Aerospace Materials: CH2 AISI 8740 BARS and FORGINGS QUENCHED and TEMPEREDB 1 750 S 2 3 1 0 C3 C2
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) | Ec Msi (Msi) | Ftu ksi (ksi) | G Msi (Msi) | basis | condition | density lb in3 (lb/in^3) | designation | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| CH2 AISI 8740 BARS AND FORGINGS QUENCHED AND TEMPEREDB 1 750 S 2 3 1 0 C3 C2 | 70 | 29 | 29 | 125 | 11 | S | Quenched and temperedb | 0.283 | AISI 8740 | Bars and forgings | 0.32 | AMS 6327 | 1.750 |
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