Aerospace Materials: HAYNES 230 BAR ANN2250
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 (ksi) | Fty ksi (ksi) | basis | condition | density lb in3 (lb/in^3) | elongation pct (%) | form | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|
| HAYNES 230 BAR ANN2250 LE1.000 A | 70 | 110 | 45 | A | 2250 Anneal | 0.324 | 35 | Bar | AMS 5891 | <=1.000 |
| HAYNES 230 BAR ANN2250 LE1.000 B | 70 | 118 | 51 | B | 2250 Anneal | 0.324 | 46 | Bar | AMS 5891 | <=1.000 |
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