Request Project Review
01 / Route
Choose Your Project Route
Custom Carbon Fiber Parts

A specific part, drawing, sample or technical requirement — engineered to a reviewed route.

Carbon Fiber OEM & ODM

A branded product program — development, packaging, MOQ and repeat supply.

Consumer Products OEM Sports & Outdoor Equipment OEM
Carbon fiber manufacturing

Custom Carbon Fiber Parts Manufacturing

Case File Trace
FILE OPENED
Custom Carbon Fiber Manufacturing

Custom Carbon Fiber Parts Manufacturing

Bring CAD, drawings, a sample, an existing part or the problem you need the part to solve. NEXWAVE develops the route toward a finished carbon fiber component that fits its assembly, performs its job and can be made again.

Custom carbon fiber component prepared for engineering and manufacturing
PROJECT FILE / OPEN8 CASES ON RECORD
ENGINEERING → DELIVERY
CASE 01 · RECOVERED SPOILER — CASE 02 · 1.15 KG END-EFFECTOR — CASE 03 · R5 HOUSING — CASE 04 · 21 VARIANTS — CASE 05 · 2 MM FENDER — CASE 06 · FENDER SET — CASE 07 · 3/12 HELD — CASE 08 · 0.5 MM E46 — 
STAKES
§01
Before any quotation

What a successful custom-partsproject should protect

S.1The part’s real job.Weight, stiffness, load direction, environment and interfaces must shape the carbon fiber structure instead of being added after the shape is fixed.Load-path engineering for a custom carbon fiber component
S.2The assembly at the other end.Holes, edges, inserts, mounting faces and visible gaps must connect to the real mating condition, not just a good-looking CAD model.Engineered inserts and assembly interfaces in a custom carbon fiber part
S.3The money already committed.Manufacturability and tooling conflicts should be found before they become a finished mold or another failed sample.Composite tooling risk reviewed before manufacturing commitment
S.4The next order.The approved part needs a production reference that captures the geometry, material, tooling, machining, inspection and finish that produced it.Matching carbon fiber parts prepared for repeat production
Where to beginIf one of those points is still uncertain, that is where the project should begin. You do not need to turn incomplete information into a perfect RFQ before asking for help.
§02
Intake & recovery

Start with the part and informationyou actually have

Sometimes the starting point is clean CAD and a released drawing. Sometimes it is an old part, a broken sample, photographs, scan data and several files that disagree with one another. The danger is not that the information is incomplete. The danger is treating every input as equally reliable and building the next tool around the wrong one.

NEXWAVE first clarifies what the part must do and what has already gone wrong. The engineering review then checks five practical areas:

01whether the geometry is complete
02which interfaces control fit
03whether a material or process has already been assumed
04what function the part must perform
05which dimensions or tolerances matter most

That review separates two very different starting states:

■ Route forwardIf the geometry, interfaces and requirements are reliable enough, the part can move into detailed composite DFM and route development.
■ Recovery pathIf critical information is missing or contradictory, the first output is a recovery path. It may call for physical measurement, 3D scanning, CAD reconstruction, a mating part, an interface drawing or an installed check before tooling begins.

Depending on the quoted scope, scanning and measurement may be completed by NEXWAVE or a fixed project partner. NEXWAVE can define the datum plan, review the point cloud or mesh, rebuild surfaces and interfaces, compare the reconstructed geometry with the source part and return controlled STEP data or interface drawings.

Acceptance disciplineA reconstructed model is not accepted just because it looks smooth on screen. Critical features are checked against the original part, scan deviation, mating references, gauges or a first-part assembly as the project requires.
Physical carbon fiber sample reviewed with measurement and CAD inputs
POINT CLOUD → CONTROLLED STEP
CASE 01Anonymous project · verified
Carbon fiber spoiler assessed for geometry reconstruction
STEP + 2D INTERFACE~2 WEEKSMOUNT CONFIRMED

A broken spoiler became a usable engineering starting point

For one anonymous replacement project, the customer had an old spoiler with a broken mounting feature plus photographs. The remaining geometry was scanned, the damaged mount was reconstructed from the symmetrical side, and the mounting relationship was checked before DFM. The customer received STEP data, a 2D interface drawing and mounting confirmation. The recovery took about two weeks for that project.

The useful result was not simply a new file. The next engineering decision was based on a defined mounting relationship instead of copying damage or guessing at the missing feature.

Boundary of recordThe timing belongs to that project and is not a universal reconstruction promise.
LOAD PATH
§03
Component engineering

Engineer the carbon fiber partfor its real job

A metal, plastic or printed part cannot be converted to carbon fiber by copying its outside shape and choosing an attractive weave.

The old geometry may carry load through thick walls, metal ribs or flexible material behavior that does not translate to a laminated composite. If those assumptions remain hidden, the new part can be lighter and still be too soft, weak around a fastener or difficult to validate.

Carbon fiber laminate and core architecture for a custom component
SHAPE COPY · LOAD PATH UNKNOWN

NEXWAVE starts with the job of the component. Depending on the engineering scope, that can include:

E.1organizing load cases, developing the structural concept
E.2defining laminate direction, selecting a core or sandwich construction
E.3adding local reinforcement, designing inserts or bonded interfaces
E.4addressing galvanic isolation and recommending a material and resin direction

Mass estimates, analysis and part-specific testing are added when they are needed and included.

DefinitionThis is where custom carbon fiber fabrication becomes component engineering: the structure, interfaces and validation method are developed together instead of treating carbon fiber as a visual material substitution.
Buyer inputs — cannot be guessedThe buyer still controls the inputs that determine whether the design is solving the right problem. Load magnitude and direction, stiffness or mass target, temperature and chemical exposure, service cycles, impact conditions, mounting interfaces, visible surfaces and product-level approval requirements cannot be guessed. If a missing condition would change the structure, the correct action is to pause that decision and obtain it.
Scope boundaryCustomer-facing engineering output can include revised CAD, 2D interface details, laminate or reinforcement definitions, a BOM, material recommendations, connection details, weight records and a validation plan. Detailed FEA or test reports are supplied when they are part of the agreed engineering service. NEXWAVE can support component design, analysis, sample testing and manufacturing conformity; validation of the complete installed system and any product or regulatory approval remains with the buyer or designated authority.
CASE 02Anonymous project · verified
Structural carbon fiber robotic end-effector assembly
2.4 1.15 KG±0.05 MM CMM10⁶ CYCLES50-PC RELEASE

What this changes in the finished part

The engineering work connects fiber direction, core, local reinforcement and interfaces to the part’s actual load path. That helps avoid a familiar failure: an expensive carbon fiber replacement that looks complete but still creeps, moves at its mounting face or misses the weight target because the old structure was copied instead of re-engineered.

In an anonymous robotic end-effector project, a carbon-filled-nylon print had developed creep and the same-function aluminum route weighed about 2.4 kg. NEXWAVE used the recorded 5 kg and ±50 N load inputs in FEA, selected an autoclave-cured sandwich construction, added local 0° UD reinforcement and CNC-finished the mounting interface. The completed carbon fiber assembly weighed 1.15 kg in the same supplied state. Its interface met the project ±0.05 mm CMM requirement, and one specimen passed the defined 1,000,000-cycle laboratory test before formal release of a 50-piece batch and later repeat orders.

Boundary of recordThose results belong to that component, interface, load definition, construction, test method and approval sequence. They show what a complete engineering-and-verification chain can look like; they are not a general weight-reduction or fatigue-life guarantee.
§04
Composite DFM

Fix manufacturability before it becomesa tool or sample problem

A CAD model can be geometrically complete and still be a poor composite part. A deep wall can trap the tool.
A tight internal corner can make the layup bridge instead of compact.
A trim boundary can be impossible to reach.
A hole or insert can sit too close to an edge for the local structure to carry its load. None of those problems becomes cheaper after the mold is finished.

Composite DFM is where NEXWAVE turns those risks into decisions. The customer-visible output may be an annotated 3D view, marked drawing, issue list, formal DFM report, revised CAD model, tooling concept or open-item register. The format can change with the project, but each useful item should make five things clear:

1the feature that creates the problem;
2the likely manufacturing or part consequence;
3the recommended change;
4any remaining trade-off; and
5who must approve the revision.

The review looks beyond generic injection-molding rules. It considers:

demolding direction & undercutslayup & vacuum-bag accessinternal radii & thickness transitionsbridging & compaction risktrim & machining accessinsert / bond areasinspection reach
Deep carbon fiber housing reviewed for manufacturability
200 MM CAVITY · CORRECTED WHILE EDITABLE
ApprovalWhen the customer owns the design, NEXWAVE can identify and explain the change. When engineering modification is assigned within the project scope, NEXWAVE can revise the model and return the controlled version. In both cases, the customer or designated design authority approves the released geometry before tool or sample work starts.
CASE 03Anonymous project · verified
200 MM CAVITYR1 R5TWO-PART TOOL

A deep housing needed a different tool concept

In an anonymous industrial-housing review, the starting geometry had a cavity roughly 200 mm deep, R1 internal transitions and a one-piece tool concept. NEXWAVE recommended R5 transitions and a two-part tool so the geometry could be laid up and released more reliably. The customer approved the revised CAD before the tool was made.

This is the point of DFM: a problem that existed as a radius and tool decision was corrected while it was still editable. It does show the customer what a useful review should change before money is locked into hardware.

Boundary of recordThe page does not assign a universal radius to every carbon fiber part, because the correct value depends on material form, laminate, thickness, tooling and process.
Split tooling concept for a deep custom carbon fiber housing
21×
§05
Route architecture

Choose the manufacturing architecture forthe part, variants and order

The most advanced-sounding process is not automatically the right process. A flat precision plate with 21 variants, a deep visible shell and a bonded sandwich assembly do not need the same combination of material, forming, tooling, machining and inspection.

NEXWAVE compares the route around the component rather than around a process label. Candidate routes can include prepreg and autoclave curing, compression molding, vacuum-bag and oven processing, VARTM, wet layup with vacuum bagging, cured carbon fiber plate plus CNC and hybrid forming, machining and assembly.

CNC machining a carbon fiber plate component
CURED PLATE + CNC · PLANAR FAMILIES

Cured plate plus CNC is often worth evaluating when the part is predominantly planar, multiple variants share the same material and thickness basis, and hole or profile changes would otherwise require repeated tooling. Forming tooling becomes necessary when the product needs a three-dimensional molded surface, controlled appearance or molded structural features. A prototype tool should not silently become the production tool if its material, stability, surface, life or process compatibility cannot reproduce the accepted part.

For a custom part with complex or changing laminate schedules, large or deeply curved molded geometry, an appearance-critical molded surface, or project-specific internal-state and cure evidence, prepreg + autoclave curing can be a candidate.

Controlled prepreg material, vacuum bagging, a defined heat-pressure-vacuum program and its run record work together to support laminate consolidation, surface condition and the approved manufacturing baseline. NEXWAVE considers the route only after checking the usable work zone for the complete part-and-tool load, drape and layup access, vacuum sealing, tool thermal behavior, the required bag-side surface and project acceptance requirements. That early check helps avoid discovering after tooling or sampling that the load will not fit, the laminate cannot be placed reliably, the bag-side surface is unacceptable or the inspection plan cannot prove the required result. The dedicated Autoclave Curing page covers the full equipment, working-zone, program-control and inspection detail.

The choice changes when any of these conditions changes:

planar / deeply formed / undercutappearance-critical surfacescore · reinforcement · molded interfaceone geometry or variant familyprototype / small batch / repeatdefined tool lifefixture & measured interfacefirst-article proof
Tool reuse checkBefore an existing tool is reused, the review checks the correct vehicle or product version, part state and revision; geometry and locating features; visible surface, flange and seal condition; damage; heating or cooling functions when applicable; historical modification; and the result of any trial part. A tool that cannot reproduce the approved geometry or process state needs repair, modification or replacement.
CASE 04Industrial UAV program · verified
Carbon fiber UAV frame plate variants prepared for CNC production
21 VARIANTS¥500K AVOIDED15 5 MIN~550 PCS/MO

Twenty-one variants did not need twenty-one forming tools

An industrial UAV program contained 21 released frame-plate variants. For a representative 180 × 180 × 2.0 mm, 50-piece configuration, NEXWAVE compared a molding route against autoclave-cured T700 plate plus CNC using the same material, thickness, finish and inspection expectation. The molding concept exposed roughly CNY 500,000 in pre-commitment tooling across the 21 variants. The released plate-plus-CNC route used one controlled program per variant and a dedicated four-part vacuum fixture.

For the representative part, the recorded complete machining cycle changed from 15 to 5 minutes after the dedicated fixture was introduced. The six-month November 2024 to April 2025 record averaged about 550 delivered pieces per month across the 21-variant family. The buyer value was concrete: the product family could be released and repeated without committing to a separate forming tool for every variant.

Boundary of recordThese are project-specific route, tooling, cycle and output records, not a general quotation, machine rate or factory-capacity promise.
The evidence pull

Eight projects, on the record

EVERY CLAIM ON THIS PAGE TRACES TO A NUMBERED PROJECT FILE · PULLED FROM THE STACK BELOW
Broken carbon fiber spoiler used for geometry reconstruction
CASE 01
STEP + 2D · ~2 WEEKS
Broken spoiler → controlled geometry
Carbon fiber robotic end-effector project record
CASE 02
2.4→1.15 KG · ±0.05
End-effector · 10⁶ cycles passed
Deep carbon fiber housing and tooling project record
CASE 03
R1 → R5 · 2-PART TOOL
200 mm cavity fixed pre-tooling
Carbon fiber UAV variant manufacturing project record
CASE 04
¥500K AVOIDED
21 variants · one plate+CNC route
Carbon fiber fender fitment checked against vehicle geometry
CASE 05
2 MM TRACED
Fender mismatch → scan → CNC fix
Finished carbon fiber fender set prepared for delivery
CASE 06
3 HANDOFFS OUT
Finished fender set · crated
Carbon sandwich frame plate under composite integrity inspection
CASE 07
3/12 HELD
C-scan gate · vacuum-bag leak traced
Automotive carbon fiber trim corrected with controlled CNC machining
CASE 08
0.5 MM → CNC
BMW E46 · hand trim eliminated
FIG.06 — THE STACK OPENS · EACH FILE CARRIES ITS OWN NUMBERS AND ITS OWN BOUNDARIES
§07
Datum discipline

Build fitment intodatums, tools and machining

A carbon fiber part can match nominal CAD and still fail at the assembly. The vehicle may have accumulated body variation.
An old source part may have been repaired.
The real mating component may not match the file that arrived with the RFQ. Carbon fiber will not conveniently bend like sheet metal to hide a poor datum decision.

Fitment begins by identifying which source controls the assembly. Depending on the project, that may be the approved 2D drawing and GD&T, released STEP model, source part, mating component, scan, complete vehicle or equipment, gauge or an established production tool. If those sources disagree, NEXWAVE asks the buyer or design authority to resolve the governing condition. Averaging conflicting data would only make the uncertainty harder to find later.

Carbon fiber component fitted against actual vehicle mounting interfaces
MOUNT POINT · VEHICLE-ACTUAL CONDITION

Once the interface is agreed, it is carried through the process:

DATUMinterface definition
TOOLlocation
CNCdrilling fixture
INSERTbond location
VERIFYCMM · gauge · fit

CAD and CMM can be sufficient when the released interface and mating geometry are reliable. Physical verification becomes important when actual build variation, a flexible assembly, prior modification, a visible gap or flush condition, or a vehicle/equipment installation determines acceptance. Depending on scope, the customer can receive CMM or critical-dimension results, gauge findings, fit photographs, an installed check or an approval record.

Why it paysThat reduces the chance that the customer must redrill holes, add shims, trim edges or reject a finished part after international delivery.
CASE 05Anonymous project · verified
Carbon fiber fender aligned to vehicle gap and mounting references
2 MM OUTSCAN CNCGAP CONFIRMED

A two-millimeter mismatch was not solved by forcing the part

During an anonymous automotive-fender project, a mounting point was about 2 mm out when the part was compared with the actual vehicle. The issue was traced to cumulative body variation against the nominal CAD condition. NEXWAVE used scan data to revise the CNC hole position, then confirmed the installation and visible gap on the vehicle.

The solution was not a promise that every carbon fiber part will “bolt on.” It was a controlled way to decide which assembly condition mattered, transfer it into machining and verify it on the actual installation.

Boundary of recordNo “bolt on” promise — a controlled decision chain from assembly condition to machining to verification.
Finished carbon fiber shell surface and edge detail
DELIVERED CONDITION · TRIM / CNC / INSERTS / FINISH / HARDWARE / PACKING
§08
Delivered condition

Receive the finished componentyou agreed to buy

A molded shape is not necessarily a finished component. It may still need trim, CNC holes, countersinks, inserts, bonded details, clear coat, paint, hardware, assembly, inspection, labels and packaging. If those responsibilities are unclear, a quotation can look complete while leaving the buyer with another list of suppliers and another round of handling.

NEXWAVE defines the delivered condition around the physical part. Depending on the project, the supply can connect forming, trimming, CNC work, drilling or countersinking, inserts, bonding, surface finishing, hardware, assembly, inspection, cleaning, protective packaging, labels and selected records. Some work may be completed internally; some may be managed through a qualified project route; and some may remain with the buyer. The quotation must state which is which.

Not administrative detailIt changes what arrives at the customer’s receiving dock and what must happen before the part can enter assembly.
Finished carbon fiber component with included interfaces and hardware
CASE 06Representative automotive project · verified
Finished carbon fiber automotive panels protected for delivery
3 HANDOFFS REMOVED5 MM EPEEXPORT CRATE

A finished automotive-fender set, not two unfinished shells

In one representative automotive project, NEXWAVE supplied a left/right carbon fiber fender pair with molding, trim, CNC holes, required inserts and installation hardware, surface finishing, inspection, cleaning, protective packing and project documents. The customer received the finished pair, hardware, an inspection report and installation instructions.

That delivery removed three downstream handoffs from the customer: separate CNC work, finish correction and hardware sourcing. The parts were protected with 5 mm EPE and CNC-cut foam inserts, packed in separate boxes and placed in an export wooden crate. Pack-state photographs, a hardware list and a shipment weight check helped confirm the contents before dispatch.

Records on selectionInspection, FAI/FAIR, material/batch, CMM, weight, surface, assembly and packing records can be supplied when selected for the project. They are not automatically included in every order. The physical work, records and packaging are agreed together, so “finished part” means the same thing to engineering, purchasing, production and receiving.
HELD
§09
Part-specific inspection

Catch fit, surface and structural problemsbefore delivery

“Strict quality control” does not tell a buyer what will actually stop a bad custom part from shipping. The useful question is simpler: what can make this particular part unusable or unacceptable, and where will that condition be checked? The answer changes with the part.

Q.1Visible molded shellsThe critical combination may include the governing revision, datums and mounting features, trim and hole condition, the approved visible surface and packing protection. Appearance may be judged against an approved sample or boundary sample under a defined light and viewing condition, with project-selected zones, gloss, color or weave direction where needed.Visible carbon fiber shell surface under inspection
Q.2CNC plates & precision interface partsThe inspection may focus on program and revision identity, profile, hole or slot position, edge condition, first-article measurement and the agreed sampling frequency. The record might be a CMM report, dimensional result or FAIR, depending on the order.Dimensional inspection of machined carbon fiber plate features
Q.3Structural parts & assembliesFor parts with inserts, bonded joints, core or local reinforcement, the check can add interface position, bond or insert condition, laminate or core evidence, applicable NDT and project-specific testing. The method is selected because of the failure risk, not because every carbon fiber part needs every available test.Structural inspection of a carbon fiber assembly and its joints
Hold logic — C-scan gate
PROJECT ACCEPTANCE LEVEL < 2% · LOCAL INDICATION 3.5% → HELD
Hold conditionsProduction or shipment is held when a critical dimension fails, the tool condition changes, the surface falls outside the approved reference, an applicable NDT indication exceeds the project rule, an insert or bond is unacceptable, or the packing trial cannot protect the part. The first response is to identify the affected scope, isolate or pause it, repeat the relevant check, complete the necessary engineering and quality review, obtain the required approval and release only the accepted disposition.
CASE 07Anonymous UAV program · verified
3/12 HELD<2% VS 3.5%BAG LEAK TRACED

Three suspect parts were stopped before shipment

On an anonymous UAV sandwich frame-plate project, the project C-scan acceptance level was below 2 percent. Three parts in a 12-piece group showed a local 3.5-percent indication. NEXWAVE traced the problem to a vacuum-bag leak, changed the bag material and vacuum monitoring, remade the three parts and confirmed that the replacements passed the project C-scan requirement.

The customer did not have to discover those parts during assembly or operation. What the case proves is the control logic: the check was tied to the actual sandwich structure, the affected scope was identified, the process cause was corrected and replacement parts were verified before release.

Boundary of recordThe percentages, quantity and corrective action belong only to this project; they are not a general void-rate claim.
Carbon sandwich UAV frame under C-scan inspection
After delivery — evidence firstIf an issue is reported after delivery, the same discipline begins with evidence. Preserve the part and revision identity, photographs, measurement method and results, packaging, transport condition and installation information before assigning cause. That helps separate a manufacturing deviation from transport damage, measurement disagreement or an installation problem, and reduces the chance that either side spends time arguing about the wrong part or condition.
§10
Production reference

Make the next ordermatch the accepted part

An approved sample is useful only if the factory can explain how it was made. If it passed after someone hand-trimmed an edge, added a shim, held it differently in a fixture or touched up a surface, that hidden correction will not automatically appear in the next batch.

NEXWAVE turns the accepted result into a production reference. Depending on the project, that reference can include:

released STEP & drawingBOM · material systemlaminate · core · reinforcementtool & fixture stateCNC programwork instructionsinspection plan & recordstarget weightapproved surface sampleassembly statepacking methodcustomer approval

Any manual correction that made the sample pass must be resolved before repeat release. The change may belong in CAD, the tool, a fixture, the CNC program, a work instruction or the inspection definition. The goal is not more paperwork. It is to make sure the next operator and next order can reproduce the accepted condition without relying on memory.

Controlled CNC correction applied to a formed carbon fiber component
CORRECTION IN THE PROGRAM — NOT IN MEMORY
Change controlChanges are then handled against that reference. A drawing revision, material or supplier change, laminate change, tool repair, fixture update, CNC program or cutter change, adhesive change, surface revision, inspection-method change, restart condition or new customer acceptance basis can trigger an affected-scope review and applicable revalidation. Work in process, stock and future orders stay subject to the resulting disposition until the responsible engineering, quality, production and buyer/design authorities approve release.
CASE 08BMW E46 foot-tray program · verified
0.5 MM BURRTOOL-COMP TRACEDHAND TRIM ELIMINATED

A hand-trimmed edge became a controlled CNC correction

During the BMW E46 carbon fiber foot-tray program, an approximately 0.5 mm edge burr was traced to CNC tool compensation. NEXWAVE corrected the program, remade the part and obtained acceptance. Later batches no longer depended on hand edge trimming.

That small example captures the purpose of a repeat-production baseline. The accepted result was not stored as “make it like last time.” The actual correction moved into the process that produced the next part. This reduces repeated approval work, hidden hand finishing and the risk that a later order drifts away from the sample the customer accepted.

§11
Same part definition

Keep delivery, acceptance and changestied to the same part definition

The engineering and manufacturing solution still needs three concise controls:

1
Delivered scope

What physical work, hardware, finish, assembly, packaging and documents NEXWAVE supplies, and what remains with the buyer.

2
Acceptance and release

The governing revision, critical characteristics, inspection method and frequency, required records, approval authority and conditions for moving forward.

3
Change and issue evidence

How a planned design or process change is approved, and what evidence preserves the identity and condition of a part when an unexpected problem is found.

Planned change ≠ nonconformanceA planned change is not the same as a nonconformance. A planned change modifies an approved design, material, process, tool or inspection basis under control. A nonconformance is a departure from the current approved basis. Both require the applicable review and approval before affected work continues or ships.
PurposeThese controls support the part solution; they are not the purpose of the page. The purpose is to solve the geometry, structure, manufacturability, route, fitment, delivery and repeatability problems that determine whether a custom carbon fiber component succeeds.
§12
Frequently asked questions

Asked before the first file is sent

Yes, for a preliminary review. Photographs with reference dimensions, an existing component or a physical sample can reveal part form, interfaces and likely problem areas. Final geometry, fitment, tolerances and the manufacturing basis still need to be confirmed before tooling or production is approved.

NEXWAVE can review custom components against customer-controlled drawings and confirmed requirements. Project suitability, component testing, documents and approval responsibilities are reviewed separately. Manufacturing support does not equal product certification, type approval or regulatory release.

No. They depend on geometry, material and process route, tooling, quantity, finish, inspection, validation, included delivery work and the information still open. The project quotation should state the applicable figures and the conditions behind them.

Carbon fiber sample, photos and measurements prepared for project review
PHOTOS · SAMPLES · CONFLICTING FILES — ALL ACCEPTED
END OF RECORD — CASE 01 · 02 · 03 · 04 · 05 · 06 · 07 · 08 — FILE YOUR PART — 
Finished custom carbon fiber component ready for engineering review
Open a project file

Bring the part problem,not a perfect RFQ

Send the CAD, drawing, sample, existing part, photographs or failure information you already trust. NEXWAVE will identify what can move forward, what still needs confirmation and which engineering or manufacturing action should address the real part problem first.

Direct line — [email protected]