Composite Material Properties: T650-35_3k_976_plain_weave

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: T650-35_3k_976_plain_weave3 rows
material systemcondition basisE1 GPa (GPa)Xt MPa (MPa)basiscategorydensity kg m3 (kg/m3)fiberply thickness mm (mm)source pagesource tabletest condition
T650-35_3k_976_plain_weaveCTD_-67F_A_mean72.395519.865meanCarbon Composite1,570T650-35 3k 976 plain weave0.1791329; 330; 331; 332; 333Table 4.2.35(a); Table 4.2.35(b); Table 4.2.35(c); Table 4.2.35(d); Table 4.2.35(e)CTD (-67F/A)
T650-35_3k_976_plain_weaveETW_250F_W_B-basis612.944BCarbon Composite1,570T650-35 3k 976 plain weave0.1791329Table 4.2.35(a)ETW (250F/W)
T650-35_3k_976_plain_weaveETW_250F_W_mean73.774730.844meanCarbon Composite1,570T650-35 3k 976 plain weave0.1791329; 330; 331; 332; 333Table 4.2.35(a); Table 4.2.35(b); Table 4.2.35(c); Table 4.2.35(d); Table 4.2.35(e)ETW (250F/W)

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