Composite Material Properties: S2_3501-6

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: S2_3501-63 rows
material systemcondition basisE1 GPa (GPa)E2 GPa (GPa)E3 GPa (GPa)G12 GPa (GPa)G13 GPa (GPa)G23 GPa (GPa)basiscategorylaminatemethodnu12 (dimensionless)nu13 (dimensionless)nu23 (dimensionless)source pagesource tabletest condition
S2_3501-6RTD_0_902s_LPT_mean38.126.46.76meanThick Section[0 /90] 2 sLPT0.16663210.2.4.2(b)RTD
S2_3501-6RTD_0_902s_Pagano_mean38.126.416.46.7665.39meanThick Section[0 /90] 2 sPagano0.1660.4050.45963210.2.4.2(b)RTD
S2_3501-6RTD_0_902s_Roy_mean38.126.415.96.766.335.2meanThick Section[0 /90] 2 sRoy0.1650.3590.42763210.2.4.2(b)RTD

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