Composite Material Properties: AS4_3501-6S

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: AS4_3501-6S2 rows
material systemcondition basisE1 GPa (GPa)S MPa (MPa)Vf pct (%)Xc MPa (MPa)Xt MPa (MPa)basiscategorydensity kg m3 (kg/m3)fibermatrixply thickness mm (mm)source pagesource tabletest condition
AS4_3501-6SETD_200F_A_mean65.70758.5758.423meanCarbon Composite1,585AS43501-6S0.2705213; 214Table 4.2.15(b); Table 4.2.15(c)ETD (200F/A)
AS4_3501-6SRTD_75F_A_mean67.08675.84258.5854.95772.213meanCarbon Composite1,585AS43501-6S0.2705212; 213; 214Table 4.2.15(a); Table 4.2.15(b); Table 4.2.15(c)RTD (75F/A)

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