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Aerospace Materials: 2024 SHEET T3

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 SHEET T34 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)formpoisson ratiospecificationthickness range
2024 SHEET T3 0.010-0.128 A7010.710.91041297388394539646347424AT30.1Sheet0.33AMS 4037 and AMS-QQ-A-250/40.010-0.128
2024 SHEET T3 0.010-0.128 B7010.710.91061317590404640656448434BT30.1Sheet0.33AMS 4037 and AMS-QQ-A-250/40.010-0.128
2024 SHEET T3 0.129-0.249 A7010.710.91061317388394540656447424AT30.1Sheet0.33AMS 4037 and AMS-QQ-A-250/40.129-0.249
2024 SHEET T3 0.129-0.249 B7010.710.91071337590404641666548434BT30.1Sheet0.33AMS 4037 and AMS-QQ-A-250/40.129-0.249

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