Composite Material Properties: AS4_5250-3

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_5250-33 rows
material systemcondition basisE1 GPa (GPa)E2 GPa (GPa)G12 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_5250-3CTD_-67F_A_mean106.8699.6535.79269.637611,365.1621,861.58434.336meanCarbon Composite1,595AS45250-30.2950.1435353; 356; 357; 360Table 4.4.4(a); Table 4.4.4(d); Table 4.4.4(e); Table 4.4.4(h)CTD (-67F/A)
AS4_5250-3ETD_350F_A_mean119.9697.1714.55171.705611,199.6881,834.00531.923meanCarbon Composite1,595AS45250-30.3020.1435353; 356; 357; 360Table 4.4.4(a); Table 4.4.4(d); Table 4.4.4(e); Table 4.4.4(h)ETD (350F/A)
AS4_5250-3ETD_450F_A_mean125.4857.4464.27562.122611,054.8981,744.37431.302meanCarbon Composite1,595AS45250-30.2950.1435354; 356; 358; 360Table 4.4.4(b); Table 4.4.4(d); Table 4.4.4(f); Table 4.4.4(h)ETD (450F/A)

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