Aerospace Materials: RENE 41 BAR FORGING STA
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) | Fcy ksi (ksi) | Fsu ksi (ksi) | Ftu ksi (ksi) | Fty ksi (ksi) | G Msi (Msi) | RA pct (%) | basis | condition | density lb in3 (lb/in^3) | elongation pct (%) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| RENE 41 BAR FORGING STA LE1.000 S | 70 | 31.6 | 31.6 | 133 | 110 | 170 | 130 | 12.1 | 10 | S | Solution treated and aged (1400(F) | 0.298 | 8 | Bar and forging | 0.31 | AMS 5712 and AMS 5713 | <=1.000 |
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