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.
~210°C
~80°C
Yes
Yes
High
Low
Advantages: Easy to print, environmentally friendly, warp resistant
Disadvantages: Brittle, lacks UV resistance
| Fiber | Volume % | Results | Reference |
|---|---|---|---|
| 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.
High
Yes
Excellent
Excellent
High
Advantages: Tough, impact resistant, durable
Disadvantages: Prone to warping, requires high temperatures
| Fiber | Volume % | Results | Reference |
|---|---|---|---|
| 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.
Up to 265°C
High (hygroscopic)
Excellent
Excellent
High
Advantages: Impact and wear resistant, durable
Disadvantages: Hygroscopic (moisture absorbing), warping tendency, high print temperatures
| Fiber | Volume % | Results | Reference |
|---|---|---|---|
| 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.
Moderate
Excellent
Excellent
Low
Yes
Advantages: UV-resistant, excellent mechanical properties, minimal warping, chemical resistant
Disadvantages: Poor adhesion, stringing during printing
| Fiber | Volume % | Results | Reference |
|---|---|---|---|
| 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.
Up to 310°C
150°C
High
Highest
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.
95
High
Excellent
Excellent
Semi-transparent
Advantages: Flexible, strong, excellent layer bonding, easy to print among flexible filaments
| Fiber | Volume % | Results | Reference |
|---|---|---|---|
| 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.
| Fiber | Content | Results | Reference |
|---|---|---|---|
| Hemp | 5% | Highest tensile strength | Sultan et al., 2024 |
| Hemp | 20% | Highest Young's modulus | Sultan et al., 2024 |
Other Thermoplastics
| Material | Key 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 Type | Examples |
|---|---|
| Photo-curable resins | UV-cured polymers |
| Acrylic-based resins | Various acrylates |
| Cyanate ether | High-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 |
|---|---|---|---|---|---|
| PLA | Low | Moderate | Low | Easy | Low |
| ABS | High | High | Moderate | Moderate | Low |
| Nylon/PA | High | High | High | Difficult | Moderate |
| PETG | Moderate | High | Moderate | Easy | Low |
| PC | Very High | Highest | Moderate | Difficult | Moderate |
| TPU | Moderate | Moderate | Highest | Moderate | Moderate |
| PP | Moderate | Moderate | High | Moderate | Low |
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 Requirement | Recommended Materials |
|---|---|
| High strength | PC, Nylon/PA + Carbon fiber |
| Flexibility | TPU |
| Outdoor use | PETG (UV resistant) |
| Biodegradability | PLA, PBS |
| Impact resistance | ABS, Nylon |
| Chemical resistance | PETG, PP |
| Food contact | PLA, PETG, Nylon (food-safe grades) |
| Low cost | PLA, 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 Type | Standard | Purpose |
|---|---|---|
| Tensile Testing | ASTM D638, ISO 527 | Measures ultimate tensile strength, modulus, and elongation |
| Flexural Testing | ASTM D790, ISO 178 | Three-point bending to measure flexural strength and modulus |
| Impact Testing | ASTM D256, ISO 179 | Izod or Charpy impact resistance |
| Interlaminar Shear | ASTM D2344 | Short beam shear test for layer adhesion |
| Dynamic Mechanical Analysis | ASTM D5023 | Viscoelastic 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:
- Scanning Electron Microscopy (SEM): Examines fiber-matrix interface, fiber pull-out, and fracture surfaces
- Micro-CT: Non-destructive 3D imaging of internal void distribution
- Optical Microscopy: Cross-sectional analysis of fiber distribution and impregnation quality
- Thermogravimetric Analysis (TGA): Measures thermal stability and fiber volume fraction
- Differential Scanning Calorimetry (DSC): Determines crystallinity and thermal transitions
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 Material | 2024-2025 Advance | Key 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:
| Institution | Key Researchers | Matrix 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:
- Composites Part A - Applied science and manufacturing
- Additive Manufacturing - AM-focused research
- Polymer Testing - Testing and characterization
- Polymers (MDPI) - Open access polymer science
See Top Journals for complete journal list with impact metrics.