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Aerospace Materials: CLAD 7475 SHEET T761

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 7475 SHEET T7615 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 LT (%)formpoisson ratiospecificationthickness range
CLAD 7475 SHEET T761 0.040-0.062 S709.7101041338397555841666656553.8ST7610.1019Sheet0.33AMS 41000.040-0.062
CLAD 7475 SHEET T761 0.063-0.187 A709.71010713686101565940676858573.8AT7610.1019Sheet0.33AMS 41000.063-0.187
CLAD 7475 SHEET T761 0.063-0.187 B709.71011014090106596241707061603.8BT7610.101Sheet0.33AMS 41000.063-0.187
CLAD 7475 SHEET T761 0.188-0.249 A709.71010813890106586140687059603.8AT7610.1019Sheet0.33AMS 41000.188-0.249
CLAD 7475 SHEET T761 0.188-0.249 B709.71011114293110606341717263623.8BT7610.101Sheet0.33AMS 41000.188-0.249

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