Aerospace Materials: INCONEL X750 STRIP ANN 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) | Ftu ksi LT (ksi) | G Msi (Msi) | basis | condition | density lb in3 (lb/in^3) | elongation pct LT (%) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| INCONEL X750 STRIP ANN AGED 0.009 S | 70 | 30.6 | 30.6 | 150 | 11.8 | S | Annealed and aged | 0.298 | — | Strip | 0.3 | AMS 5542 | 0.009 |
| INCONEL X750 STRIP ANN AGED 0.010 S | 70 | 30.6 | 30.6 | 155 | 11.8 | S | Annealed and aged | 0.298 | 15 | Strip | 0.3 | AMS 5542 | 0.010 |
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