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Aerospace Materials: 2024 TUBE T42

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: 2024 TUBE T421 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)Fsu ksi (ksi)Ftu ksi (ksi)Fty ksi (ksi)G Msi (Msi)basisconditiondensity lb in3 (lb/in^3)formpoisson ratiospecificationthickness range
2024 TUBE T42 0.018-0.500 S7010.510.7931185361383862384ST42a0.1Drawn tubing0.33WW-T-700/30.018-0.500

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