Aerospace Materials: HAYNES 230 PLATE ANN2200
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 | Ftu ksi LT (ksi) | Fty ksi LT (ksi) | basis | condition | density lb in3 (lb/in^3) | elongation pct LT (%) | form | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|
| HAYNES 230 PLATE ANN2200 LE0.400 A | 70 | 115 | 50 | A | 2200 Anneal | 0.324 | 40 | Plate | AMS 5878 | <=0.400 |
| HAYNES 230 PLATE ANN2200 LE0.400 B | 70 | 120 | 55 | B | 2200 Anneal | 0.324 | 43 | Plate | AMS 5878 | <=0.400 |
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