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Kevlar 49 CHOP

Reinforced grade

CHOP = chopped fiber (3–12 mm) for compounds and friction materials

Pick for thermoplastic/thermoset compounding, brake and gasket materials, and asbestos replacement.

High cost $$$$

Values for the CHOP 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
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—
CHOPThis page
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 CHOP?

Kevlar 49 CHOP is Kevlar 49 in the CHOP grade — pick for thermoplastic/thermoset compounding, brake and gasket materials, and asbestos replacement. Kevlar 49 CHOP has a tensile strength of 3,000 MPa (435 ksi), stronger than 81% of composite grades. Elongation at break is 2.4% and the elastic modulus is 112 GPa (16.2 Msi). Kevlar 49 CHOP has a density of 1.44 g/cm³ (0.052 lb/in³), lighter than 61% 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 — 0.04 W/m·K (0.0231 BTU/hr·ft·°F), worse than 91% of composite grades
  • Difficult to machine — 20/100, worse than 77% of composite grades

Kevlar 49 CHOP properties

Typical room-temperature values for Kevlar 49 CHOP; 11 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 CHOP has a density of 1.44 g/cm³ (0.052 lb/in³), lighter than 61% of composite grades. Its glass-transition temperature is 360°C (680 °F).

Density1.44 g/cm³0.05 lb/in³
Glass Transition (Tg)360°C680 °F
Water Absorption (Saturation)4%

Mechanical5

Kevlar 49 CHOP has a tensile strength of 3,000 MPa (435 ksi), stronger than 81% of composite grades. Elongation at break is 2.4% and the elastic modulus is 112 GPa (16.2 Msi).

Elastic (Young's) Modulus112 GPa16.2 Msi
Shear Modulus2.9 GPa0.42 Msi
Poisson's Ratio0.36
Tensile Strength (Ultimate)3,000 MPa435 ksi
Elongation at Break2.4%

Thermal8

Kevlar 49 CHOP is rated for continuous service to 180°C (356 °F). It conducts heat at 0.04 W/m·K (0.0231 BTU/hr·ft·°F), worse than 91% of composite grades. Thermal expansion is -2 µm/m·K (-1.11 µin/in·°F).

Thermal Conductivity0.04 W/m·K0.02 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)180°C356 °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 Index29%
Max Service Temperature (short-term)250°C482 °F

Electrical4

Kevlar 49 CHOP has an electrical resistivity of 1×10¹³ Ω·m.

Electrical Resistivity1×10¹³ Ω·m3.94×10²⁰ 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 (70/100), worse than 64% of composite grades. UV resistance is poor.

Corrosion ResistanceVery good70/100
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 CHOP 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 CHOP'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 CHOP

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 CHOP — frequently asked

What is Kevlar 49 CHOP used for?

Kevlar 49 CHOP 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 CHOP?

Kevlar 49 CHOP has a typical tensile strength of 3,000 MPa (435 ksi) — stronger than 81% of composite grades. Strength varies by condition: see the 5 listed tempers.

Is Kevlar 49 CHOP 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 CHOP 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 CHOP?

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 CHOP 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 CHOP?

Kevlar 49 CHOP is rated for continuous use to about 180°C (356 °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.