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Aerospace Materials: 2024 BAR T351

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 BAR T3516 rows
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 (ksi)Ftu ksi LT (ksi)Fty ksi (ksi)Fty ksi LT (ksi)G Msi (Msi)basisconditiondensity lb in3 (lb/in^3)elongation pct (%)formpoisson ratiospecificationthickness range
2024 BAR T351 0.500-1.000 S7010.510.7901156374344137626145364ST3510.110Bar and rod; rolled, drawn, or cold-finished0.33AMS 4120 and AMS-QQ-A-225/60.500-1.000
2024 BAR T351 1.001-2.000 S7010.510.7901156374344137625945364ST3510.110Bar and rod; rolled, drawn, or cold-finished0.33AMS 4120 and AMS-QQ-A-225/61.001-2.000
2024 BAR T351 2.001-3.000 S7010.510.7901156374344137625745364ST3510.110Bar and rod; rolled, drawn, or cold-finished0.33AMS 4120 and AMS-QQ-A-225/62.001-3.000
2024 BAR T351 3.001-4.000 S7010.510.7901156374344137625545364ST3510.110Bar and rod; rolled, drawn, or cold-finished0.33AMS 4120 and AMS-QQ-A-225/63.001-4.000
2024 BAR T351 4.001-5.000 S7010.510.7901156374344137625445364ST3510.110Bar and rod; rolled, drawn, or cold-finished0.33AMS 4120 and AMS-QQ-A-225/64.001-5.000a
2024 BAR T351 5.001-6.000 S7010.510.7901156374344137625245364ST3510.110Bar and rod; rolled, drawn, or cold-finished0.33AMS 4120 and AMS-QQ-A-225/65.001-6.000a

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