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Aerospace Materials: CH2 9NI 4CO 0 20C STEEL PLATE PLATE QUENCHED and TEMPERED 0 250 SA 2 4 2 0 B C1

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 9NI 4CO 0 20C STEEL PLATE PLATE QUENCHED and TEMPERED 0 250 SA 2 4 2 0 B C11 row
material idtemp fE Msi (Msi)Ec Msi (Msi)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 (%)basisconditiondensity lb in3 (lb/in^3)elongation pct LT (%)formpoisson ratiospecificationthickness range
CH2 9NI 4CO 0 20C STEEL PLATE PLATE QUENCHED AND TEMPERED 0 250 SA 2 4 2 0 B C17028.828.818818711418619017317511.145SaQuenched and tempered0.2835Plate0.3AMS 6523<0.250

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