Aerospace Materials: CH2 17 4PH STAINLESS STEEL BAR BAR H925 8 000 B 2 6 9 0 E 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) | basis | condition | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|
| CH2 17 4PH STAINLESS STEEL BAR BAR H925 8 000 B 2 6 9 0 E C4 | 70 | 28.5 | 30 | 178 | 167 | 11.2 | B | H925 | Bar | 0.27 | AMS 5643 | <8.000 |
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