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Composite Material Properties: AS4 3501-6

RTD ±602s LPT 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 3501-65 rowsPage 3 of 3
material systemcondition basisE1 GPa (GPa)E2 GPa (GPa)E3 GPa (GPa)G12 GPa (GPa)G13 GPa (GPa)G23 GPa (GPa)S MPa (MPa)Vf pct (%)Xc MPa (MPa)basiscategorydensity kg m3 (kg/m3)fiberlaminatematrixmethodnu12 (dimensionless)nu13 (dimensionless)ply thickness mm (mm)source pagesource tabletest condition
AS4 3501-6RTD ±602s LPT mean12.247.223.6meanThick Section[±60] 2sLPT0.29563010.2.4.2(a)RTD
AS4 3501-6RTD ±602s Pagano mean12.247.211.423.63.534.86meanThick Section[±60] 2sPagano0.2950.3963010.2.4.2(a)RTD
AS4 3501-6RTD ±602s Roy mean12.247.21223.63.554.88meanThick Section[±60] 2sRoy0.2940.43463010.2.4.2(a)RTD
AS4 3501-6RTD ±602s Sun mean12.247.111.423.63.534.86meanThick Section[±60] 2sSun0.2950.3963010.2.4.2(a)RTD
AS4 3501-6RTW 75F W mean64.81175.15351.5772.213meanCarbon Composite1,545AS43501-60.2019186; 188; 204; 206Table 4.2.12(c); Table 4.2.12(e); Table 4.2.14(b); Table 4.2.14(d)RTW (75F/W)

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