ZenCore 3D
Carbon fiber composite manufacturing aerospace-grade parts
Structural Composites · Automotive · Aerospace · UAV

Advanced Composite ManufacturingCarbon Fiber & Fiberglass

Lightweight, high-strength composite components for automotive, UAV, and industrial applications. Hand layup, vacuum bagging, and resin infusion processes with aerospace-grade precision and traceability.

70%Weight reduction vs steel
Strength-to-weight vs aluminium
T700Carbon fiber grade
65%Max fibre volume fraction
Definition

What Are Composite Materials?

Composite materials combine continuous reinforcement fibers — carbon or glass — with a polymer resin matrix to create structures with exceptional strength-to-weight ratios unachievable with metals or unreinforced plastics alone.

The fiber provides tensile strength and stiffness along its length, while the resin binds the fibers, transfers load between plies, and protects against environmental degradation. The laminate designer controls ply orientation, fiber type, and core sandwich construction to precisely tailor stiffness and strength in any direction.

ZenCore 3D produces composite structures from prototype to small-series using proven wet layup, vacuum infusion, and autoclave-ready prepreg processes — with full documentation conforming to aerospace quality standards.

Weight Reduction

Up to 70% vs steel

vs equivalent strength

Structural Rigidity

High stiffness-to-weight

directional control

Impact Resistance

Excellent (GF variants)

energy absorption

Custom Layup

Any ply angle & count

per structural analysis

Processes

Manufacturing Methods

Four production processes matched to volume, geometry complexity, and required laminate quality — from rapid prototype hand layup to production-grade resin infusion.

Hand Layup

Flexible

Fiber plies placed manually onto the mold surface with wet or prepreg systems. Ideal for complex geometry, prototypes, and low-volume production where automation is not economical.

Use Cases

Applications Across Industries

From motorsport body panels to aerospace-grade UAV structures, our composites capability addresses the most demanding lightweight engineering requirements.

Carbon Fiber Car Body Panels

Door panels, hoods, wings, and bumpers for motorsport, tuning, and automotive OEM programs.

Automotive Dashboard Components

Interior trim, centre console panels, and structural dash carriers with integrated A-surface finish.

Aerospace Housings & Fairings

Lightweight structural enclosures, fairings, and access panels for aviation and space applications.

Fixed-Wing Drone Fuselage

Full fuselage shells and wing structures for UAV platforms requiring maximum strength-to-weight.

Drone Wings & Control Surfaces

Structural wing skins, control surfaces, and spars with calculated layup schedules for flight loads.

Industrial Covers & Enclosures

Machine guards, access panels, and protective covers replacing heavy steel or aluminium sheet.

Carbon fiber layup workshop composite manufacturing

Hand layup — carbon weave ply placement

Automotive carbon fiber body panel motorsport

Motorsport body panels

Carbon fiber UAV drone fuselage aerospace lightweight

Fixed-wing UAV structures

Methodology

Composite Manufacturing Workflow

An 8-stage manufacturing process from structural design through quality inspection, with full traceability at each step for aerospace and automotive program requirements.

Step 01

Design & Structural Analysis

Laminate schedule defined based on load requirements. FEA simulation validates ply orientation, core material selection, and failure modes before production begins.

Step 02

Mold Preparation

Mold surfaces cleaned and treated with release agent or PTFE film. Hard tooling CNC-machined from composite master; soft tooling produced from SLA prints for prototypes.

Step 03

Fiber Layup

Carbon or glass fabric plies cut to pattern and placed per laminate schedule. Ply angles programmed per structural analysis (0°, ±45°, 90°). Core materials interleaved where required.

Step 04

Resin Infusion

Epoxy or vinyl ester resin introduced through inlet ports. Vacuum draws resin front uniformly through fiber stack. Fibre volume fraction monitored via resin flow balance.

Step 05

Curing

Parts cured at 60–120 °C depending on resin system. Post-cure at elevated temperature achieves full glass transition temperature. Cure monitoring via thermocouple array.

Step 06

Demolding

Bagging materials removed. Part carefully separated from mold. Release quality checked. Complex molds split along pre-planned parting lines.

Step 07

Trimming & Finishing

Diamond-blade waterjet or CNC trim to net shape. Edge sealing applied. Surface finishing options: raw carbon weave, lacquer, gel coat, or primer-ready for paint.

Step 08

Quality Inspection

Dimensional check (CMM or ATOS scan). Tap test for delamination detection. Destructive coupon testing for first-article batch qualification. Full traceability report issued.

Production Envelope

Technical Capabilities

Our composite manufacturing cell handles parts up to 2,000 × 1,000 mm with fibre volume fractions up to 65%. Full laminate schedule documentation is provided with every production batch.

Capability Specifications

Maximum Part Dimensions
2,000 × 1,000 × 500 mm

standard production cell

Fiber Orientation Control
0° / 45° / 90° / custom

per ply schedule

Fibre Volume Fraction
50 – 65%

infusion process

Surface Finish (A-side)
Ra 0.4 – 1.6 µm

hard mold surface

Surface Finish (B-side)
Ra 1.6 – 6.3 µm

bag-side finish

Typical Wall Thickness
0.5 – 6 mm

dependent on ply count

Carbon Fiber Grades
T300 / T700 / T800

3K, 6K, 12K tow

Core Materials
Foam / Nomex / Aluminum

sandwich construction

Available Fiber & Resin Systems

Carbon Fiber

3K / 6K / 12K plain weave
2×2 twill weave (visual finish)
UD prepreg tape
T300 / T700 / T800 grades

Fiberglass

E-glass woven fabric
S-glass high-performance
Chopped strand mat (CSM)
Biaxial ±45° NCF

Resin Systems

Epoxy (ambient & elevated cure)
Vinyl ester (corrosion resistant)
Phenolic (fire-rated)
Bio-based epoxy variants

Weight vs Structural Performance

CFRP (Carbon/Epoxy)600–900 MPa
GFRP (Glass/Epoxy)350–500 MPa
Aluminium 6061310 MPa
ABS Plastic40 MPa

Tensile strength comparison — higher is better

Decision Guide

Composites vs Aluminium vs 3D Printed Parts

Weight-to-strength is where composites excel. Use this guide to determine when the investment in composite manufacturing is justified for your application.

CriterionComposites (CFRP/GFRP)AluminiumABS Plastic3D Printed
Specific strength (strength/weight)★★★★★ Best in class★★★☆☆ Good★★☆☆☆ Low★★★☆☆ Variable
Specific stiffness★★★★★ CFRP dominant★★★★☆ Good (isotropic)★★☆☆☆ Poor★★★☆☆ Moderate
Part weightUp to 70% lighterBaseline reference~35% lighterMaterial-dependent
Corrosion resistanceExcellent — no corrosionModerate — anodizing req.GoodVaries
Tooling cost€€ – €€€€ mold€€€ – €€€€€ CNC€€€ injection mold€ – none
Production speedDays per part (manual)Fast (CNC automated)Fast (injection)Fastest (no tooling)
Design freedomVery high – complex curvesLimited by machiningModerateHighest
Best applicationStructural · Lightweight · AeroPrecision · Thermal · EDMConsumer · Low loadPrototype · Custom

Choose Advanced Composites when…

  • Weight reduction is a primary structural requirement
  • Operating environment includes corrosive or marine conditions
  • Fatigue resistance over long service life is critical
  • Thermal expansion must be minimized or tailored
  • Electrical isolation or EMI transparency is required
  • Complex organic geometry cannot be achieved in metal

Consider alternatives when…

  • Production volume exceeds 1,000+ identical parts (consider thermoplastic)
  • Tight tolerance holes or threads require machined metal inserts
  • Budget does not allow for specialized composite tooling
  • Part requires isotropic mechanical properties in all directions
  • Post-weld repair or field modification is required
  • Timeline requires rapid iteration without mold investment
Aerospace & Motorsport Grade

Start Your Composite Project

Upload your technical drawings or CAD files and receive a composite manufacturing quote with material and process recommendations within 48 hours.

48h quote response
Aerospace-grade materials
Full laminate documentation
NDA available on request