Kevlar 49/Epoxy Unidirectional (MIL-HDBK-17)
VerifiedcompositeKevlar 49/Epoxy unidirectional composite is a fiber-reinforced polymer made from DuPont Kevlar 49 aramid fibers aligned in a single direction (0°) and bonded in an epoxy matrix using prepreg layup manufacturing. This material balances exceptional tensile strength-to-weight ratio with impact resistance and damping characteristics inherent to aramid fibers, making it well-suited for applications demanding lightweight structural performance without the brittleness of carbon fiber composites. It is widely specified in aerospace, defense, and sporting goods industries where impact tolerance, vibration damping, and damage resistance outweigh the need for maximum stiffness, and its unidirectional ply format allows engineers to build custom laminate schedules for directional load optimization.
Compliance & Regulations
Fiber Direction
Ply Schedule
Laminate Code
[0]T
Fiber angles relative to the 0° reference direction (red arrow in 3D view). 0° = longitudinal, 90° = transverse, ±45° = shear paths.
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Compressive Strength(σc) | 60.05 | ksi | L | ||
Poisson's Ratio(ν) | 0.3400 | - | notes | ||
Shear Modulus(G) | 300.2 | ksi | notes | ||
Ultimate Tensile Strength(σUTS) | 4.351 | ksi | T | ||
Young's Modulus(E) | 11,022.9 | ksi | L |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Coefficient of Thermal Expansion(α (CTE)) | 30.00 | µin/in·°F | T |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | 0.04986 | lb/in³ | — |