Aerospace Materials: INCONEL600 BAR
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 | Ftu ksi (ksi) | Fty ksi (ksi) | elongation pct (%) | specification | thickness range |
|---|---|---|---|---|---|---|
| INCONEL600 BAR | 600 | 90.5 | 31 | 46 | AMS 5540; AMS 5665 | bar/billet (annealed) |
| INCONEL600 BAR | 800 | 88.5 | 29.5 | 49 | AMS 5540; AMS 5665 | bar/billet (annealed) |
| INCONEL600 BAR | 1,000 | 84 | 28.5 | 47 | AMS 5540; AMS 5665 | bar/billet (annealed) |
| INCONEL600 BAR | 1,200 | 65 | 26.5 | 39 | AMS 5540; AMS 5665 | bar/billet (annealed) |
| INCONEL600 BAR | 1,400 | 27.5 | 17 | 46 | AMS 5540; AMS 5665 | bar/billet (annealed) |
| INCONEL600 BAR | 1,600 | 15 | 9 | 80 | AMS 5540; AMS 5665 | bar/billet (annealed) |
| INCONEL600 BAR | 1,800 | 7.5 | 4 | 118 | AMS 5540; AMS 5665 | bar/billet (annealed) |
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