Composite Material Properties: T700S_3900-2

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: T700S_3900-23 rows
material systemcondition basisS MPa (MPa)Vf pct (%)basiscategorydensity kg m3 (kg/m3)fibermatrixply thickness mm (mm)source pagesource tabletest condition
T700S_3900-2CTD_-67F_A_mean85.49555meanCarbon Composite1,540T700S3900-20.1867317Table 4.2.33(a)CTD (-67F/A)
T700S_3900-2ETW_180F_W_mean52.88355meanCarbon Composite1,540T700S3900-20.1867317Table 4.2.33(a)ETW (180F/W)
T700S_3900-2RTD_75F_A_mean71.01655meanCarbon Composite1,540T700S3900-20.1867317Table 4.2.33(a)RTD (75F/A)

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