Composite Material Properties: Carbon_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: Carbon_SiC3 rows
material systemcondition basisE1 GPa (GPa)E2 GPa (GPa)S MPa (MPa)Vf pct (%)Xt MPa (MPa)Yt MPa (MPa)basiscategorydensity kg m3 (kg/m3)fibermatrixply thickness mm (mm)source pagesource tabletest condition
Carbon_SiCCTD_-157C_A_mean57.957.913345485485meanCMC1,100Carbon T300SiC0.1232; 233; 234Vol5 Part D page 232; Vol5 Part D page 233; Vol5 Part D page 234CTD (-157C/A)
Carbon_SiCETD_1200C_A_mean11411445546546meanCMC1,100Carbon T300SiC0.1232; 233Vol5 Part D page 232; Vol5 Part D page 233ETD (1200C/A)
Carbon_SiCETD_1400C_A_mean95.795.745523523meanCMC1,100Carbon T300SiC0.1232; 233; 235Vol5 Part D page 232; Vol5 Part D page 233; Vol5 Part D page 235ETD (1400C/A)

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