Aerospace Materials: WASPALOY BAR
70 to 1000
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 |
|---|---|---|---|---|---|---|---|
| WASPALOY BAR | 70 | — | 209 | 156 | 27 | AMS 5544; AMS 5586; AMS 5704 | bar |
| WASPALOY BAR | 1,000 | 26.7 | 197 | 142 | 22 | AMS 5544; AMS 5586; AMS 5704 | bar |
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