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Aerospace Materials: CH2 17 7PH STAINLESS STEEL SHEET and PLATE PLATE TH1050 0 188 0 500 S 2 6 10 0 B 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).

Materials Sciencematerial id: CH2 17 7PH STAINLESS STEEL SHEET and PLATE PLATE TH1050 0 188 0 500 S 2 6 10 0 B C31 row
material idtemp fE 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 LT (ksi)Fty ksi LT (ksi)G Msi (Msi)basisconditiondensity lb in3 (lb/in^3)elongation pct LT (%)formpoisson ratiospecificationthickness range
CH2 17 7PH STAINLESS STEEL SHEET AND PLATE PLATE TH1050 0 188 0 500 S 2 6 10 0 B C370293031035722824016016611418015011.5STH10500.2766Plate0.28AMS 55280.188-0.500

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