Aerospace Materials: HAYNES25 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 |
|---|---|---|---|---|---|---|---|
| HAYNES25 SHEET | 70 | 32.6 | 150 | 70 | 65 | AMS 5537; AMS 5759 | sheet/bar (solution HT) |
| HAYNES25 SHEET | 600 | 30.2 | 120.4 | 44.3 | 80 | AMS 5537; AMS 5759 | sheet (solution HT) |
| HAYNES25 SHEET | 1,000 | 27.3 | 106.2 | 39 | 72 | AMS 5537; AMS 5759 | sheet (solution HT) |
| HAYNES25 SHEET | 1,200 | 26.3 | 103 | 35.4 | 35 | AMS 5537; AMS 5759 | sheet (solution HT) |
| HAYNES25 SHEET | 1,400 | 25.2 | 84.5 | 35.1 | 28 | AMS 5537; AMS 5759 | sheet (solution HT) |
| HAYNES25 SHEET | 1,600 | 23.7 | 46.6 | 34.5 | 30 | AMS 5537; AMS 5759 | sheet (solution HT) |
| HAYNES25 SHEET | 1,800 | 22.4 | 33.5 | 18.2 | 40 | AMS 5537; AMS 5759 | sheet (solution HT) |
| HAYNES25 SHEET | 2,000 | 21.2 | 19.6 | 12 | 34 | AMS 5537; AMS 5759 | sheet (solution HT) |
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