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Composite Material Properties: T-300 F650

CTD -67F 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-300 F6505 rows
material systemcondition basisE1 GPa (GPa)G12 GPa (GPa)S MPa (MPa)Vf pct (%)Xt MPa (MPa)basiscategorydensity kg m3 (kg/m3)fibermatrixply thickness mm (mm)source pagesource tabletest condition
T-300 F650CTD -67F A mean131.69611,337.583meanCarbon Composite1,570T-300F6500.1778338Table 4.4.1(a)CTD (-67F/A)
T-300 F650ETD 350F A mean38.54252meanCarbon Composite1,510T-300F6500.381344Table 4.4.2(b)ETD (350F/A)
T-300 F650ETD 400F A mean64.742611,578.899meanCarbon Composite1,570T-300F6500.1778338; 339Table 4.4.1(a); Table 4.4.1(b)ETD (400F/A)
T-300 F650ETD 450F A mean39.9952meanCarbon Composite1,510T-300F6500.381344Table 4.4.2(b)ETD (450F/A)
T-300 F650RTD 75F A mean130.3114.75740.196521,709.9meanCarbon Composite1,510T-300F6500.381338; 339; 343; 344Table 4.4.1(a); Table 4.4.1(b); Table 4.4.2(a); Table 4.4.2(b)RTD (75F/A)

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