Aerospace Materials: HASTELLOY X SHEET PLATE ST 0.188-GT2.000
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) | Fty ksi LT (ksi) | G Msi (Msi) | basis | condition | density lb in3 (lb/in^3) | elongation pct LT (%) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| HASTELLOY X SHEET PLATE ST 0.188-GT2.000 2.000 S T6 3 1 0b C6 | 70 | 29.8 | 29.8 | 100 | 40 | 11.3 | S | Solution treated (annealed) | 0.297 | 35 | Sheeta and plate | 0.32 | AMS 5536 | 0.188->2.000 2.000 |
| HASTELLOY X SHEET PLATE ST 0.188-GT2.000 2.000 S T6 3 1 0b C7 | 70 | 29.8 | 29.8 | 95 | 40 | 11.3 | S | Solution treated (annealed) | 0.297 | 35 | Sheeta and plate | 0.32 | AMS 5536 | 0.188->2.000 2.000 |
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