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Composite Material Properties: T300 15k 976

CTD -67F A mean 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: T300 15k 9764 rows
material systemcondition basisE1 GPa (GPa)E2 GPa (GPa)G12 GPa (GPa)S MPa (MPa)Vf pct (%)Xc MPa (MPa)Xt MPa (MPa)Yc MPa (MPa)Yt MPa (MPa)basiscategorydensity kg m3 (kg/m3)fibermatrixnu12 (dimensionless)ply thickness mm (mm)source pagesource tabletest condition
T300 15k 976CTD -67F A mean129.62112.6866.895114.453691,323.7931,372.057242.00632.612meanCarbon Composite1,630T300 15k9760.3180.1321226; 228; 229; 231; 232; 233Table 4.2.17(a); Table 4.2.17(c); Table 4.2.17(d); Table 4.2.17(f); Table 4.2.17(g); Table 4.2.17(h)CTD (-67F/A)
T300 15k 976ETD 260F A mean126.86412.6866.13664.535691,013.5291,627.163155.82226.269meanCarbon Composite1,630T300 15k9760.3120.1321226; 228; 229; 231; 232; 233Table 4.2.17(a); Table 4.2.17(c); Table 4.2.17(d); Table 4.2.17(f); Table 4.2.17(g); Table 4.2.17(h)ETD (260F/A)
T300 15k 976ETD 350F A mean135.82711.3075.30959.29569937.6871,599.584131.6923.925meanCarbon Composite1,630T300 15k9760.3480.1321227; 228; 230; 231; 232; 233Table 4.2.17(b); Table 4.2.17(c); Table 4.2.17(e); Table 4.2.17(f); Table 4.2.17(g); Table 4.2.17(h)ETD (350F/A)
T300 15k 976RTD 72F A mean128.93210.0666.27488.942691,296.2141,454.794206.84339.024meanCarbon Composite1,630T300 15k9760.3180.1321226; 228; 229; 231; 232; 233Table 4.2.17(a); Table 4.2.17(c); Table 4.2.17(d); Table 4.2.17(f); Table 4.2.17(g); Table 4.2.17(h)RTD (72F/A)

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