Aerospace Materials: INCONEL 718 TUBE STA O.D. GT0.125 WALL
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 718 TUBE STA O.D. GT0.125 WALL GT0.0 S T6 3 5 0b C6 | 70 | 29.4 | 30.9 | 185 | 150 | 11.4 | S | Solution treated and aged per indicated specification | 0.297 | 12 | Tubing | 0.29 | AMS 5589 | O.D. > 0.125 | Wall > 0.015 |
| INCONEL 718 TUBE STA O.D. GT0.125 WALL GT0.0 S T6 3 5 0b C7 | 70 | 29.4 | 30.9 | 170 | 145 | 11.4 | S | Solution treated and aged per indicated specification | 0.297 | 15 | Tubing | 0.29 | AMS 5590 | O.D. > 0.125 | Wall > 0.015 |
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