Composite Material Properties: T-300_934

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: T-300_9343 rows
material systemcondition basisE1 GPa (GPa)E2 GPa (GPa)S MPa (MPa)Vf pct (%)Xc MPa (MPa)Xt MPa (MPa)Yc MPa (MPa)Yt MPa (MPa)basiscategorydensity kg m3 (kg/m3)fibermatrixply thickness mm (mm)source pagesource tabletest condition
T-300_934CTD_-65F_A_mean56.53757.91682.04859717.055572.265710.16551.581meanCarbon Composite1,555T-3009340.1981115; 117; 119; 121; 123Table 4.2.6(a); Table 4.2.6(c); Table 4.2.6(e); Table 4.2.6(g); Table 4.2.6(i)CTD (-65F/A)
T-300_934ETD_250F_A_mean57.91660.67463.43259689.476751.529565.37648.107meanCarbon Composite1,555T-3009340.1981115; 117; 119; 121; 123Table 4.2.6(a); Table 4.2.6(c); Table 4.2.6(e); Table 4.2.6(g); Table 4.2.6(i)ETD (250F/A)
T-300_934ETW_160F_W_mean67.56968.94859510.212661.897517.107668.791meanCarbon Composite1,555T-3009340.1981116; 118; 120; 122Table 4.2.6(b); Table 4.2.6(d); Table 4.2.6(f); Table 4.2.6(h)ETW (160F/W)

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