Aerospace Materials: CH2 17 4PH STAINLESS STEEL FORGING TUBING and RINGS NA H925 NA S 2 6 9 0 D C2
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 | elongation pct (%) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| CH2 17 4PH STAINLESS STEEL FORGING TUBING AND RINGS NA H925 NA S 2 6 9 0 D C2 | 70 | 28.5 | 30 | 170 | 155 | 11.2 | S | H925 | 10 | . . . . | 0.27 | . . . . | . . . . |
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