Aerospace Materials: MP35N BAR CW
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 | reduction area pct | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| MP35N BAR CW 1.001-1.750 S | 70 | 34 | — | 260 | 230 | 11.7 | S | Solution treated and cold drawn | 0.304 | 8 | Bar | 35 | AMS 5844 | 1.001-1.750 |
| MP35N BAR CW LE1.000 S | 70 | 34 | 145 | 260 | 230 | 11.7 | S | Solution treated and cold drawn | 0.304 | 8 | Bar | 35 | AMS 5844 | <=1.000 |
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