Composite Material Properties: S2-449_SP_381

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: S2-449_SP_3813 rows
material systemcondition basisE1 GPa (GPa)E2 GPa (GPa)S MPa (MPa)Vf pct (%)Xc MPa (MPa)Xt MPa (MPa)Yt MPa (MPa)basisdensity kg m3 (kg/m3)fibermatrixply thickness mm (mm)source pagesource tabletest condition
S2-449_SP_381CTD_-65F_A_mean47.64314.548102.73251.751,144.531,840.968.948mean1,895S2-449SP 3810.0813397; 399; 400; 402; 403; 411; 413; 414; 416; 417Table 6.2.1(a); Table 6.2.1(c); Table 6.2.1(d); Table 6.2.1(f); Table 6.2.1(g); Table 6.2.2(a); Table 6.2.2(c); Table 6.2.2(d); Table 6.2.2(f); Table 6.2.2(g)CTD (-65F/A)
S2-449_SP_381ETD_180F_A_mean48.0569.79165.551.751,137.6351,551.3244.126mean1,895S2-449SP 3810.0813397; 399; 400; 402; 403; 411; 413; 414; 416; 417Table 6.2.1(a); Table 6.2.1(c); Table 6.2.1(d); Table 6.2.1(f); Table 6.2.1(g); Table 6.2.2(a); Table 6.2.2(c); Table 6.2.2(d); Table 6.2.2(f); Table 6.2.2(g)ETD (180F/A)
S2-449_SP_381ETW_160F_W_mean47.9887.58452.451.75930.792799.79224.821mean1,895S2-449SP 3810.0813398; 399; 401; 402; 403; 412; 413; 415; 416; 417Table 6.2.1(b); Table 6.2.1(c); Table 6.2.1(e); Table 6.2.1(f); Table 6.2.1(g); Table 6.2.2(b); Table 6.2.2(c); Table 6.2.2(e); Table 6.2.2(f); Table 6.2.2(g)ETW (160F/W)

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