Aerospace Materials: CH2 15 5PH STAINLESS STEEL PLATE PLATE H1025A 2 001 3 000 S 2 6 7 0 C C3
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) | Fbru ksi (ksi) | Fbru ksi 2 (ksi) | Fbry ksi (ksi) | Fbry ksi 2 (ksi) | Fcy ksi (ksi) | Fcy ksi LT (ksi) | Fsu ksi (ksi) | Ftu ksi (ksi) | Ftu ksi LT (ksi) | Fty ksi (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 2 001 3 000 S 2 6 7 0 C C3 | 70 | 28.5 | 29.2 | 257 | 331 | 211 | 246 | 150 | 146 | 96 | 154 | 155 | 143 | 145 | 11.2 | 40 | S | H1025a | 0.283 | 12 | Plate | 0.27 | AMS 5862 | 2.001-3.000 |
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