Aerospace Materials: HAYNES230 SHEET
70 to 2000
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) | Ftu ksi (ksi) | Fty ksi (ksi) | elongation pct (%) | specification | thickness range |
|---|---|---|---|---|---|---|---|
| HAYNES230 SHEET | 70 | 30.6 | 124.9 | 56.9 | 47.7 | AMS 5878 | sheet (2250°F solution annealed) |
| HAYNES230 SHEET | 1,000 | 26.4 | 103.1 | 39.7 | 55.7 | AMS 5878 | sheet (2250°F solution annealed) |
| HAYNES230 SHEET | 1,200 | 25.3 | 97.2 | 39 | 55 | AMS 5878 | sheet (2250°F solution annealed) |
| HAYNES230 SHEET | 1,400 | 24.1 | 84.9 | 41.2 | 46.1 | AMS 5878 | sheet (2250°F solution annealed) |
| HAYNES230 SHEET | 1,600 | 23.1 | 58.3 | 32.4 | 58.9 | AMS 5878 | sheet (2250°F solution annealed) |
| HAYNES230 SHEET | 1,800 | 21.9 | 32.5 | 17.3 | 70.5 | AMS 5878 | sheet (2250°F solution annealed) |
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