Aerospace Materials: INCONEL X750 BAR FORGING EQ AGED
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) | Ec Msi (Msi) | Fbru ksi (ksi) | Fbru ksi 2 (ksi) | Fbry ksi (ksi) | Fbry ksi 2 (ksi) | Fcy ksi (ksi) | Fsu ksi (ksi) | Ftu ksi (ksi) | Fty ksi (ksi) | G Msi (Msi) | RA pct (%) | basis | condition | density lb in3 (lb/in^3) | elongation pct (%) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| INCONEL X750 BAR FORGING EQ AGED 4.000-10.000 S | 70 | 30.6 | 30.6 | 240 | 304 | 150 | 180 | 100 | 99 | 160 | 100 | 11.8 | 17 | S | Equalized and aged | 0.298 | 15 | Bars and forgings | 0.3 | AMS 5667 | 4.000-10.000 |
| INCONEL X750 BAR FORGING EQ AGED LT4.000 S | 70 | 30.6 | 30.6 | 247 | 313 | 157 | 189 | 105 | 102 | 165 | 105 | 11.8 | 25 | S | Equalized and aged | 0.298 | 20 | Bars and forgings | 0.3 | AMS 5667 | <4.000 |
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