Composite Material Properties: T-500_976

Fiber-reinforced composite lamina (ply-level) mechanical properties from CMH-17 Rev G, MIL-HDBK-17, and authoritative datasheets. Covers carbon/epoxy, glass/epoxy, aramid/epoxy, PEEK thermoplastic, metal matrix composites (MMC), and ceramic matrix composites (CMC). Properties include elastic constants (E1, E2, G12, nu12), strengths (Xt, Xc, Yt, Yc, S), and physical properties across multiple test conditions (RTD, CTD, ETD, ETW) with mean and B-basis values.

Aerospace Engineeringmaterial_system: T-500_9763 rows
material systemcondition basisE1 GPa (GPa)Vf pct (%)Xt MPa (MPa)basiscategorydensity kg m3 (kg/m3)fibermatrixply thickness mm (mm)source pagesource tabletest condition
T-500_976CTD_-65F_A_mean13161.51,468.583meanCarbon Composite1,590T-5009760.135975Table 4.2.1(a)CTD (-65F/A)
T-500_976ETD_250F_A_mean153.06461.51,882.269meanCarbon Composite1,590T-5009760.135975Table 4.2.1(a)ETD (250F/A)
T-500_976RTD_75F_A_mean150.99561.52,033.953meanCarbon Composite1,590T-5009760.135975Table 4.2.1(a)RTD (75F/A)

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