Sample data from Engineering Database — 375 reference tables, deterministic calculators, and Engineering AI. Sign up free

Composite Material Properties: IM6 3501-6 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: IM6 3501-6 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
IM6 3501-6 TAPERTD mean168.921628.9631885.1710789.63188621,447.89962,551.0612193.0532851.7107mean1,550.0744Unidirectional Tape0.30.127RTD

What else is in Engineering Database

Related data