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Composite Material Properties: T-500 12k 976

CTD -65F A mean to RTD 75F 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: T-500 12k 9763 rows
material systemcondition basisE2 GPa (GPa)Vf pct (%)Yt MPa (MPa)basiscategoryfibermatrixply thickness mm (mm)source pagesource tabletest condition
T-500 12k 976CTD -65F A mean10.34261.571.016meanCarbon CompositeT-500 12k9760.135976Table 4.2.1(b)CTD (-65F/A)
T-500 12k 976ETD 250F A mean8.27461.554.469meanCarbon CompositeT-500 12k9760.135976Table 4.2.1(b)ETD (250F/A)
T-500 12k 976RTD 75F A mean8.96361.570.327meanCarbon CompositeT-500 12k9760.135976Table 4.2.1(b)RTD (75F/A)

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