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Composite Material Properties: AS4 E7K8

CTD -65F A mean to RTW 75F W mean

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 E7K85 rows
material systemcondition basisE1 GPa (GPa)E2 GPa (GPa)S MPa (MPa)Vf pct (%)Xc MPa (MPa)Xt MPa (MPa)Yt MPa (MPa)basiscategorydensity kg m3 (kg/m3)fibermatrixnu12 (dimensionless)ply thickness mm (mm)source pagesource tabletest condition
AS4 E7K8CTD -65F A mean121.348541,902.9532,006.374meanCarbon Composite1,550AS4E7K80.2880.137289; 92Table 4.2.3(a); Table 4.2.3(d)CTD (-65F/A)
AS4 E7K8ETD 180F A mean100.66356meanCarbon Composite1,545AS4E7K80.139794Table 4.2.3(f)ETD (180F/A)
AS4 E7K8ETW 180F W mean124.10692.39561,034.2142,137.375meanCarbon Composite1,545AS4E7K80.2880.139790; 93; 94Table 4.2.3(b); Table 4.2.3(e); Table 4.2.3(f)ETW (180F/W)
AS4 E7K8RTD 75F A mean62.1918.48166.74151.5765.3182,089.11137.714meanCarbon Composite1,530AS4E7K80.320.2019179; 180; 89; 91; 92; 94Table 4.2.11(a); Table 4.2.11(b); Table 4.2.3(a); Table 4.2.3(c); Table 4.2.3(d); Table 4.2.3(f)RTD (75F/A)
AS4 E7K8RTW 75F W mean127.553104.111561,482.3732,096.006meanCarbon Composite1,545AS4E7K80.139789; 92; 94Table 4.2.3(a); Table 4.2.3(d); Table 4.2.3(f)RTW (75F/W)

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