Aerospace Materials: INCONEL625 SHEET
70 to 1800
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 |
|---|---|---|---|---|---|---|---|
| INCONEL625 SHEET | 70 | 30.2 | 138.8 | 72 | 38 | AMS 5599; AMS 5869 | sheet/plate (annealed) |
| INCONEL625 SHEET | 400 | 28.8 | 129.4 | 62.2 | 44 | AMS 5599; AMS 5869 | sheet/plate (annealed) |
| INCONEL625 SHEET | 600 | 27.7 | 125.6 | 59.5 | 45 | AMS 5599; AMS 5869 | sheet/plate (annealed) |
| INCONEL625 SHEET | 800 | 26.7 | 122.2 | 59.2 | 45 | AMS 5599; AMS 5869 | sheet/plate (annealed) |
| INCONEL625 SHEET | 1,000 | 25.6 | 119.9 | 58.8 | 46 | AMS 5599; AMS 5869 | sheet/plate (annealed) |
| INCONEL625 SHEET | 1,200 | 24.3 | 119.6 | 57 | 47 | AMS 5599; AMS 5869 | sheet/plate (annealed) |
| INCONEL625 SHEET | 1,400 | 22.8 | 88.4 | 55.3 | 70 | AMS 5599; AMS 5869 | sheet/plate (annealed) |
| INCONEL625 SHEET | 1,600 | 21.2 | 52.1 | 34.9 | 69 | AMS 5599; AMS 5869 | sheet/plate (annealed) |
| INCONEL625 SHEET | 1,800 | 18.7 | 25 | 10.8 | 108 | AMS 5599; AMS 5869 | sheet/plate (annealed) |
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