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Aerospace Materials: INCONELX750 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).

Materials Sciencematerial id: INCONELX750 BAR5 rows
material idtemp fE Msi (Msi)Ftu ksi (ksi)Fty ksi (ksi)elongation pct (%)specificationthickness range
INCONELX750 BAR70311619222AMS 5542; AMS 5667; AMS 5668; AMS 5669; AMS 5670; AMS 5671bar
INCONELX750 BAR1,000251408320AMS 5542; AMS 5667; AMS 5668; AMS 5669; AMS 5670; AMS 5671bar
INCONELX750 BAR1,2001208210AMS 5542; AMS 5667; AMS 5668; AMS 5669; AMS 5670; AMS 5671bar
INCONELX750 BAR1,400806810AMS 5542; AMS 5667; AMS 5668; AMS 5669; AMS 5670; AMS 5671bar
INCONELX750 BAR1,50018.5474520AMS 5542; AMS 5667; AMS 5668; AMS 5669; AMS 5670; AMS 5671bar

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