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Composite Material Properties: T300 5208 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: T300 5208 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
T300 5208 TAPERTD mean144.789968.9631884.48159462.0528460999.74021,503.05768165.4742441.36856mean1,550.0744Unidirectional Tape0.30.127RTD

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