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Composite Material Properties: E GLASS EPOXY TAPE

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: E GLASS EPOXY TAPE1 row
material systemcondition basisE1 GPa (GPa)E2 GPa (GPa)G12 GPa (GPa)S MPa (MPa)Vf pct (%)Xc MPa (MPa)Xt MPa (MPa)Yc MPa (MPa)Yt MPa (MPa)basisdensity kg m3 (kg/m3)formnu12 (dimensionless)ply thickness mm (mm)test condition
E GLASS EPOXY TAPERTD mean38.6106568.2737124.13685659.98441255606.738881,061.79304137.895234.4738mean1,992.9528Unidirectional Tape0.260.254RTD

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