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Composite Material Properties: Celion 3000 F670

ETD 550F A B-basis 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: Celion 3000 F6703 rows
material systemcondition basisE1 GPa (GPa)E2 GPa (GPa)S MPa (MPa)Vf pct (%)Xc MPa (MPa)Xt MPa (MPa)Yc MPa (MPa)Yt MPa (MPa)basisdensity kg m3 (kg/m3)fibermatrixply thickness mm (mm)source pagesource tabletest condition
Celion 3000 F670ETD 550F A B-basis60.520.684B1,610Celion 3000F6700.3505370Table 4.5.1(d)ETD (550F/A)
Celion 3000 F670ETD 550F A mean55.77952.88360.5455.054799.792373.696623.286mean1,610Celion 3000F6700.3505367; 368; 369; 370Table 4.5.1(a); Table 4.5.1(b); Table 4.5.1(c); Table 4.5.1(d)ETD (550F/A)
Celion 3000 F670RTD 75F A mean59.36455.7175.15360.5685.339910.108543.996737.739mean1,610Celion 3000F6700.3505367; 368; 369; 370; 372Table 4.5.1(a); Table 4.5.1(b); Table 4.5.1(c); Table 4.5.1(d); Table 4.5.1(f)RTD (75F/A)

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