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Aerospace Materials: 7475 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: 7475 PLATE T6513 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 (%)elongation pct LT (%)formpoisson ratiospecificationthickness range
7475 PLATE T651 0.250-0.499 S7010.210.611314491106677044777869673.9ST6510.1011010Plate0.33AMS 40900.250-0.499
7475 PLATE T651 0.500-1.000 S7010.210.611314493107687143777870683.9ST6510.10199Plate0.33AMS 40900.500-1.000
7475 PLATE T651 1.001-1.500 S7010.210.611314493107677141777870683.9ST6510.10199Plate0.33AMS 40901.001-1.500

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