Aerospace Materials: HAYNES188 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 |
|---|---|---|---|---|---|---|---|
| HAYNES188 SHEET | 70 | 33.6 | 137.2 | 67.3 | 53 | AMS 5608; AMS 5772 | sheet 0.029–0.050" (solution HT) |
| HAYNES188 SHEET | 1,000 | 27.6 | 108.5 | 42 | 61 | AMS 5608; AMS 5772 | sheet 0.029–0.050" (solution HT) |
| HAYNES188 SHEET | 1,200 | — | 103.3 | 39.7 | 59 | AMS 5608; AMS 5772 | sheet 0.029–0.050" (solution HT) |
| HAYNES188 SHEET | 1,400 | 24.9 | 89.9 | 38.9 | 63 | AMS 5608; AMS 5772 | sheet 0.029–0.050" (solution HT) |
| HAYNES188 SHEET | 1,600 | — | 60 | 35.9 | 64 | AMS 5608; AMS 5772 | sheet 0.029–0.050" (solution HT) |
| HAYNES188 SHEET | 1,800 | 22.3 | 35.2 | 19 | 59 | AMS 5608; AMS 5772 | sheet 0.029–0.050" (solution HT) |
| HAYNES188 SHEET | 2,000 | — | 18.7 | 9.3 | 32 | AMS 5608; AMS 5772 | sheet 0.029–0.050" (solution HT) |
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