Carbon Fiber PEEK Matrix
Matrix
also CFRP, CFF
Pick for 250 °C service, hot-wet/chemical exposure, weldable and reformable thermoplastic structure.
Values for the PEEK Matrix condition
Other Carbon Fiber grades and fills
Carbon Fiber is listed in 7 conditions; see the grade overview at Carbon Fiber.
Compare all 7 grades and fillsHide
| Grade · open for datasheet | Best for | Yield MPa | Tensile MPa | Elong. % | Hardness |
|---|---|---|---|---|---|
compression-molded chopped prepreg or SMC | Pick for complex net-shape parts and thick sections where quasi-isotropic mid-level properties are enough. | 250 | 0.9 | ||
Woven 2×2 Twill / Plain | Pick for panels, plates and cosmetic parts needing equal 0/90 properties and drapeable layup. | 620 | 1.2 | ||
Epoxy MatrixDefault woven-fabric epoxy prepreg laminate (autoclave/press cured) | Default general-purpose CFRP: 3K twill/plain woven fabric in 120–180 °C cure epoxy, balanced 0/90 properties, panels and plates. | 650 | 1.2 | ||
high-modulus PAN or pitch fiber epoxy laminate (UD, 0°) | Pick when stiffness and dimensional stability dominate (optical benches, satellite structures); strength and toughness are sacrificed. | 1,300 | 0.4 | ||
high-temperature laminate | Pick when continuous service is 180–230 °C (engine nacelles, hot structure, high-speed airframe) and low outgassing is required. | 1,900 | 1.4 | ||
PEEK MatrixThis page CF/PEEK thermoplastic composite (APC-2 type, UD) | Pick for 250 °C service, hot-wet/chemical exposure, weldable and reformable thermoplastic structure. | 2,070 | 1.4 | ||
Unidirectional prepreg laminate, 0° fiber direction | Pick for maximum stiffness/strength along one axis: spars, tubes, pultruded rods, stiffening caps. | 2,100 | 1.5 |
What is Carbon Fiber PEEK Matrix?
Carbon Fiber PEEK Matrix is Carbon Fiber in the PEEK Matrix condition — pick for 250 °C service, hot-wet/chemical exposure, weldable and reformable thermoplastic structure. Carbon Fiber PEEK Matrix has a tensile strength of 2,070 MPa (300 ksi), stronger than 77% of composite grades. Elongation at break is 1.4% and the elastic modulus is 138 GPa (20 Msi). Carbon Fiber PEEK Matrix has a density of 1.6 g/cm³ (0.0578 lb/in³), lighter than 53% of composite grades. Its glass-transition temperature is 143°C (289 °F). Epoxy Matrix is the default condition FabDigit quotes; PEEK Matrix is available on request or by drawing note.
Advantages
- Low, predictable mold shrinkage — 0.1%, better than 100% of composite grades
- Polishes to a fine finish — 60/100, better than 90% of composite grades
- Tough — resists crack growth — 30 MPa·√m (27.3 ksi·√in), better than 85% of composite grades
- Low moisture uptake — 0.1%, better than 85% of composite grades
Carbon Fiber PEEK Matrix properties
Typical room-temperature values for Carbon Fiber PEEK Matrix; 13 are specific to this condition. Other listed values are Carbon Fiber reference data and may not represent this condition. Bars are the position among composite grades.
Physical4
Carbon Fiber PEEK Matrix has a density of 1.6 g/cm³ (0.0578 lb/in³), lighter than 53% of composite grades. Its glass-transition temperature is 143°C (289 °F).
Mechanical11
Carbon Fiber PEEK Matrix has a tensile strength of 2,070 MPa (300 ksi), stronger than 77% of composite grades. Elongation at break is 1.4% and the elastic modulus is 138 GPa (20 Msi).
Thermal9
Carbon Fiber PEEK Matrix is rated for continuous service to 250°C (482 °F). It conducts heat at 5 W/m·K (2.89 BTU/hr·ft·°F), better than 64% of composite grades. Thermal expansion is 2 µm/m·K (1.11 µin/in·°F).
Electrical3
Carbon Fiber PEEK Matrix has an electrical resistivity of 0.0015 Ω·m.
Chemical & Environmental3
Corrosion resistance is excellent (85/100), better than 65% of composite grades. UV resistance is fair.
Sustainability4
Producing a kilogram of Carbon Fiber PEEK Matrix takes about 350 MJ of energy and emits 24 kg of CO₂ — more than 75% of composite grades. Typical recycled content is 0%.
Manufacturability3
Carbon Fiber PEEK Matrix's machinability is fair (40/100, better than 57% of composite grades).
Values are nominal handbook figures for design screening. Confirm any required mill or lot documentation when quoting.
Working with Carbon Fiber PEEK Matrix
Is Carbon Fiber easy to machine?
Use PCD/diamond-coated or diamond-abrasive tooling, high speed and low feed with backing support to avoid delamination and fiber pull-out; vacuum extraction is mandatory (conductive, respirable dust) and coolant/tool wear is the cost driver.
Can Carbon Fiber be welded?
Thermoset CFRP cannot be welded — join by adhesive bonding (peel-ply/abraded surfaces) or bolted joints with generous bearing area; thermoplastic-matrix (PEEK/PA) variants can be induction, resistance or ultrasonically welded.
Can Carbon Fiber be formed, bent or molded?
Formed by prepreg hand layup/AFP with autoclave or press cure (120–180 °C), RTM/infusion of dry fabric, filament winding, pultrusion, or chopped-prepreg compression molding; thermoplastic tapes are stamp-formed above Tm.
What surface finishes work on Carbon Fiber?
Cannot be anodized or plated conventionally; finish by resin/gel surfacing film, filler-primer and 2K clear or paint with UV blocker, and always isolate from aluminium/steel with glass-fiber ply or sealant to prevent galvanic corrosion.
Carbon Fiber 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.
| Element | Spec limit (wt %) | Nominal |
|---|---|---|
| carbon fiber (PAN-based, T300/T700 classwt %; ≈50–60 vol % for autoclave prepreg laminates | 50 – 70 | 60 |
| sizing / interlayer toughenerfiber sizing plus thermoplastic toughening particles in aerospace prepregs | 0 – 2 | 1 |
| epoxy resin matrixDGEBA/amine or 180 °C-cure toughened epoxy; substituted by PEEK, BMI, cyanate ester or PA in other variants | ≥ 30 (balance) |
Carbon Fiber PEEK Matrix — frequently asked
What is Carbon Fiber PEEK Matrix used for?
Carbon Fiber PEEK Matrix is typically used for aerospace structural panels, bicycle frames, UAV airframes and booms, robot arms and end effectors, motorsport bodywork and aerodynamic parts and machine tool gantries and idler rollers. In short: lightweight aerospace laminate.
What is the tensile strength of Carbon Fiber PEEK Matrix?
Carbon Fiber PEEK Matrix has a typical tensile strength of 2,070 MPa (300 ksi) — stronger than 77% of composite grades. Strength varies by condition: see the 7 listed tempers.
Is Carbon Fiber PEEK Matrix easy to machine?
Not especially — machinability is rated fair (40/100, better than 57% of composite grades). Use PCD/diamond-coated or diamond-abrasive tooling, high speed and low feed with backing support to avoid delamination and fiber pull-out; vacuum extraction is mandatory (conductive, respirable dust) and coolant/tool wear is the cost driver.
Can Carbon Fiber PEEK Matrix be welded?
Thermoset CFRP cannot be welded — join by adhesive bonding (peel-ply/abraded surfaces) or bolted joints with generous bearing area; thermoplastic-matrix (PEEK/PA) variants can be induction, resistance or ultrasonically welded.
What surface finishes work on Carbon Fiber PEEK Matrix?
Cannot be anodized or plated conventionally; finish by resin/gel surfacing film, filler-primer and 2K clear or paint with UV blocker, and always isolate from aluminium/steel with glass-fiber ply or sealant to prevent galvanic corrosion.
Can Carbon Fiber PEEK Matrix be formed, bent or molded?
Formed by prepreg hand layup/AFP with autoclave or press cure (120–180 °C), RTM/infusion of dry fabric, filament winding, pultrusion, or chopped-prepreg compression molding; thermoplastic tapes are stamp-formed above Tm.
What is the maximum service temperature of Carbon Fiber PEEK Matrix?
Carbon Fiber PEEK Matrix is rated for continuous use to about 250°C (482 °F), and briefly to 180°C. Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.
Can FabDigit make parts in Carbon Fiber PEEK Matrix?
Yes — Carbon Fiber PEEK Matrix is available for CNC machining and sheet metal with instant online pricing. Upload a STEP file to get a price and a DFM check.
Sources
- CMH-17 Composite Materials Handbook, Vol. 2 (Polymer Matrix Composites — Material Properties) — SAE International / CMH-17 (2012)
- ASM Handbook Vol. 21: Composites — ASM International (2001)
- T300 / T700S / M55J carbon fiber and prepreg data sheets — Toray Composite Materials (2023)
- HexPly 8552 / 913 prepreg and HexTow fiber data sheets — Hexcel (2023)
- APC-2 / AS4-PEEK thermoplastic tape data sheet — Solvay (Cytec) (2022)
- Continuous Fiber Reinforcement (CFF/CFR) material properties — Markforged (2023)
- ASTM D3039 / D6641 / D7264 / D2344 composite test methods — ASTM International (2021)
- CES / Ashby material property and eco-property data for CFRP — Ansys Granta (2022)
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.