Composite Material Properties: Hi-Nicalon_Mi_SiC

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: Hi-Nicalon_Mi_SiC2 rows
material systemcondition basisE1 GPa (GPa)E2 GPa (GPa)Vf pct (%)Xt MPa (MPa)basiscategorydensity kg m3 (kg/m3)fibermatrixply thickness mm (mm)source pagesource tabletest condition
Hi-Nicalon_Mi_SiCETD_1204C_A_mean14414437271meanCMC2,675Hi-NicalonSiC + Siliconized SiC0.3238; 239Vol5 Part D page 238; Vol5 Part D page 239ETD (1204C/A)
Hi-Nicalon_Mi_SiCRTD_23C_A_mean14519637271meanCMC2,675Hi-NicalonSiC + Siliconized SiC0.3238; 239; 240Vol5 Part D page 238; Vol5 Part D page 239; Vol5 Part D page 240RTD (23C/A)

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