Aerospace Materials: INCONELX750 BAR
70 to 1500
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 |
|---|---|---|---|---|---|---|---|
| INCONELX750 BAR | 70 | 31 | 161 | 92 | 22 | AMS 5542; AMS 5667; AMS 5668; AMS 5669; AMS 5670; AMS 5671 | bar |
| INCONELX750 BAR | 1,000 | 25 | 140 | 83 | 20 | AMS 5542; AMS 5667; AMS 5668; AMS 5669; AMS 5670; AMS 5671 | bar |
| INCONELX750 BAR | 1,200 | — | 120 | 82 | 10 | AMS 5542; AMS 5667; AMS 5668; AMS 5669; AMS 5670; AMS 5671 | bar |
| INCONELX750 BAR | 1,400 | — | 80 | 68 | 10 | AMS 5542; AMS 5667; AMS 5668; AMS 5669; AMS 5670; AMS 5671 | bar |
| INCONELX750 BAR | 1,500 | 18.5 | 47 | 45 | 20 | AMS 5542; AMS 5667; AMS 5668; AMS 5669; AMS 5670; AMS 5671 | bar |
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