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Aerospace Materials: 7075 FORGING T73

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 FORGING T735 rows
material idtemp fE Msi (Msi)Ec Msi (Msi)Fcy ksi (ksi)Fcy ksi LT (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 (%)elongation pct LT (%)elongation pct ST (%)formpoisson ratiospecificationthickness range
7075 FORGING T73 2.001-3.000 S7010.210.45652396664615654523.8ST73a0.101743Hand forging0.33AMS-A-22771 and AMS-QQ-A-3672.001-3.000
7075 FORGING T73 3.001-4.000 S7010.210.46463605553513.8ST73a0.101732Hand forging0.33AMS-A-22771 and AMS-QQ-A-3673.001-4.000
7075 FORGING T73 4.001-5.000 S7010.210.46261585351503.8ST73a0.101732Hand forging0.33AMS-A-22771 and AMS-QQ-A-3674.001-5.000
7075 FORGING T73 5.001-6.000 S7010.210.46159575150493.8ST73a0.101632Hand forging0.33AMS-A-22771 and AMS-QQ-A-3675.001-6.000
7075 FORGING T73 LE2.000 S7010.210.4565239666456543.8ST73a0.10174Hand forging0.33AMS-A-22771 and AMS-QQ-A-367<=2.000

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