Composite Material Properties: AS4_PEEK_APC2_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: AS4_PEEK_APC2_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
AS4_PEEK_APC2_TAPERTD_mean131.000449.9974024.48159499.97402581,103.16162,109.79656186.1585259.984412mean1,577.7543Thermoplastic Tape0.270.1397RTD

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