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Aerospace Materials: 2297 PLATE T87

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: 2297 PLATE T875 rows
material idtemp fE Msi (Msi)Fbru ksi (ksi)Fbru ksi 2 (ksi)Fbry ksi (ksi)Fbry ksi 2 (ksi)Ftu ksi (ksi)Ftu ksi 45Ftu ksi LT (ksi)Ftu ksi ST (ksi)Fty ksi (ksi)Fty ksi LT (ksi)Fty ksi ST (ksi)basisconditiondensity lb in3 (lb/in^3)elongation pct (%)elongation pct LT (%)elongation pct ST (%)formspecificationthickness range
2297 PLATE T87 3.001-4.000 S7011.398128859962606259575754ST870.096541.5PlateAMS 43303.001-4.000
2297 PLATE T87 4.001-5.000 A7011.397126849861596158565652AT870.096541.5PlateAMS 43304.001-5.000
2297 PLATE T87 4.001-5.000 B7011.3102132859962636461585754BT870.096PlateAMS 43304.001-5.000
2297 PLATE T87 5.001-6.000 A7011.395123829660596057555552AT870.096541.5PlateAMS 43305.001-6.000
2297 PLATE T87 5.001-6.000 B7011.3102132859962636461585754BT870.096PlateAMS 43305.001-6.000

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