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Aerospace Materials: CLAD 2024 SHEET T3

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 T38 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 T3 0.008-0.009 A7010.210.496119688236423759584439AT30.110Flat sheet and plate0.33AMS-QQ-A-250/50.008-0.009
CLAD 2024 SHEET T3 0.008-0.009 B7010.210.497121708437433760594540BT30.1Flat sheet and plate0.33AMS-QQ-A-250/50.008-0.009
CLAD 2024 SHEET T3 0.010-0.062 A7010.210.497121688236423760594439AT30.1Flat sheet and plate0.33AMS-QQ-A-250/50.010-0.062
CLAD 2024 SHEET T3 0.010-0.062 B7010.210.499123708437433861604540BT30.1Flat sheet and plate0.33AMS-QQ-A-250/50.010-0.062
CLAD 2024 SHEET T3 0.063-0.128 A7010.210.4101125708437433862614540AT30.115Flat sheet and plate0.33AMS-QQ-A-250/50.063-0.128
CLAD 2024 SHEET T3 0.063-0.128 B7010.210.4102127738839453963624742BT30.1Flat sheet and plate0.33AMS-QQ-A-250/50.063-0.128
CLAD 2024 SHEET T3 0.129-0.249 A7010.210.4102127708437433963624540AT30.115Flat sheet and plate0.33AMS-QQ-A-250/50.129-0.249
CLAD 2024 SHEET T3 0.129-0.249 B7010.210.4104129738839454064634742BT30.1Flat sheet and plate0.33AMS-QQ-A-250/50.129-0.249

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