Aerospace Materials: CH2 AISI 301AND RELATEDA B C STAINLESS STEELS SHEET and STRIP HARD NA A 2 7 1 0 B C4
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) | Fbry ksi (ksi) | Fbry ksi 2 (ksi) | Fcy ksi (ksi) | Fcy ksi LT (ksi) | Ftu ksi (ksi) | Ftu ksi LT (ksi) | Fty ksi LT (ksi) | G Msi (Msi) | basis | condition | density lb in3 (lb/in^3) | elongation pct LT (%) | form | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| CH2 AISI 301AND RELATEDA B C STAINLESS STEELS SHEET AND STRIP HARD NA A 2 7 1 0 B C4 | 70 | 29 | 28 | 189 | 152 | 137 | 92 | 152 | 30 | 124 | 69 | 11.2 | A | ½ Hard | 0.286 | 185 | Sheet and strip | AMS 5518 | ... |
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