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Aerospace Materials: CH2 AISI 1025 CARBON STEEL BAR ALL NA SB 2 2 1 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 AISI 1025 CARBON STEEL BAR ALL NA SB 2 2 1 0 B C31 row
material idtemp fE Msi (Msi)Ec Msi (Msi)Fbru ksi 2 (ksi)Fcy ksi (ksi)Fcy ksi LT (ksi)Fcy ksi ST (ksi)Fsu ksi (ksi)Ftu ksi (ksi)Ftu ksi LT (ksi)Ftu ksi ST (ksi)Fty ksi (ksi)Fty ksi LT (ksi)Fty ksi ST (ksi)G Msi (Msi)basisconditiondensity lb in3 (lb/in^3)formpoisson ratiospecificationthickness range
CH2 AISI 1025 CARBON STEEL BAR ALL NA SB 2 2 1 0 B C3702929903636363555555536363611SbAll0.284Bar0.32AMS 5075, AMS 5077 ASTM A 108 AMS-T-5066a and...

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