Aerospace Materials: INCONEL 718 BAR
-320 to 1200
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) | Fbru ksi (ksi) | Fcy ksi (ksi) | Fsu ksi (ksi) | Ftu ksi (ksi) | Fty ksi (ksi) | elongation pct (%) | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|
| INCONEL 718 BAR | 70 | 29 | 270 | 155 | 108 | 180 | 150 | 12 | AMS 5664 | up to 4.0 in dia |
| INCONEL 718 BAR | 400 | 28 | 260 | 149 | 104 | 173 | 144 | 12 | AMS 5664 | up to 4.0 in dia |
| INCONEL 718 BAR | 600 | 27.5 | 252 | 143 | 101 | 168 | 138 | 12 | AMS 5664 | up to 4.0 in dia |
| INCONEL 718 BAR | 800 | 27 | 244 | 137 | 98 | 163 | 132 | 12 | AMS 5664 | up to 4.0 in dia |
| INCONEL 718 BAR | 1,000 | 26 | 232 | 129 | 93 | 155 | 124 | 12 | AMS 5664 | up to 4.0 in dia |
| INCONEL 718 BAR | 1,200 | 25 | 195 | 110 | 78 | 130 | 105 | 12 | AMS 5664 | up to 4.0 in dia |
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