Aerospace Materials: INCOLOY901 BAR
70 to 1500
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 | Ftu ksi (ksi) | Fty ksi (ksi) | elongation pct (%) | specification | thickness range |
|---|---|---|---|---|---|---|
| INCOLOY901 BAR | 70 | 175 | 125 | 15 | AMS 5660; AMS 5661 | bar |
| INCOLOY901 BAR | 800 | 159 | 116.5 | 16 | AMS 5660; AMS 5661 | bar |
| INCOLOY901 BAR | 1,000 | 156 | 113 | 17 | AMS 5660; AMS 5661 | bar |
| INCOLOY901 BAR | 1,200 | 150 | 117 | 14 | AMS 5660; AMS 5661 | bar |
| INCOLOY901 BAR | 1,300 | 130 | 114 | 11.5 | AMS 5660; AMS 5661 | bar |
| INCOLOY901 BAR | 1,400 | 107.5 | 102.5 | 9 | AMS 5660; AMS 5661 | bar |
| INCOLOY901 BAR | 1,500 | 81 | 79 | 13 | AMS 5660; AMS 5661 | bar |
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