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Composite Material Properties: M55J 954-3

RTD 72F A A-basis to RTD 72F A 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: M55J 954-33 rows
material systemcondition basisE1 GPa (GPa)S MPa (MPa)Vf pct (%)Xc MPa (MPa)Xt MPa (MPa)basiscategorydensity kg m3 (kg/m3)fibermatrixply thickness mm (mm)source pagesource tabletest condition
M55J 954-3RTD 72F A A-basis60.5661.8971,723.689ACarbon Composite1,650M55J954-30.0597388; 389Table 4.10.1(a); Table 4.10.1(b)RTD (72F/A)
M55J 954-3RTD 72F A B-basis60.5751.5291,971.901BCarbon Composite1,650M55J954-30.0597388; 389Table 4.10.1(a); Table 4.10.1(b)RTD (72F/A)
M55J 954-3RTD 72F A mean308.88576.53262937.6872,233.901meanCarbon Composite1,650M55J954-30.0597388; 389; 390Table 4.10.1(a); Table 4.10.1(b); Table 4.10.1(c)RTD (72F/A)

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