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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).

Materials Sciencematerial id: INCONEL 718 TUBE STA O.D. GT0.125 WALL2 rows
material idtemp fE Msi (Msi)Ec Msi (Msi)Ftu ksi (ksi)Fty ksi (ksi)G Msi (Msi)basisconditiondensity lb in3 (lb/in^3)elongation pct (%)formpoisson ratiospecificationthickness range
INCONEL 718 TUBE STA O.D. GT0.125 WALL GT0.0 S T6 3 5 0b C67029.430.918515011.4SSolution treated and aged per indicated specification0.29712Tubing0.29AMS 5589O.D. > 0.125 | Wall > 0.015
INCONEL 718 TUBE STA O.D. GT0.125 WALL GT0.0 S T6 3 5 0b C77029.430.917014511.4SSolution treated and aged per indicated specification0.29715Tubing0.29AMS 5590O.D. > 0.125 | Wall > 0.015

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