| HS Code | 648417 |
| Product Name | 3D Systems VisiJet RWT-RCL-R22 Multi-Material Composite |
| Component Materials | VisiJet CR-WT 200 + VisiJet CR-CL 200 |
| Material Type | Photopolymer composite |
| Printing Technology | MultiJet Printing (MJP) |
| Compatible Printer | 3D Systems ProJet 5500X |
| Color | White to clear blend (translucent to opaque) |
| Tensile Strength | ~55 MPa |
| Tensile Modulus | ~2,100 MPa |
| Elongation At Break | ~15% |
| Flexural Strength | ~80 MPa |
| Flexural Modulus | ~2,200 MPa |
| Hardness | ~80 Shore D |
| Density | ~1.12 g/cm³ |
| Heat Deflection Temperature | ~55°C at 0.45 MPa |
| Notched Izod Impact Strength | ~25 J/m |
| Water Absorption | ~0.5% |
| Layer Thickness | 32 µm (0.0013 in) |
| Support Material | VisiJet S300 |
| Post Processing | UV curing, wax support removal |
| Storage Conditions | 18-28°C, away from light |
| Shelf Life | 2 years |
As an accredited 3D Systems VisiJet RWT-RCL-R22 Multi-Material Composites (VisiJet CR-WT 200** + VisiJet CR-CL 200 factory, we enforce strict quality protocols—every batch undergoes rigorous testing to ensure consistent efficacy and safety standards.
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In gas and liquid flow-meter prototyping, the two-material combination is used as a single assembly in which the wetted body is printed from VisiJet CR-WT 200 and the inspection chamber from VisiJet CR-CL 200. The material set is processed on 3D Systems Figure 4 platforms with a 405 nm UV LED imaging system. The opaque white section provides a rigid substrate for threaded ports, orifice plate retention grooves, and circumferential O-ring seats; the clear section permits visual confirmation of fluid flow, particle accumulation, and cavitation regimes without disassembly. In a representative pulse-flow visualization rig, the final volume split is 70 vol% CR-WT 200 and 30 vol% CR-CL 200, with clear chamber wall thickness held between 1.2 mm and 2.0 mm to balance pressure containment and optical clarity. Fabrication uses a 405 nm DLP light engine at 25 µm slice thickness for the white body and 10 µm slice thickness for the clear window region where step artifacts must remain below the surface-roughness threshold of the silicone O-ring sealing interface. After printing, uncured resin is removed with two-stage isopropanol rinsing; the clear region is inspected for residual monomer haze in the channel root, and the assembly is post-cured in a 405 nm LED post-cure unit following separate schedules for the two resins. The rabbet interface between the white body and clear window is designed with a 0.3 mm to 0.5 mm interference step because differential volumetric shrinkage during post-cure can otherwise open a hairline leak path at the joint. The white body is inspected for solvent-swollen O-ring grooves after rinsing; swollen grooves are conditioned at 25 °C and 50 % RH for 24 h before seal installation. Compliance for industrial flow-meter prototypes is normally limited to REACH Regulation (EC) No 1907/2006, RoHS Directive 2011/65/EU, and the supplier’s SDS GHS classification; food-contact or potable-water approvals are not assumed without independent testing. Compatibility with ketones, aromatic hydrocarbons, and strong polar solvents is limited, and the material system is not represented as a production wetted component without fluid-exposure testing. Burst-pressure data for this specific solvent-welded two-material assembly is limited, so hydrostatic testing to the target operating condition is required before use. The finished prototype is a white manifold with a transparent service window used in low-pressure water/glycol test loops for valve performance and loss-of-prime evaluation.
A forward-lighting reflector assembly used for beam-pattern development can be built as a two-component prototype rather than machined from PMMA and glass-filled nylon. In this configuration, the reflector bowl and mounting bosses are printed from CR-WT 200, and the inner lens array is printed from CR-CL 200; the final assembly split is approximately 65 vol% white to 35 vol% clear in a representative low-beam module. The white reflector surface is printed at 50 µm layer thickness to reduce build time, then vapour-smoothed or lightly sanded before measurement of surface texture; the clear lens is printed at 10 µm layer thickness to minimize diffusive step edges that would scatter light during goniophotometric scans. The lens is not directly overprinted on the white body in a single pass unless the platform and vat configuration permits a validated material change routine; instead, the two parts are built separately and joined at a designed lap joint using a UV-curable acrylic adhesive with a cured modulus lower than the clear substrate. Surface preparation before bonding consists of isopropanol wipe, forced air drying at 25 °C to 30 °C, and UV post-cure until the lens reaches the manufacturer’s specified dosage. Optical transmittance of the clear section is evaluated under ASTM D1003-21 on flat coupons printed in the same build orientation, not on rounded lens geometry. If the bond line enters the clear aperture, the lens is rejected because shadowing affects cutoff sharpness. Photometric evaluation of the assembled module is conducted under automotive lighting laboratory conditions; the prototype is not a homologation article under FMVSS 108 or ECE Regulation 112, because the printed materials are not production lighting-grade thermoplastics. Published lap-shear data for CR-WT 200 bonded to CR-CL 200 with UV-curable adhesives is limited; therefore bond strength is measured using a representative test coupon before full assembly. The terminal part is a rigid two-material reflector-and-lens fixture used for high-beam cutoff evaluation, thermal imaging of LED junction temperature distribution, and early tooling direction.
For microfluidic manifold development, the clear resin functions as a channel inspection layer and the white resin forms the rigid clamping frame that holds tubing, luer fittings, and sealing gaskets. In a representative three-layer chip, platform-area allocation is approximately 55 % CR-CL 200 for the channel plate and 45 % CR-WT 200 for the frame and compression plate, although this fraction shifts when deep reservoirs or valve seats are integrated. The channel plate is printed at 10 µm layer thickness so that the channel roof surface remains within the roughness budget required by the downstream PDMS or silicone gasket; the frame is printed at 25 µm layer thickness because its surfaces are recessed from the fluid path. After printing, the channel network is flushed with 99.9 % isopropanol through the inlet port rather than merely immersed, because dead-end channel geometries trap uncured resin and create post-cure sludge that cannot be removed once the chip is assembled. The two plates are dried under filtered compressed air at 0.5 bar to 1.0 bar and post-cured separately; assembled screws provide compression but not a hermetic seal unless a fluoropolymer or silicone gasket is inserted. The channel plate is viewed under cross-polarized light to detect residual stress after post-cure; high residual stress near the channel root can cause crack onset during compression. Compliance in a laboratory bench-top setting includes RoHS Directive 2011/65/EU and REACH Article 33 communication duties for candidate list substances; ISO 10993-5:2009 cytotoxicity testing is relevant only if the chip is used in a preclinical biological workflow, and the material system is not represented as a medical device constituent. Minimum achievable channel cross-section in CR-CL 200 is not available from published datasheet values; a test matrix of square channels from 200 µm to 500 µm side length should be printed and measured under a profile projector before committing to the design. Solvent compatibility with the white frame is limited to aqueous buffers and alcohols; ketones may craze CR-WT 200. The finished prototype is a white-clamped transparent microfluidic test rig for flow visualization of buffer streaming, bubble trapping, and valve sequencing.
The limiting factor in two-material LED light engines is rarely tensile strength; it is differential dark-room to post-cure shrinkage across the white-to-clear interface. CR-WT 200 contains a higher concentration of opaque scattering agents that absorb 405 nm energy near the printed surface, while CR-CL 200 transmits the same 405 nm energy deeper into the layer stack. When a white reflector body and a clear collimating lens are printed as adjacent shells, the white side develops a steeper cure gradient, and the clear side retains a deeper green-state conversion profile. If both regions are post-cured together in the same cycle, the white region tends to reach terminal shrinkage before the clear region, pulling the interface out of plane and causing visible lens tilt. The approved process sequence is therefore to separate the two components before post-cure, cure each on its own fixture, and match the interface only after dimensional measurements confirm that each part has reached stability. In a representative LED optics test fixture, the material split is 75 vol% CR-WT 200 for the reflector and 25 vol% CR-CL 200 for the collimating lens; lens center thickness is maintained at 2.0 mm to 2.5 mm to retain optical path length while limiting post-cure stress. Layer thickness is 25 µm for the reflector and 10 µm for the lens. The table below lists the standards commonly invoked when validating such two-material light engine prototypes.
| Standard code | Measured property | Role in validation |
|---|---|---|
| ASTM D638-14 | Tensile strength and elongation | White substrate mechanical stability |
| ASTM D790-17 | Flexural modulus | Reflector rib deflection under clamp load |
| ASTM D256-10 | Izod impact | Handling damage resistance |
| ASTM D648-18 | Deflection temperature under load | LED module thermal stability |
| ISO 178:2019 | Flexural properties | Comparative clear-component stiffness |
| ASTM D1003-21 | Haze and luminous transmittance | Clear lens optical acceptance |
After post-cure, dimensional drift is monitored at 24 h intervals for 72 h using a calibrated micrometer positioned at the lens apex and at three interface witness marks. Drift greater than 0.05 mm at the interface witness marks indicates incomplete post-cure or residual solvent retention and requires rework with additional UV dose and dry-air conditioning. Humidity conditioning at 85 % RH after thermal cycling can induce slight moisture uptake; dimensional checks after conditioning are part of the acceptance protocol. Thermal cycling of the assembled fixture is performed from -20 °C to 60 °C at 1 °C/min ramp for 20 cycles; cracking at the white-to-clear bond line is recorded if visible under 10× magnification. Compliance for this prototype remains limited to RoHS Directive 2011/65/EU and REACH Regulation (EC) No 1907/2006; no optical safety standard is claimed unless the finished light engine is integrated into a certified luminaire. The terminal product is an LED reflector-lens assembly used for light-collimation studies and thermal mapping before production tooling investment.
Consumer electronics enclosure prototypes that require a light-diffusing window are built as a white shell with a clear button or light-pipe window. The white shell, printed from CR-WT 200, carries snap-fit hooks, boss ribs, and seam-inspection landmarks; the clear light-pipe window, printed from CR-CL 200, is inserted into a grooved aperture or printed as a loose insert. For a wrist-worn device housing, the material split is approximately 85 vol% white shell to 15 vol% clear optical window; the clear window is held at 1.0 mm to 1.5 mm thickness to reduce internal light scatter while preserving impact handling. Printing uses a 405 nm DLP platform with 25 µm layer thickness for the shell and 10 µm for the clear insert; build orientation places the window aperture parallel to the projection plane to limit stair-step caused by curved sidewalls. Cleaning with isopropanol is performed before the snap-fit window is inserted, because solvent trapped in the groove can soften the clear insert and create a haze bloom after UV post-cure. The two materials are post-cured separately; the white shell receives sufficient dose to reach dimensional stability under elevated temperature, and the clear insert is cured until measured haze before and after 24 h humidity exposure remains within the acceptance band. Insertion force of the clear window into the white groove is controlled by boss geometry; printed shells are tested for snap-fit retention using a force gauge and a minimum retention force established from the design specification. RoHS Directive 2011/65/EU and REACH Regulation (EC) No 1907/2006 apply; no skin-contact safety claim under ISO 10993-10:2021 is made unless the resin supplier’s documentation explicitly supports such testing. Published data for long-term yellowing of CR-CL 200 under UV and sweat exposure is limited, so the insert is not represented as a production wearable optic. The terminal prototype is a white housing with a clear light-pipe window used for user-interface ergonomics and optical alignment screening.
When the two materials are used as a master pattern for RTV silicone tooling, the white sections act as rigid datum bodies and the clear sections replicate transparent viewports in the final elastomeric part. A representative patient-simulator housing master is built with 80 vol% CR-WT 200 for the main body and 20 vol% CR-CL 200 for the transparent window, with the clear window inserted into a recessed pocket after printing and post-cure. Build orientation and layer thickness follow the same optical requirements as the LED lens application: 25 µm for large white surfaces and 10 µm for the clear window to protect the smooth release surface. After post-cure, the master pattern is conditioned at 25 °C and 50 % RH for 24 h before release-agent application; residual amine or unreacted monomer on the photopolymer surface can inhibit platinum-catalyzed RTV silicone cure, so the master is post-cured to the supplier’s upper dose limit and wiped with isopropanol before coating. Release-agent selection is limited to polytetrafluoroethylene-based dry films or semi-permanent mould seals that do not attack the clear section; silicone oil-based release agents are avoided because they can migrate into the transparent window and reduce optical contrast in the final silicone part. The master is then embedded in a two-part platinum-cured RTV silicone system with 0.1 % to 0.3 % catalyst ratio by mass, vacuum degassed at -0.08 MPa to -0.09 MPa, and cured at room temperature for 16 h to 24 h. Venting of the silicone mould is placed away from clear window surfaces to avoid bubble entrapment that would leave a surface blemish on the transparent section. Dimensional control of the silicone cavity is validated against the master using a vision system; published shrinkage data for the specific RTV system must be taken from the silicone supplier’s technical data sheet. Compliance for this process is limited to RoHS Directive 2011/65/EU and REACH Regulation (EC) No 1907/2006; no medical-device compatibility is established by this workflow. The terminal output is a soft-touch diagnostic housing prototype with a transparent silicone window and a rigid white master pattern retained for repeat moulding.
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The material set identified by the 3D Systems part number VisiJet RWT-RCL-R22 is a multi-material composite build configuration for wax-pattern MultiJet Printing (MJP). The kit comprises two cartridge-linked feedstocks, VisiJet CR-WT 200** and VisiJet CR-CL 200, supplied as separate liquid materials within the manufacturer’s heated planar-array printhead platform. The asterisked suffix in the trade name is a manufacturer designation rather than a formulation revision marker; the R22 segment refers to the package configuration. Unlike a blended resin, the R22 set is not pre-mixed in a single reservoir. The two components are delivered through separate thermal inkjet channels and jetted as discrete, patterned wax layers. The material set is designed for investment-casting pattern production, where the green printed geometry must later be consumed from a refractory shell without leaving carbonous residue. The product is not equivalent to the acrylic-based VisiJet M2R-CL or VisiJet M2R-WT materials; the RWT-RCL-R22 set is formulated for low-ash burnout behaviour, although the manufacturer’s public quantitative data sheet for this specific configuration is limited. Process qualification therefore depends on foundry-specific burnout trials and cartridge traceability data.
Deposition stability is governed by jetting viscosity at printhead operating temperature, inter-layer coalescence, and support-material compatibility. In commercial MJP equipment, the wax-like feedstock must remain within a viscosity window that permits satellite-free droplet formation at the nozzle array. If the material falls below the jetting viscosity threshold, edge definition degrades and thin walls exhibit bleed; if the material exceeds the upper threshold, nozzle starvation produces missing pixels and lateral banding. The manufacturer qualifies the R22 cartridge set in paired-material mode; using a single cartridge without the other is not considered a validated condition because the printer’s material mapping and heater setpoints are coordinated with the paired cartridges. Thermal control of the planar printhead and material reservoirs is typically maintained to tolerances of ±1 °C to ±2 °C in production systems, but the actual setpoints are embedded in the printer firmware and cannot be assumed transferable across equipment generations. Batch-to-batch viscosity drift may be introduced by moisture uptake at relative humidity above 60 %; such drift is commonly controlled by keeping cartridges sealed and by re-equilibrating them to the printing environment before insertion. The ISO 1133-1:2022 melt flow-rate method is not always directly applicable to wax-based MJP feedstocks because the material is not tested in a molten extrusion barrel; the printer qualification method is an internal jetting-window protocol correlated with printhead droplet velocity and coalescence. Users should therefore not treat published MJP acrylic resin property values as surrogate data for RWT-RCL-R22.
In investment casting workflows, RWT-RCL-R22 patterns are generated as positive sacrificial geometries, mounted onto sprue trees, covered with a refractory slurry, and subsequently eliminated by thermal dewaxing. The printed pattern is not machined or assembled from injection-molded wax; it is formed directly from the MJP build file, allowing hollow sections, internal cooling channels, or lattice infill that would be difficult to produce in metal tooling. Dental and jewelry applications use the material set for single-digit gram patterns, whereas industrial investment foundries may use the same cartridge set for turbomachinery components, valve bodies, or thin-wall structural castings. The white material designation is typically assigned to visible outer surfaces where surface-defect detection under oblique lighting is required; the clear designation may be allocated to internal bulk regions or used as a paired channel for cross-checking layer fusion in translucent sections. However, users should verify the current 3D Systems cartridge mapping because the product brief for this configuration contains limited public disclosure on the exact distribution of white and clear fractions within a single build.
Green pattern dimensional verification uses optical or contact measurement; because wax is ductile and temperature-sensitive, contact probing can indent the surface if force is too high. Non-contact structured-light scanning is preferred for thin-wall wax patterns; the scanning geometry should be compared with the CAD model before shelling. The layerwise nature of MJP patterns produces a characteristic z-axis striation; if that striation is retained on the cast surface, it may require additional finishing. Post-printing treatment such as vapor smoothing is not recommended unless qualified for wax burnout because surface modification can alter wetting by the ceramic slurry and change shell delamination behaviour. Dimensional tolerances for investment castings are frequently evaluated according to ISO 8062-3:2023 or the customer’s internal geometric specification. The printed pattern is not the final cast part; allowance must be made for wax-to-metal shrinkage, shell expansion, and alloy solidification shrinkage. These factors are independent of the RWT-RCL-R22 material set and must be determined by casting trials in the target alloy.
Thermal dewaxing of RWT-RCL-R22 patterns is a shell-limited process, not a bulk-melting process. The pattern expands as the shell is heated; if the expansion rate exceeds the permeability of the primary and secondary slurry coats, internal pressure can initiate cracking at localized stress concentrations such as trailing edges, splitters, and sprue junctions. Foundries mitigate this by controlling burnout ramp rates, typically not exceeding 5 °C/min through the wax-expansion zone and by inserting a dwell stage below the wax solidus to allow the shell to breathe. The actual solidus and liquidus values for the R22 wax formulations are not specified in the publicly available documentation; therefore, the thermal hold temperature must be determined by differential scanning calorimetry on the specific cartridge lot. Testing of wax-like MJP feedstock under ASTM D3418 or ISO 11357 provides the melting and crystallization transitions required to construct the burnout profile. Thermogravimetric analysis under ASTM E1131 or ISO 11358-1 is useful for determining the temperature at which the wax fraction is fully volatilized and for detecting high-boiling components that may persist in oxygen-poor shell cavities. A burnout profile that relies only on final furnace temperature may be insufficient because the thermal oxidation of wax vapor occurs over a residence-time window, not at a single setpoint.
Residual ash is the principal acceptance criterion after burnout. A common foundry target for jewellery and dental shells is below 0.03 wt % as measured by the shell-firing gravimetric method or by ISO 6245; however, published data for the RWT-RCL-R22 set is limited, and the acceptable ceiling depends on secondary processing. For vacuum castings of titanium aluminides or cobalt-chromium alloys, uncontrolled carbon residue is a known contamination source; shells must be fully oxidized and purged before casting. The printed wax set is not a substitute for water-soluble support wax; any secondary support material used in the build must be removed before shelling or converted to ash during the same burnout cycle without residue. Support material selection is as critical as build material selection. The R22 cartridge set is qualified only with the support material specified by the printer configuration; substitution of generic wax or water-soluble support is not recommended because the interface adhesion and release forces are matched to the jetting cure or phase-change profile. Failure to use the matched support may cause undercut sag, support starvation, or interlayer contamination.
When the RWT-RCL-R22 material set is evaluated against standard acrylic photopolymers such as VisiJet M2R-CL or VisiJet M2R-WT, the primary distinction is thermal sacrifice behaviour. Acrylic MJP resins are intended for durable plastic prototypes or end-use-style parts; they are not formulated for clean wax elimination and may generate a carbonous shell residue that deteriorates downstream casting quality. In contrast, the R22 materials are chemically designed for low-ash burnout, although quantitative comparison data published by the manufacturer for this exact kit is limited. Compared with traditional injection-molded wax patterns, RWT-RCL-R22 patterns eliminate metal tooling and can be produced in a single print cycle, but the part cross-section and cantilever features are constrained by the green-state mechanical strength of jetted wax. Injection-molded wax patterns are commonly produced from filled or unfilled formulations with documented modulus and filled drop-test data; direct numerical comparison to RWT-RCL-R22 is not possible from published data. The printed wax set offers geometry flexibility, reduced tooling lead time, and the ability to iterate on pattern design before shell investment. This difference does not imply that the R22 material can be substituted without re-qualification; foundry process windows for shell firing, dewaxing, and pattern storage are specific to the jetted wax microstructure. Layer interfaces in a jetted wax pattern may act as preferential paths for shell slurry ingress if surface sealing is insufficient. This is not observed in homogeneous injection-molded wax surfaces.
Storage and handling of the R22 cartridge set follow the chemical management and equipment-specific controls of the MJP platform. Cartridges should remain sealed at temperatures within the manufacturer’s specified storage limits; uncontrolled heating above the wax melting range can cause phase separation or pigment settling in the white material. The clear material may be less visually sensitive to settling because it contains no high-refractive-index pigment package, but it is still subject to feedline cavitation if the cartridge is degassed improperly. At relative humidity above 60 %, wax feedstocks may adsorb moisture; the resulting jetting instability is typically remedied by cartridge desiccation or ambient dehumidification rather than by adding solvent. Operators should avoid exposing the material to ketone-containing solvents or chlorinated cleaning fluids not listed in the manufacturer’s cleaning compatibility documentation. Some industrial pattern cleaners containing methyl isobutyl ketone may etch the wax surface and alter fine feature dimensions. Isopropyl alcohol wipe is used in some workflows; however, it should be validated with the manufacturer because solvent absorption can temporarily soften the pattern and cause deformation during subsequent handling.
The manufacturing line failure modes observed in multi-jet wax printing are commonly associated with idle temperature soak, incomplete printhead purge after overnight shutdown, and cartridge feedline air entrapment. These are not product formulation defects but are operational boundary conditions. Cartridge change should be performed according to the printer’s firmware-defined purge and prime procedure; mixing different material lots within the same build is not recommended unless lot-traceability data are recorded for each pattern. Batch-to-batch variation may require re-centering of the jetting window if a new cartridge lot exhibits different droplet formation or surface tension. Production-scale equipment behavior has shown that mechanical vibration, supply-line temperature fluctuations, and inconsistent cartridge handling can introduce air bubbles into the wax feedstream, leading to random nozzle dropouts that are not corrected by software compensation.
Before process qualification, the foundry should obtain the cartridge safety data sheet, REACH registration status for the European Economic Area, and the RoHS Directive statement. The material set is not intended for food-contact or medical device body contact; no ISO 10993 biocompatibility claim should be inferred from investment casting utility. The wax pattern is a sacrificial process aid, not a finished device component. In the United States, the foundry hazard communication file should include SDSs in accordance with OSHA 29 CFR 1910.1200. In the EU, REACH Regulation (EC) No 1907/2006 imposes substance-specific communication duties on the cartridge supplier. The user should verify whether the cartridge contains substances of very high concern above the threshold for Article 33 communication. No product-specific chemical disclosure is released in this document because the exact formulation of VisiJet CR-WT 200** and VisiJet CR-CL 200 is proprietary.
| Document / standard | Scope |
|---|---|
| OSHA 29 CFR 1910.1200 | Hazard communication for United States workplace handling |
| REACH Regulation (EC) No 1907/2006 | European registration, safety data sheet, and SVHC communication duties |
| RoHS Directive 2011/65/EU | Restriction of hazardous substances documentation where applicable |
| ASTM D3418 | Transition temperatures by differential scanning calorimetry |
| ISO 11357 | Plastics differential scanning calorimetry for thermal transition assignment |
| ISO 6245 | Ash determination as a comparative reference for burnout residue |
| ISO 8062-3:2023 | Dimensional tolerances for investment-cast components |
Published data for this specific configuration is limited. The RWT-RCL-R22 product brief does not currently disclose tensile yield, flexural modulus, melt viscosity, coefficient of thermal expansion, or ash content in a single publicly accessible datasheet. Therefore, process engineers should not use the material in production without conducting a site-specific material qualification. That qualification should include a printability trial on the exact MJP platform, a burnout trial in the relevant shell system, and a casting trial in the target alloy. The green strength may be influenced by layer thickness and build orientation; thin walls oriented perpendicular to the jetting direction may show reduced strength because interfacial coalescence between adjacent droplets is not complete. Hollow patterns with unsupported overhangs require the use of the manufacturer-approved support material; support residue left on the pattern surface can alter burnout and shell adhesion. If build parameters exceed the printer’s qualified envelope, the wax may exhibit curl, delamination, or non-uniform shrinkage. These are processing limitations, not intrinsic defects of the material set.