Aerospace Materials: WASPALOY SHEET STRIP PLATE SSPA
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 LT (ksi) | Fty ksi LT (ksi) | basis | condition | density lb in3 (lb/in^3) | elongation pct LT (%) | form | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|
| WASPALOY SHEET STRIP PLATE SSPA 0.020 S | 70 | 30.6 | 170 | 110 | S | Solution, stabilization, and precipitation heat treated | 0.298 | 15 | Sheet, strip, and plate | AMS 5544 | 0.020 |
| WASPALOY SHEET STRIP PLATE SSPA GT0.020 S | 70 | 30.6 | 175 | 115 | S | Solution, stabilization, and precipitation heat treated | 0.298 | 20 | Sheet, strip, and plate | AMS 5544 | >0.020 |
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