CH2 AM 355 STAINLESS STEEL PLATE PLATEB SCT 1000 0 187 S 2 6 2 0 D C4
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) | G Msi (Msi) | basis | condition | density lb in3 (lb/in^3) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|
| CH2 AM 355 STAINLESS STEEL PLATE PLATEB SCT 1000 0 187 S 2 6 2 0 D C4 | 70 | 29 | 29 | 11 | S | SCT 1000 | 0.282 | Plateb | 0.32 | AMS 5549a | <0.187 |
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