Matrix Materials
Thermoplastics8+
Most CommonPLA, Nylon, ABS
High-PerformancePEEK, PEI
Print Temp Range180-400°C

Overview

The matrix material in fiber-reinforced composites serves three critical functions: transferring loads between fibers, protecting fibers from environmental damage, and maintaining fiber alignment during and after fabrication. In FDM continuous fiber composites, the matrix also determines processability—the material must flow through the nozzle while adequately wetting the reinforcing fibers. Two main categories of matrix materials are used: thermoplastics (which melt and solidify reversibly) and thermosets (which cure irreversibly). FDM primarily uses thermoplastics due to the melt-extrusion nature of the process, though thermoset-coated fibers from companies like Anisoprint have also been developed.

Research on matrix materials for FDM composites is published in journals including Composites Part A, Composites Part B, Polymer Testing, Polymers, and Additive Manufacturing. Key research groups at the University of Tehran, Xi'an Jiaotong University, and various European institutions have extensively characterized matrix-fiber interactions. This means that comprehensive data exists for most common matrix-fiber combinations. For example, PLA is widely studied because it is easy to print and biodegradable, but it has limited temperature resistance (Tg ~60°C). In contrast, PEEK offers exceptional high-temperature performance, specifically for aerospace applications, but requires specialized high-temperature printing equipment. The choice of matrix material fundamentally determines the processing parameters, mechanical performance, and application suitability of the final composite.

Matrix characterization typically involves thermal analysis (DSC, TGA), mechanical testing (tensile, flexural, impact per ASTM standards), and interface characterization (fiber push-out, fragmentation tests). Understanding the properties, processing requirements, and limitations of each matrix material is essential for optimizing FDM composite fabrication.

See also: Fiber Types | FDM Mechanisms | Top Journals | Research Teams

Why Matrix Material Selection Matters

Matrix material selection is one of the most critical decisions in FDM composite design, affecting nearly every aspect of both the manufacturing process and final part performance. The matrix must be compatible with the chosen fiber type, processable at temperatures that don't degrade the fibers, and suitable for the intended application environment.

Thermal compatibility is the first consideration. Each thermoplastic has a specific processing temperature window—too low and the polymer won't flow properly around the fibers, too high and thermal degradation occurs. For natural fibers like flax or hemp, this is particularly important as these fibers begin to degrade around 200°C, limiting matrix choices to lower-temperature polymers like PLA.

Crystallinity affects both processability and mechanical properties. Semi-crystalline polymers (Nylon, PP, PEEK) offer higher strength and chemical resistance but are more prone to warping during cooling. Amorphous polymers (ABS, PC, PETG) are more dimensionally stable but may have lower ultimate strength.

Fiber-matrix adhesion is crucial for load transfer. Poor adhesion leads to fiber pull-out under stress, negating much of the reinforcement benefit. Surface treatments, coupling agents, or matrix modifications can improve adhesion, but inherent chemical compatibility between fiber and matrix remains the foundation of good interfacial bonding.

Key Selection Criteria

  • Processing temperature: Must be compatible with fiber thermal stability
  • Viscosity: Lower viscosity improves fiber impregnation
  • Shrinkage: High shrinkage causes warping and residual stresses
  • Chemical compatibility: Affects fiber-matrix adhesion
  • Environmental resistance: UV, moisture, and chemical exposure
  • Cost and availability: Practical considerations for production

Thermoplastic Matrices

Thermoplastics melt at elevated temperatures and solidify during cooling, making them suitable for FDM's layer-by-layer deposition process. Unlike thermosets, thermoplastics can be remelted and reshaped, which is essential for the extrusion-based FDM process where material flows through a heated nozzle before deposition.

The thermoplastic matrices used in FDM composites span a wide range of properties and costs, from commodity polymers like PLA and ABS to high-performance engineering plastics like PEEK. Each material offers distinct trade-offs between ease of processing, mechanical performance, environmental resistance, and cost. The following sections detail the most commonly used thermoplastic matrices for continuous fiber FDM composites.

PLA (Polylactic Acid)

Biodegradable thermoplastic derived from organic (non-petroleum) sources.

Print temp
~210°C
Bed temp
~80°C
Biodegradable
Yes
Food safe
Yes
Warp resistance
High
UV resistance
Low

Advantages: Easy to print, environmentally friendly, warp resistant

Disadvantages: Brittle, lacks UV resistance

FiberVolume %ResultsReference
Carbon 6.6% In-nozzle impregnation method developed Matsuzaki et al., 2016
Carbon 27% Bending strength 335 MPa, modulus 30 GPa Tian et al., 2016
Carbon 34% 14% tensile, 164% bending strength increase Li et al., 2016
Carbon/Flax 18.86-39.27% 430% (carbon), 325% (flax) tensile increase Kuschmitz et al., 2021
Aramid 8.6% Comprehensive mechanical characterization Bettini et al., 2017
Flax 211% flexural strength, 224% modulus increase Zhang et al., 2020
Basalt Comparable tensile, superior flexural vs PLA/CF Sang et al., 2019

ABS (Acrylonitrile Butadiene Styrene)

Widely used engineering plastic with excellent toughness.

Print temp
High
Food safe
Yes
Impact resistance
Excellent
Wear resistance
Excellent
Warp tendency
High

Advantages: Tough, impact resistant, durable

Disadvantages: Prone to warping, requires high temperatures

FiberVolume %ResultsReference
Carbon 6.5% Flexural strength 127 MPa, UTS 147 MPa, shear 2.81 MPa Yang et al., 2017
Carbon 1.6% Enhanced tensile and fatigue strength with thermal bonding Nakagawa et al., 2017
Kenaf 5-10% Tensile strength 11.48-18.59 MPa Han et al., 2022

Nylon / Polyamide (PA)

Engineering thermoplastic with excellent wear resistance and durability. PA6 is the most common grade for FDM filaments.

Print temp
Up to 265°C
Moisture absorption
High (hygroscopic)
Impact resistance
Excellent
Wear resistance
Excellent
Warp tendency
High

Advantages: Impact and wear resistant, durable

Disadvantages: Hygroscopic (moisture absorbing), warping tendency, high print temperatures

FiberVolume %ResultsReference
Kevlar 4.04-10.1% Elastic modulus 1767-9001 MPa Melenka et al., 2016
Carbon 6CF layers Tensile strength 370-520 MPa Van Der Klift et al., 2016
Carbon/Glass/Kevlar 26.8-73.4% Highest shear strength for carbon Caminero et al., 2018
Carbon/Glass 25% modulus decrease at 95% RH (carbon) Chabaud et al., 2019

Moisture Effects on PA6

  • At 9-98% moisture content: 25% decrease in longitudinal tensile modulus for carbon fiber composites
  • 18% decrease in tensile strength for carbon fiber composites
  • Glass fiber composites: stable modulus but 25% strength decrease
  • Debonding more significant at 95% RH vs 15% RH

Source: Chabaud et al., 2019

PETG (Polyethylene Terephthalate Glycol-Modified)

Modified PET with lower melting temperature and improved printability.

Print temp
Moderate
UV resistance
Excellent
Chemical resistance
Excellent
Warp tendency
Low
Food safe
Yes

Advantages: UV-resistant, excellent mechanical properties, minimal warping, chemical resistant

Disadvantages: Poor adhesion, stringing during printing

FiberVolume %ResultsReference
Aramid 45% +1550% modulus, +1150% strength vs unreinforced Rijckaert et al., 2022
Carbon 20% 23% yield strength improvement vs conventional structures Alarifi, 2023

PC (Polycarbonate)

Advanced engineering thermoplastic with the highest strength among FDM filaments.

Print temp
Up to 310°C
Glass transition
150°C
Hygroscopic
High
Strength
Highest
Warp tendency
High

Advantages: Highest strength, excellent mechanical properties, high temperature resistance

Disadvantages: Requires very high print temperatures, highly hygroscopic, warping prone

TPU (Thermoplastic Polyurethane)

Flexible filament with excellent elasticity.

Shore Hardness
95
Flexibility
High
Layer bonding
Excellent
Abrasion resistance
Excellent
Appearance
Semi-transparent

Advantages: Flexible, strong, excellent layer bonding, easy to print among flexible filaments

FiberVolume %ResultsReference
Glass 34.8% >700% increase in tensile strength and elastic modulus Akhoundi et al., 2020

PP (Polypropylene)

Recycled-compatible thermoplastic with good chemical resistance and low cost.

FiberContentResultsReference
Hemp 5% Highest tensile strength Sultan et al., 2024
Hemp 20% Highest Young's modulus Sultan et al., 2024

Other Thermoplastics

MaterialKey Characteristics
HIPS (High-Impact Polystyrene)Soluble support material, durable, emits fumes
PVA (Polyvinyl Alcohol)Water-soluble support, biodegradable, expensive
PEEK (Polyetheretherketone)High-performance, biomedical applications
PEI (Polyetherimide)High temperature resistance
PPSU (Polyphenyl Sulfone)Chemical resistance
PBS (Polybutylene Succinate)Biodegradable (63% modulus improvement with hemp)

Thermoset Matrices

Thermosets undergo irreversible curing (hardening) and are less common in FDM but used in some continuous fiber composite applications. Unlike thermoplastics, once cured, thermosets cannot be remelted or reshaped, which presents both advantages and limitations for additive manufacturing.

The primary advantage of thermosets is their superior fiber wetting and impregnation during the liquid resin stage, which typically results in better fiber-matrix adhesion and lower void content compared to thermoplastic composites. However, the requirement for curing (often with heat or UV light) adds complexity to the manufacturing process and eliminates the possibility of recycling or repair through remelting.

Material TypeExamples
Photo-curable resinsUV-cured polymers
Acrylic-based resinsVarious acrylates
Cyanate etherHigh-temperature applications

Anisoprint uses thermosetting resin for pre-impregnating continuous fibers, combining the benefits of thermoset fiber wetting with the geometric freedom of additive manufacturing.

Matrix Material Comparison

The following table provides a comparative overview of the major thermoplastic matrices used in FDM composites. These properties represent general trends; specific grades and formulations may vary significantly.

Material Print Temp Strength Flexibility Ease of Print Cost
PLALowModerateLowEasyLow
ABSHighHighModerateModerateLow
Nylon/PAHighHighHighDifficultModerate
PETGModerateHighModerateEasyLow
PCVery HighHighestModerateDifficultModerate
TPUModerateModerateHighestModerateModerate
PPModerateModerateHighModerateLow

Material Selection Guide

Selecting the optimal matrix material requires balancing multiple factors including the intended application, environmental conditions, available equipment, and budget constraints. The following table provides guidance for common application requirements.

Application RequirementRecommended Materials
High strengthPC, Nylon/PA + Carbon fiber
FlexibilityTPU
Outdoor usePETG (UV resistant)
BiodegradabilityPLA, PBS
Impact resistanceABS, Nylon
Chemical resistancePETG, PP
Food contactPLA, PETG, Nylon (food-safe grades)
Low costPLA, ABS, PETG

When selecting a matrix material, also consider the available fiber types. Carbon fibers are compatible with most matrices, but natural fibers require lower processing temperatures (typically <200°C) to avoid thermal degradation. Glass fibers offer good compatibility across the temperature range but may require coupling agents for optimal adhesion with certain polymers.

Testing Methods

Characterizing the mechanical properties of matrix materials and their composites requires standardized testing methods. The following protocols are commonly used in the literature to evaluate FDM composite performance.

Mechanical Testing Standards

Test TypeStandardPurpose
Tensile TestingASTM D638, ISO 527Measures ultimate tensile strength, modulus, and elongation
Flexural TestingASTM D790, ISO 178Three-point bending to measure flexural strength and modulus
Impact TestingASTM D256, ISO 179Izod or Charpy impact resistance
Interlaminar ShearASTM D2344Short beam shear test for layer adhesion
Dynamic Mechanical AnalysisASTM D5023Viscoelastic properties and glass transition temperature

Microstructural Analysis

Understanding the fiber-matrix interface and void distribution is critical for optimizing composite properties. Common characterization techniques include:

These analytical methods help researchers correlate processing parameters with microstructural features and ultimately with mechanical performance, enabling systematic optimization of FDM composite fabrication.

Recent Developments (2024-2025)

Significant advances in matrix materials for FDM continuous fiber composites have emerged:

PEEK Vacuum Printing

Printing high-temperature PEEK matrix composites in vacuum environments has achieved significant improvements. Research demonstrated maximum flexural stress of 516 MPa for CFRTP parts printed with novel water-cooling systems in vacuum chambers, addressing the challenges of reduced heat transfer during high-temperature processing [J. Manuf. Processes, 2024].

Continuous Glass Fiber/PEEK for Aerospace

CGF/PEEK composites show promise for aerospace radome applications requiring both structural support and dielectric performance under aerothermal conditions. Recent work prepared CGF/PEEK filaments optimized for additive manufacturing with high-temperature resistance [Composites Part B, 2024].

Heat Treatment Optimization

Optimized heat treatment at 250°C for 6 hours improves interlaminar shear strength (ILSS) by 85% for continuous fiber reinforced PEEK compared to untreated samples. UV laser-assisted FDM combined with post-treatment addresses dimensional accuracy issues from crystallization-induced shrinkage [Polymer Composites, 2024].

Thermoset Matrix Printing

Continuous carbon fiber reinforced phenolic resin composites have been produced via in-situ curing 3D printing. This enables high-temperature resistant thermoset CFRPs previously not achievable with FDM thermoplastic approaches [J. Reinf. Plastics Comp., 2025].

Matrix Material2024-2025 AdvanceKey Result
PEEK (vacuum) Vacuum environment printing with water cooling 516 MPa flexural stress
PEEK (heat treated) Optimized heat treatment protocol 85% ILSS improvement
CGF/PEEK Aerospace radome-grade filaments High-temp + dielectric performance
Phenolic resin In-situ curing thermoset printing Expanded high-temp applications
Bio-based PA10.10 Sustainable automotive-grade matrix 25% weight reduction vs ABS

Space Environment Performance (2025)

Research on continuous carbon fiber reinforced PEEK for space applications has characterized mechanical behavior at operating temperatures from -150°C to +150°C, demonstrating PEEK's suitability for space structures requiring thermal cycling resistance [Polymer Composites, 2025].

Leading Research Teams

Key research groups advancing matrix material development:

InstitutionKey ResearchersMatrix Focus
Politecnico di Torino Padovano, E. [Scholar], Lupone, F., Badini, C. PA/carbon fiber composites, layup optimization
Xi'an Jiaotong University Tian, X. [RG], Yang, C., Li, D. PLA matrix optimization, interface enhancement
NASA Langley Research Center Gardner, J.M. [Scholar], Siochi, E.J. [RG] High-temperature thermoplastics (ULTEM), CNT reinforcement
University of Alberta Melenka, G.W. [Scholar], Carey, J.P. [Scholar] Nylon matrix composites, predictive modeling

See Research Teams for complete listing.

Key Journals

Matrix material research for FDM composites is primarily published in:

See Top Journals for complete journal list with impact metrics.