Composite Material Properties: AS4_938

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: AS4_9383 rows
material systemcondition basisE1 GPa (GPa)E2 GPa (GPa)S MPa (MPa)Vf pct (%)Xc MPa (MPa)Xt MPa (MPa)Yt MPa (MPa)basiscategorydensity kg m3 (kg/m3)fibermatrixply thickness mm (mm)source pagesource tabletest condition
AS4_938CTD_-65F_A_mean134.44854.52,040.848meanCarbon Composite1,560AS49380.1194107Table 4.2.5(a)CTD (-65F/A)
AS4_938ETD_200F_A_mean140.6538.48195.83755.52,213.21760.95meanCarbon Composite1,570AS49380.1448107; 108; 111Table 4.2.5(a); Table 4.2.5(b); Table 4.2.5(e)ETD (200F/A)
AS4_938ETW_200F_W_mean131.69571,310.004meanCarbon Composite1,565AS49380.1372109Table 4.2.5(c)ETW (200F/W)

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