Aerospace Materials: INCONEL718 BAR
70 to 1400
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 |
|---|---|---|---|---|---|---|---|
| INCONEL718 BAR | 70 | 29.6 | 204 | 170 | 21 | AMS 5662; AMS 5663; AMS 5664 | bar/sheet/plate |
| INCONEL718 BAR | 400 | 28.8 | 198 | 163 | 20 | AMS 5662; AMS 5663; AMS 5664 | bar/sheet/plate |
| INCONEL718 BAR | 600 | 27.6 | 195 | 159 | 20 | AMS 5662; AMS 5663; AMS 5664 | bar/sheet/plate |
| INCONEL718 BAR | 800 | 26.5 | 191 | 156 | 19 | AMS 5662; AMS 5663; AMS 5664 | bar/sheet/plate |
| INCONEL718 BAR | 1,000 | 25.5 | 185 | 155 | 18 | AMS 5662; AMS 5663; AMS 5664 | bar/sheet/plate |
| INCONEL718 BAR | 1,200 | 24.5 | 168 | 149 | 19 | AMS 5662; AMS 5663; AMS 5664 | bar/sheet/plate |
| INCONEL718 BAR | 1,400 | 23.1 | 110 | 110 | 27 | AMS 5662; AMS 5663; AMS 5664 | bar/sheet/plate |
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