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Aerospace Materials: 5083 SHEET O

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: 5083 SHEET O7 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
5083 SHEET O 0.051-1.500 A7010.210.460763238181825404018183.85AO0.09616Sheet and plate0.33AMS 4056 and AMS-QQ-A-250/60.051-1.500
5083 SHEET O 0.051-1.500 B7010.210.462783440191926414119193.85BO0.096Sheet and plate0.33AMS 4056 and AMS-QQ-A-250/60.051-1.500
5083 SHEET O 1.501-3.000 S7010.210.439173.85SO0.09616Sheet and plate0.33AMS 4056 and AMS-QQ-A-250/61.501-3.000
5083 SHEET O 3.001-4.000 S7010.210.438163.85SO0.09616Sheet and plate0.33AMS 4056 and AMS-QQ-A-250/63.001-4.000
5083 SHEET O 4.001-5.000 S7010.210.438163.85SO0.09614Sheet and plate0.33AMS 4056 and AMS-QQ-A-250/64.001-5.000
5083 SHEET O 5.001-7.000 S7010.210.437153.85SO0.09614Sheet and plate0.33AMS 4056 and AMS-QQ-A-250/65.001-7.000
5083 SHEET O 7.001-8.000 S7010.210.436143.85SO0.09612Sheet and plate0.33AMS 4056 and AMS-QQ-A-250/67.001-8.000

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