Composite Material Properties: IM7_977-3_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: IM7_977-3_TAPE1 row
material systemcondition basisE1 GPa (GPa)E2 GPa (GPa)G12 GPa (GPa)Vf pct (%)Xc MPa (MPa)Xt MPa (MPa)Yc MPa (MPa)Yt MPa (MPa)basisformnu12 (dimensionless)ply thickness mm (mm)test condition
IM7_977-3_TAPERTD_mean163.8194988.9356094.35059459.21,682.321442,289.06032168.23214463.983373meanUnidirectional Tape0.3240.12954RTD

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