Composite Material Properties: AS4_12k_997

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_12k_9973 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
AS4_12k_997CTD_-65F_A_B-basis58.51,316.8991,813.32146.81574.463BCarbon Composite1,585AS4 12k9970.146289; 290; 291; 292Table 4.2.28(a); Table 4.2.28(b); Table 4.2.28(c); Table 4.2.28(d)CTD (-65F/A)
AS4_12k_997CTD_-65F_A_mean124.79510.687159.26958.51,606.4782,109.796268.89687.563meanCarbon Composite1,590AS4 12k9970.141289; 290; 291; 292; 293; 294Table 4.2.28(a); Table 4.2.28(b); Table 4.2.28(c); Table 4.2.28(d); Table 4.2.28(e); Table 4.2.28(f)CTD (-65F/A)
AS4_12k_997ETW_180F_W_B-basis58.5930.7922,054.638161.33728.613BCarbon Composite1,585AS4 12k9970.146289; 290; 291; 292Table 4.2.28(a); Table 4.2.28(b); Table 4.2.28(c); Table 4.2.28(d)ETW (180F/W)

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