Aerospace Materials: MP159 BAR CW-AGED
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).
| material id | temp f | E Msi (Msi) | Fsu ksi (ksi) | Ftu ksi (ksi) | Fty ksi (ksi) | G Msi (Msi) | basis | condition | density lb in3 (lb/in^3) | elongation pct (%) | form | poisson ratio | reduction area pct | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| MP159 BAR CW-AGED 0.501-0.800 A | 70 | 35.3 | — | 260 | 250 | 11.3 | A | Solution treated, cold drawn, and aged | 0.302 | 6 | Bar | 0.37 | 32 | AMS 5843 | 0.501-0.800 |
| MP159 BAR CW-AGED 0.501-0.800 B | 70 | 35.3 | — | 269 | 262 | 11.3 | B | Solution treated, cold drawn, and aged | 0.302 | — | Bar | 0.37 | — | AMS 5843 | 0.501-0.800 |
| MP159 BAR CW-AGED 0.501-1.750 S | 70 | 35.3 | — | 260 | 250 | 11.3 | S | Solution treated, cold drawn, and aged | 0.302 | 6 | Bar | 0.37 | 32 | AMS 5842 | 0.501-1.750 |
| MP159 BAR CW-AGED 0.801-1.750 S | 70 | 35.3 | — | 260 | 250 | 11.3 | S | Solution treated, cold drawn, and aged | 0.302 | 6 | Bar | 0.37 | 32 | AMS 5843 | 0.801-1.750 |
| MP159 BAR CW-AGED LE0.500 A | 70 | 35.3 | 131 | 260 | 250 | 11.3 | A | Solution treated, cold drawn, and aged | 0.302 | 6 | Bar | 0.37 | 32 | AMS 5843 | <=0.500 |
| MP159 BAR CW-AGED LE0.500 B | 70 | 35.3 | 144 | 269 | 262 | 11.3 | B | Solution treated, cold drawn, and aged | 0.302 | — | Bar | 0.37 | — | AMS 5843 | <=0.500 |
| MP159 BAR CW-AGED LE0.500 S | 70 | 35.3 | 131 | 260 | 250 | 11.3 | S | Solution treated, cold drawn, and aged | 0.302 | 6 | Bar | 0.37 | 32 | AMS 5842 | <=0.500 |
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