Composite Material Properties: KEVLAR 49 EPOXY FABRIC
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.
| material system | condition basis | E1 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) | basis | density kg m3 (kg/m3) | form | nu12 (dimensionless) | ply thickness mm (mm) | test condition |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| KEVLAR 49 EPOXY FABRIC | RTD mean | 41.36856 | 41.36856 | 2.964747 | 51.7107 | 55 | 393.00132 | 393.00132 | 20.68428 | 20.68428 | mean | 1,383.995 | Balanced Fabric | 0.05 | 0.254 | RTD |
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