Aerospace Materials: RENE41 BAR
70 to 1700
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 |
|---|---|---|---|---|---|---|---|
| RENE41 BAR | 70 | 31.6 | 206 | 154 | 14 | AMS 5712; AMS 5713 | bar |
| RENE41 BAR | 1,000 | 27.3 | 203 | 147 | 14 | AMS 5712; AMS 5713 | bar |
| RENE41 BAR | 1,100 | — | 200 | 146 | 14 | AMS 5712; AMS 5713 | bar |
| RENE41 BAR | 1,200 | 26 | 194 | 145 | 14 | AMS 5712; AMS 5713 | bar |
| RENE41 BAR | 1,400 | 24.8 | 160 | 136 | 11 | AMS 5712; AMS 5713 | bar |
| RENE41 BAR | 1,500 | — | 126 | 118 | 14 | AMS 5712; AMS 5713 | bar |
| RENE41 BAR | 1,600 | 23.2 | 90 | 80 | 19 | AMS 5712; AMS 5713 | bar |
| RENE41 BAR | 1,700 | — | 58 | 50 | 26 | AMS 5712; AMS 5713 | bar |
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