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Aerospace Materials: 2024 PLATE T851

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 PLATE T8514 rows
material idtemp fFbru 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)basisconditiondensity lb in3 (lb/in^3)elongation pct LT (%)formspecificationthickness range
2024 PLATE T851 0.250-0.499 A701021318610158593867675858AT8510.15PlateAMS-QQ-A-250/40.250-0.499
2024 PLATE T851 0.250-0.499 B701031338910560613968686060BT8510.15PlateAMS-QQ-A-250/40.250-0.499
2024 PLATE T851 0.500-1.000 S701001298610158583766665858ST8510.15PlateAMS-QQ-A-250/40.500-1.000
2024 PLATE T851 1.001-1.499 S70100129859956573766665757ST8510.15PlateAMS-QQ-A-250/41.001-1.499

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