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Kevlar 49 PREPREG-EP

Matrix

Pick for autoclave/oven-cured aerospace and sporting-goods laminates needing repeatable fiber volume and resin content.

High cost $$$$

Values for the PREPREG-EP condition

Other Kevlar 49 grades and fills

Kevlar 49 is listed in 5 conditions; see the grade overview at Kevlar 49.

Compare all 5 grades and fillsHide
Grade · open for datasheetBest forYield MPaTensile MPaElong. %Hardness
Woven fabric / epoxy laminate, Vf ≈ 50 %
Design values for quasi-isotropic hand-layup or infused panels (hulls, radomes, impact skins).—4801.9—
Kevlar 49 / carbon hybrid fabric laminate
Pick when carbon stiffness/compression must be combined with aramid impact and splinter containment.—6201.488 Shore D
PREPREG-EPThis page
Epoxy prepreg (UD or woven, 120–180 °C cure)
Pick for autoclave/oven-cured aerospace and sporting-goods laminates needing repeatable fiber volume and resin content.—1,3501.886 Shore D
Unidirectional Kevlar 49 / epoxy laminate, Vf ≈ 60 %
Design values for 0° dominated tension-critical structures (pressure vessels, tension members).—1,3801.8—
Chopped fiber (3–12 mm) for compounds and friction materials
Pick for thermoplastic/thermoset compounding, brake and gasket materials, and asbestos replacement.—3,0002.4—

What is Kevlar 49 PREPREG-EP?

Kevlar 49 PREPREG-EP is Kevlar 49 in the PREPREG-EP condition — pick for autoclave/oven-cured aerospace and sporting-goods laminates needing repeatable fiber volume and resin content. Kevlar 49 PREPREG-EP has a tensile strength of 1,350 MPa (196 ksi), stronger than 73% of composite grades. Elongation at break is 1.8% and the elastic modulus is 75 GPa (10.9 Msi). Kevlar 49 PREPREG-EP has a density of 1.37 g/cm³ (0.0495 lb/in³), lighter than 67% of composite grades. Its glass-transition temperature is 360°C (680 °F).

Limitations

  • Degrades in UV without stabilisers — 20/100, worse than 94% of composite grades
  • Poor heat conductor — 0.2 W/m·K (0.116 BTU/hr·ft·°F), worse than 79% of composite grades
  • Limited service temperature — 120°C (248 °F), worse than 78% of composite grades
  • Difficult to machine — 20/100, worse than 77% of composite grades

Kevlar 49 PREPREG-EP properties

Typical room-temperature values for Kevlar 49 PREPREG-EP; 18 are specific to this condition. Other listed values are Kevlar 49 reference data and may not represent this condition. Bars are the position among composite grades.

Physical3

Kevlar 49 PREPREG-EP has a density of 1.37 g/cm³ (0.0495 lb/in³), lighter than 67% of composite grades. Its glass-transition temperature is 360°C (680 °F).

Density1.37 g/cm³0.05 lb/in³
Glass Transition (Tg)360°C680 °F
Water Absorption (Saturation)4%

Mechanical5

Kevlar 49 PREPREG-EP has a tensile strength of 1,350 MPa (196 ksi), stronger than 73% of composite grades. Elongation at break is 1.8% and the elastic modulus is 75 GPa (10.9 Msi).

Elastic (Young's) Modulus75 GPa10.9 Msi
Shear Modulus2.9 GPa0.42 Msi
Poisson's Ratio0.36
Tensile Strength (Ultimate)1,350 MPa196 ksi
Elongation at Break1.8%

Thermal8

Kevlar 49 PREPREG-EP is rated for continuous service to 120°C (248 °F). It conducts heat at 0.2 W/m·K (0.116 BTU/hr·ft·°F), worse than 79% of composite grades. Thermal expansion is -2 µm/m·K (-1.11 µin/in·°F).

Thermal Conductivity0.2 W/m·K0.12 BTU/hr·ft·°F
Specific Heat Capacity1,420 J/kg·K0.34 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)-2 µm/m·K-1.1 µin/in·°F
Max Service Temperature (continuous)120°C248 °F
Min Service Temperature-196°C-321 °F
Flammability (UL 94)Self-extinguishing, does not melt or drip; chars above ~425 °C. Aramid fabric/laminates commonly qualify V-0 in thin sections.
Limiting Oxygen Index28%
Max Service Temperature (short-term)250°C482 °F

Electrical4

Kevlar 49 PREPREG-EP has an electrical resistivity of 1×10¹² Ω·m.

Electrical Resistivity1×10¹² Ω·m3.94×10¹⁹ µΩ·in
Dielectric Constant (1 MHz)4
Dissipation Factor (1 MHz)0.02
Volume Resistivity1×10¹⁵ Ω·cm

Chemical & Environmental3

Corrosion resistance is very good (75/100), worse than 55% of composite grades. UV resistance is poor.

Corrosion ResistanceVery good75/100
UV / Weathering ResistancePoor20/100
Chemical Resistance SummaryExcellent against hydrocarbons, ketones, alcohols, chlorinated solvents and seawater; degraded by strong mineral acids, hot concentrated alkalis, chlorine bleach and prolonged UV/sunlight; hydrolytically sensitive at high temperature and humidity.

Sustainability3

Producing a kilogram of Kevlar 49 PREPREG-EP takes about 280 MJ of energy and emits 17 kg of CO₂ — more than 63% of composite grades. Typical recycled content is 0%.

Embodied Energy (primary production)280 MJ/kg120,378 BTU/lb
Embodied Carbon (primary production)17 kg CO₂/kg
Typical Recycled Content0%

Manufacturability1

Kevlar 49 PREPREG-EP's machinability is poor (20/100, worse than 77% of composite grades).

MachinabilityPoor20/100

Values are nominal handbook figures for design screening. Confirm any required mill or lot documentation when quoting.

Working with Kevlar 49 PREPREG-EP

Is Kevlar 49 easy to machine?

Cut with serrated/shear scissors, hot knife or abrasive waterjet; drilling needs brad-point or dagger drills with backing to stop fuzzing and delamination — carbide tools dull quickly.

Can Kevlar 49 be welded?

Not weldable; join by adhesive bonding, co-cured resin joints or mechanical fasteners with bushings to avoid fiber crushing.

Can Kevlar 49 be formed, bent or molded?

Excellent drape for hand layup, RTM/infusion, braiding and filament winding; dry the fiber (~4 h at 100–120 °C) before impregnation and use low-viscosity resin plus vacuum to fully wet the yarns.

What surface finishes work on Kevlar 49?

Seal all cut edges with resin to block moisture wicking; sanding leaves fuzz, so use peel-ply for bond surfaces and pigmented/UV-blocking topcoats or gelcoat for outdoor exposure.

Kevlar 49 chemical composition (wt %)

Limits by weight percent from the governing specification, written the way the spec states them — a single maximum for impurities, a range for alloying elements, and the base element as balance. Nominal is the typical mid-range value.

ElementSpec limit (wt %)Nominal
p-phenylenediamine (PPD) monomer unitas-polymerized mole basis≈ 4545
terephthaloyl chloride (TCl) monomer unias-polymerized mole basis≈ 5555
surface finish / sizingform-dependent (weaving, epoxy-compatible or none)0 – 10.3
poly(p-phenylene terephthalamide) (PPTA)condensation polymer of p-phenylenediamine and terephthaloyl chloride; ~0.1–1 % surface finish/sizing depending on formbalance—

Kevlar 49 PREPREG-EP — frequently asked

What is Kevlar 49 PREPREG-EP used for?

Kevlar 49 PREPREG-EP is typically used for aerospace composite panels, boat hulls, pressure vessels, sporting goods and armor laminates. In short: standard structural aramid fiber; best impact-to-weight laminate; poor compressive strength.

What is the tensile strength of Kevlar 49 PREPREG-EP?

Kevlar 49 PREPREG-EP has a typical tensile strength of 1,350 MPa (196 ksi) — stronger than 73% of composite grades. Strength varies by condition: see the 5 listed tempers.

Is Kevlar 49 PREPREG-EP easy to machine?

Not especially — machinability is rated poor (20/100, worse than 77% of composite grades). Cut with serrated/shear scissors, hot knife or abrasive waterjet; drilling needs brad-point or dagger drills with backing to stop fuzzing and delamination — carbide tools dull quickly.

Can Kevlar 49 PREPREG-EP be welded?

Not weldable; join by adhesive bonding, co-cured resin joints or mechanical fasteners with bushings to avoid fiber crushing.

What surface finishes work on Kevlar 49 PREPREG-EP?

Seal all cut edges with resin to block moisture wicking; sanding leaves fuzz, so use peel-ply for bond surfaces and pigmented/UV-blocking topcoats or gelcoat for outdoor exposure.

Can Kevlar 49 PREPREG-EP be formed, bent or molded?

Excellent drape for hand layup, RTM/infusion, braiding and filament winding; dry the fiber (~4 h at 100–120 °C) before impregnation and use low-viscosity resin plus vacuum to fully wet the yarns.

What is the maximum service temperature of Kevlar 49 PREPREG-EP?

Kevlar 49 PREPREG-EP is rated for continuous use to about 120°C (248 °F), and briefly to 250°C. Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

Sources

  1. Kevlar Aramid Fiber Technical Guide (Kevlar 49 properties) — DuPont (2017)
  2. ASM Handbook Vol. 21: Composites — ASM International (2001)
  3. CMH-17 (MIL-HDBK-17) Composite Materials Handbook, Vol. 3 Polymer Matrix Composites — SAE International / CMH-17 (2012)
  4. ASTM D7269 – Tensile Testing of Aramid Yarns — ASTM (2017)
  5. CES/Granta EduPack eco and mechanical data, aramid fiber & KFRP records — Ansys Granta (2023)

Property data is compiled from published supplier and standards handbooks and normalised for comparison. Nothing on this page is a certification — request mill certs, CoC or material test reports with your order.