Aerospace Materials: CH2 AM 355 STAINLESS STEEL BAR and FORGING SCT1000 NA S 2 6 2 0 C 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) | Ftu ksi (ksi) | Fty ksi (ksi) | G Msi (Msi) | RA pct (%) | basis | condition | density lb in3 (lb/in^3) | elongation pct (%) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| CH2 AM 355 STAINLESS STEEL BAR AND FORGING SCT1000 NA S 2 6 2 0 C C4 | 70 | 29 | 29 | 170 | 155 | 11 | 25 | S | SCT1000 | 0.282 | 12 | Bar and forging | 0.32 | AMS 5743 | . . . |
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