Composite Material Properties: T300_3k_EA_9396

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: T300_3k_EA_93963 rows
material systemcondition basisE2 GPa (GPa)G12 GPa (GPa)S MPa (MPa)Vf pct (%)Yc MPa (MPa)Yt MPa (MPa)basiscategorydensity kg m3 (kg/m3)fibermatrixnu12 (dimensionless)ply thickness mm (mm)source pagesource tabletest condition
T300_3k_EA_9396CTD_-65F_A_mean60.6055.716126.86455.45595.707645.349meanCarbon Composite1,490T300 3kEA 93960.05430.3937280; 283; 285Table 4.2.27(b); Table 4.2.27(e); Table 4.2.27(g)CTD (-65F/A)
T300_3k_EA_9396CTW_-65F_W_mean63.0185.681115.83255.45548.133689.476meanCarbon Composite1,490T300 3kEA 93960.05350.3937281; 284; 285Table 4.2.27(c); Table 4.2.27(f); Table 4.2.27(g)CTW (-65F/W)
T300_3k_EA_9396ETD_200F_A_mean56.9512.84853.91755.45290.269543.996meanCarbon Composite1,490T300 3kEA 93960.05750.3937280; 283; 285Table 4.2.27(b); Table 4.2.27(e); Table 4.2.27(g)ETD (200F/A)

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