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Aerospace Materials: CLAD 2024 SHEET T4

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 2024 SHEET T44 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)basisconditiondensity lb in3 (lb/in^3)elongation pct LT (%)formpoisson ratiospecificationthickness range
CLAD 2024 SHEET T4 0.010-0.062 A701010.296119637636363758583636AT40.1Coiled sheet0.33AMS-QQ-A-250/50.010-0.062
CLAD 2024 SHEET T4 0.010-0.062 B701010.297121668038383759593838BT40.1Coiled sheet0.33AMS-QQ-A-250/50.010-0.062
CLAD 2024 SHEET T4 0.063-0.128 A701010.2101125668038383861613838AT40.115Coiled sheet0.33AMS-QQ-A-250/50.063-0.128
CLAD 2024 SHEET T4 0.063-0.128 B701010.2102127688239393962623939BT40.1Coiled sheet0.33AMS-QQ-A-250/50.063-0.128

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