Aerospace Materials: CH2 LOW ALLOY STEELS ALL WROUGHT FORMS QUENCHED and TEMPEREDA NA D 2 3 1 0 G2 C1
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) | Fbru ksi (ksi) | Fbru ksi 2 (ksi) | Fbry ksi (ksi) | Fbry ksi 2 (ksi) | G Msi (Msi) | basis | condition | density lb in3 (lb/in^3) | form | poisson ratio | specification |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| CH2 LOW ALLOY STEELS ALL WROUGHT FORMS QUENCHED AND TEMPEREDA NA D 2 3 1 0 G2 C1 | 70 | 29 | 29 | 220 | 294 | 146 | 273 | 11 | d | Quenched and tempereda | 0.283 | All wrought forms | 0.32 | AMS 6427; see Tables 2.3.1.0(a) and (b) |
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