Composite Material Properties: Celion_12k_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: Celion_12k_9383 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)fibermatrixnu12 (dimensionless)ply thickness mm (mm)source pagesource tabletest condition
Celion_12k_938CTD_-67F_A_mean129.6219.308110.31661.51,654.7421,806.42665.5mean1,590Celion 12k9380.2790.1372127; 129; 130; 132Table 4.2.7(a); Table 4.2.7(c); Table 4.2.7(d); Table 4.2.7(f)CTD (-67F/A)
Celion_12k_938ETD_250F_A_mean124.7958.41296.52761.51,344.4782,130.4860.674mean1,590Celion 12k9380.280.1372127; 129; 130; 132Table 4.2.7(a); Table 4.2.7(c); Table 4.2.7(d); Table 4.2.7(f)ETD (250F/A)
Celion_12k_938ETW_180F_W_mean125.4858.20596.52761.51,275.531,909.84839.99mean1,590Celion 12k9380.3450.1372128; 129; 131; 132Table 4.2.7(b); Table 4.2.7(c); Table 4.2.7(e); Table 4.2.7(f)ETW (180F/W)

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