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Aerospace Materials: 7075 EXTRUSION T6

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: 7075 EXTRUSION T65 rowsPage 2 of 2
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)Fcy ksi LT (ksi)Fcy ksi ST (ksi)Fsu ksi (ksi)Ftu ksi (ksi)Ftu ksi LT (ksi)Ftu ksi ST (ksi)Fty ksi (ksi)Fty ksi LT (ksi)Fty ksi ST (ksi)G Msi (Msi)basisconditiondensity lb in3 (lb/in^3)elongation pct (%)formpoisson ratiospecificationthickness range
7075 EXTRUSION T6 3.000-4.499 S7010.410.710213283100706161397864647055554ST6, T6510, T6511, and T62a0.1016Extrusion (rod, bar, and shapes)0.33AMS-QQ-A-200/113.000-4.499
7075 EXTRUSION T6 4.500-5.000 A7010.410.71011317995685757387863636852524AT6, T6510, T6511, and T62a0.1016Extrusion (rod, bar, and shapes)0.33AMS-QQ-A-200/114.500-5.000
7075 EXTRUSION T6 4.500-5.000 B7010.410.710513683100716060408165657155554BT6, T6510, T6511, and T62a0.101Extrusion (rod, bar, and shapes)0.33AMS-QQ-A-200/114.500-5.000
7075 EXTRUSION T6 LE0.249 A7010.410.711114092108707241787570664AT6, T6510, T6511, and T62a0.1017Extrusion (rod, bar, and shapes)0.33AMS-QQ-A-200/11<=0.249
7075 EXTRUSION T6 LE0.249 B7010.410.711714897114747644827974704BT6, T6510, T6511, and T62a0.101Extrusion (rod, bar, and shapes)0.33AMS-QQ-A-200/11<=0.249

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