Aerospace Materials: INCONEL 600 BAR CW
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) | Ftu ksi (ksi) | Fty ksi (ksi) | G Msi (Msi) | basis | condition | density lb in3 (lb/in^3) | elongation pct (%) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| INCONEL 600 BAR CW 0.251-0.499 S | 70 | 30 | 30 | 95 | 70 | 11 | S | Cold-worked | 0.304 | 7 | Square, hexagon, and rectangle | 0.29 | ASTM B166 | 0.251-0.499 |
| INCONEL 600 BAR CW LE0.250 S | 70 | 30 | 30 | 100 | 80 | 11 | S | Cold-worked | 0.304 | 5 | Square, hexagon, and rectangle | 0.29 | ASTM B166 | <=0.250 |
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