Aerospace Materials: WASPALOY BAR FORGING 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 (ksi) | Fty ksi (ksi) | RA pct (%) | basis | condition | density lb in3 (lb/in^3) | elongation pct (%) | form | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|
| WASPALOY BAR FORGING SSPA 3.500 S T6 3 8 0b C3 | 70 | 30.6 | 175 | 120 | 18 | S | Solution, stabilization, and precipitation heat treated | 0.298 | 15 | Bar, forging, and Forging ring | AMS 5706 and AMS 5704 AMS 5707 | 3.500 |
| WASPALOY BAR FORGING SSPA 3.500 S T6 3 8 0b C4 | 70 | 30.6 | 160 | 110 | 18 | S | Solution, stabilization, and precipitation heat treated | 0.298 | 15 | Bar, forging, and Forging ring | AMS 5706 and AMS 5704 AMS 5707 | 3.500 |
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