Aerospace Material Allowables
Aerospace material mechanical 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).
Attributes
Ftu_ksiksi
Fty_ksiksi
Fcy_ksiksi
Fsu_ksiksi
Fbru_ksiksi
E_MsiMsi
elongation_pct%
thickness_range
specification
Browse data
15-5PH_BAR1 row2024-T3_SHEET3 rows2024-T4_BAR1 row2024-T4_SHEET2 rows2219-T87_PLATE1 row2219-T87_SHEET2 rows300M_STEEL_BAR1 row4130_STEEL_SHEET1 row4340_STEEL_BAR1 row6061-T6_EXTRUSION1 row6061-T6_SHEET1 row7050-T7451_PLATE1 row7075-T651_PLATE1 row7075-T6_PLATE3 rows7075-T6_SHEET1 row7075-T73_FORGING1 row7075-T73_PLATE1 rowA286_BAR3 rowsCUSTOM455_BAR3 rowsINCOLOY901_BAR3 rowsINCONEL600_BAR3 rowsINCONELX750_BAR3 rowsINCONEL_718_BAR3 rowsINCONEL_718_SHEET1 rowRENE41_BAR3 rows
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