Aerospace Materials: CH2 17 7PH STAINLESS STEEL SHEET and PLATE PLATE TH1050 0 501 1 000 S 2 6 10 0 B 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) | basis | condition | density lb in3 (lb/in^3) | elongation pct LT (%) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| CH2 17 7PH STAINLESS STEEL SHEET AND PLATE PLATE TH1050 0 501 1 000 S 2 6 10 0 B C4 | 70 | 29 | 30 | 180 | 150 | 11.5 | S | TH1050 | 0.276 | 6 | Plate | 0.28 | AMS 5528 | 0.501-1.000 |
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