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Aerospace Materials: 2014 BAR T6 and T651

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: 2014 BAR T6 and T6517 rows
material idtemp fE Msi (Msi)Ec Msi (Msi)Fbru ksi (ksi)Fbru ksi 2 (ksi)Fbry ksi (ksi)Fbry ksi 2 (ksi)Fcy ksi (ksi)Fsu ksi (ksi)Ftu ksi (ksi)Ftu ksi LT (ksi)Fty ksi (ksi)Fty ksi LT (ksi)G Msi (Msi)basisconditiondensity lb in3 (lb/in^3)elongation pct (%)formpoisson ratiospecificationthickness range
2014 BAR T6 AND T651 1.001-2.000 S7010.510.75338656355524ST6 and T6510.1018Bar, rod, and shapes, rolled, drawn, or cold-finished0.33AMS 4121 and AMS-QQ-A-225/41.001-2.000
2014 BAR T6 AND T651 2.001-3.000 S7010.510.75338656255514ST6 and T6510.1018Bar, rod, and shapes, rolled, drawn, or cold-finished0.33AMS 4121 and AMS-QQ-A-225/42.001-3.000
2014 BAR T6 AND T651 3.001-4.000 S7010.510.75338656155504ST6 and T6510.1018Bar, rod, and shapes, rolled, drawn, or cold-finished0.33AMS 4121 and AMS-QQ-A-225/43.001-4.000
2014 BAR T6 AND T651 4.001-5.000 S7010.510.75338656055494ST6 and T6510.1018Bar, rod, and shapes, rolled, drawn, or cold-finished0.33AMS 4121 and AMS-QQ-A-225/44.001-5.000b
2014 BAR T6 AND T651 5.001-6.000 S7010.510.75338655955484ST6 and T6510.1018Bar, rod, and shapes, rolled, drawn, or cold-finished0.33AMS 4121 and AMS-QQ-A-225/45.001-6.000b
2014 BAR T6 AND T651 6.001-8.000 S7010.510.7533865554ST6 and T6510.1018Bar, rod, and shapes, rolled, drawn, or cold-finished0.33AMS 4121 and AMS-QQ-A-225/46.001-8.000b
2014 BAR T6 AND T651 UP-1.000 S7010.510.79812477885338656455534ST6 and T6510.1018Bar, rod, and shapes, rolled, drawn, or cold-finished0.33AMS 4121 and AMS-QQ-A-225/4Up to 1.000

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