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Aerospace Materials: CLAD 7075 PLATE T651

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: CLAD 7075 PLATE T6514 rowsPage 2 of 2
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)Fcy ksi ST (ksi)Fsu ksi (ksi)Ftu ksi (ksi)Ftu ksi LT (ksi)Ftu ksi ST (ksi)Fty ksi (ksi)Fty ksi LT (ksi)Fty ksi ST (ksi)basisconditionelongation pct LT (%)formpoisson ratiospecificationthickness range
CLAD 7075 PLATE T651 3.001-3.500 A701010.31041288610053596140686965585654AT6515Plate0.33AMS 4049 and AMS-QQ-A-250/133.001-3.500a
CLAD 7075 PLATE T651 3.001-3.500 B701010.31071328910455616342707167605855BT651Plate0.33AMS 4049 and AMS-QQ-A-250/133.001-3.500a
CLAD 7075 PLATE T651 3.501-4.000 A701010.398121809349555738646561545250AT6513Plate0.33AMS 4049 and AMS-QQ-A-250/133.501-4.000a
CLAD 7075 PLATE T651 3.501-4.000 B701010.3101124849751575939666763565452BT651Plate0.33AMS 4049 and AMS-QQ-A-250/133.501-4.000a

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