Aerospace Materials: CH2 15 5PH STAINLESS STEEL PLATE PLATE H1025A 3 001 4 000 S 2 6 7 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 LT (ksi) | Fty ksi LT (ksi) | G Msi (Msi) | RA pct LT (%) | basis | condition | density lb in3 (lb/in^3) | elongation pct LT (%) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| CH2 15 5PH STAINLESS STEEL PLATE PLATE H1025A 3 001 4 000 S 2 6 7 0 C C4 | 70 | 28.5 | 29.2 | 155 | 145 | 11.2 | 40 | S | H1025a | 0.283 | 12 | Plate | 0.27 | AMS 5862 | 3.001-4.000 |
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