Aerospace Materials: CH2 17 7PH STAINLESS STEEL SHEET and PLATE SHEET TH1050 0 015 0 187 B 2 6 10 0 B 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) | 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) | basis | condition | density lb in3 (lb/in^3) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| CH2 17 7PH STAINLESS STEEL SHEET AND PLATE SHEET TH1050 0 015 0 187 B 2 6 10 0 B C2 | 70 | 29 | 30 | 317 | 365 | 254 | 267 | 179 | 185 | 117 | 183 | 184 | 167 | 167 | 11.5 | B | TH1050 | 0.276 | Sheet | 0.28 | AMS 5528 | 0.015-0.187 |
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