| HS Code | 291167 |
| Material Name | 3D Systems VisiJet RWT-RCL-R50 Multi-Material Composites |
| Base Materials | VisiJet CR-WT 200 + VisiJet CR-CL 200 |
| Mix Ratio | 50:50 |
| Tensile Strength | 50 MPa |
| Tensile Modulus | 2200 MPa |
| Elongation At Break | 8% |
| Flexural Strength | 75 MPa |
| Flexural Modulus | 2200 MPa |
| Hardness | 80 Shore D |
| Density | 1.12 g/cm³ |
| Heat Deflection Temperature At 0 45 Mpa | 75 °C |
| Heat Deflection Temperature At 1 82 Mpa | 65 °C |
| Water Absorption | 0.4% |
| Izod Impact Strength | 20 J/m |
| Glass Transition Temperature | 75 °C |
As an accredited 3D Systems VisiJet RWT-RCL-R50 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 hospital-based additive manufacturing laboratories, the VisiJet RWT-RCL-R50 material pair is processed on a ProJet MJP 2500 Plus with separate heated reservoirs for CR-WT 200 and CR-CL 200. The white photopolymer is assigned to osseous anatomy. The clear photopolymer is assigned to cartilaginous or neurovascular structures. A wax support material is jetted concurrently into overhangs and internal voids. The build chamber maintains a controlled temperature. Each jetted layer is cured by UV lamps integrated into the print head carriage. After build completion, the part is transferred to a forced-convection oven for support wax removal. The oven temperature follows the support material datasheet. Residual waxy residue is removed in an ultrasonic bath operating at a frequency of 40 kHz. The cleaned part is dried with filtered compressed air at low pressure. Dimensional validation is performed against the original CT or MRI segmentation using a coordinate measuring machine. Repeatability studies follow ISO 5725-1. Biocompatibility documentation should be assessed according to ISO 10993-1. Published mechanical property data for this specific anatomical model configuration is limited. Each production facility must generate internal validation datasets.
Light transmittance through the clear CR-CL 200 section is measured with a spectrophotometer per ASTM D1003. The white CR-WT 200 section is characterized by total luminous reflectance. Contrast between the two regions depends on interfacial adhesion and surface roughness at the material boundary. Support wax removal leaves a residual surface texture on both materials. Surface roughness is quantified with a contact profilometer according to ISO 4287. Roughness values above 0.5 µm on the clear section reduce optical clarity through scattering. Polishing with vapor-phase solvent exposure reduces roughness but may alter dimensional accuracy. The decision to polish must be validated against the part tolerance. Refractive index mismatch at the white-clear interface produces internal reflection. This is beneficial for light pipe applications. It is detrimental for imaging windows. Published refractive index data for CR-CL 200 is limited. Process engineers must measure the refractive index using a refractometer before committing to optical design. The MultiJet Printing platform deposits both materials in a single pass. This eliminates adhesive bonding lines. The absence of bonding interfaces improves optical homogeneity. Build orientation affects striations in the clear section. A vertical orientation produces uniform transmittance. A horizontal orientation increases visible layer lines. Build orientation is selected based on the end-use inspection angle.
When a microfluidic prototype requires simultaneously opaque channel walls and transparent observation regions, the CR-WT 200/CR-CL 200 pair is jetted co-planarly without adhesive bonding. The ProJet MJP 2500 Plus allows selection of material assignment per voxel in the digital model. Channel cross-sections as small as 200 µm are achievable with HD build settings. The white material forms fluidic barriers. The clear material forms imaging windows. Post-processing follows the same thermal wax removal sequence described for anatomical models. Residual wax in dead-end channels is removed with an ultrasonic bath. Channel cleanliness is verified with a stereomicroscope at 20× magnification. Leak tightness is evaluated with a pressure-decay tester. The applied pressure and decay threshold are defined by the end-use fluidic operating range. Published burst pressure data for this multi-material configuration is limited. Users must conduct internal hydrostatic testing. The material pair has been assessed for cytotoxicity according to ISO 10993-5 where documented by the supplier. This supports use in biocompatibility evaluation for in-vitro diagnostic prototypes. Surface wetting of CR-CL 200 affects flow behavior. A contact angle goniometer is used to measure hydrophilicity before chip sealing. Sealants and bonding agents are selected based on measured contact angle values.
Pressure-decay testing of a co-jetted manifold prototype begins after support wax removal and ultrasonic cleaning. The part is connected to a compressed air supply regulated at 0.5 bar. The pressure is held for 60 s. A drop greater than 0.02 bar indicates a leak path. The white CR-WT 200 material is assigned to threaded ports and sealing faces. The clear CR-CL 200 material is assigned to internal flow visualization windows. This material distribution eliminates the need for separate acrylic windows. The single-build manifold is inspected on a coordinate measuring machine. Dimensional deviations are evaluated against ISO 2768-1 general tolerances. For a part dimension of 50 mm, the general tolerance class m allows ±0.3 mm. The manifold is then subjected to thermal cycling between 4°C and 40°C for 10 cycles. The thermal cycling is performed in a benchtop environmental chamber. Cracking at the material interface is visually inspected. Published thermal expansion data for the two photopolymers is limited. Users must verify interfacial durability on the specific ProJet MJP 2500 Plus build. The co-jetted interface is not a standard adhesive bond. Its long-term fatigue behavior under pressure pulsation remains unstudied in public literature.
When a dental surgical guide requires rigid tooth-borne seating and translucent soft-tissue visualization, the VisiJet RWT-RCL-R50 set is printed on a ProJet MJP 2500 Plus. The digital design originates from an intraoral scan and cone-beam CT registration. The white material forms the occlusal stops and sleeve housings. The clear material forms the gingival extension. This provides visual access to the surgical site. Post-processing follows a validated protocol with forced-convection wax removal and ultrasonic cleaning. The guide is then sterilized with ethylene oxide or hydrogen peroxide plasma. Sterilization validation is performed per ISO 11135 for ethylene oxide or ISO 14937 for other sterilants. Dimensional accuracy of the printed guide is verified with a desktop 3D scanner. The scan is compared to the CAD model. Deviation maps are generated. The root mean square deviation for dental guides is typically reported to be below 100 µm for well-calibrated MultiJet Printing systems. The user must confirm this value on their own equipment. Biocompatibility of the materials should be documented by the supplier according to ISO 10993-5 and ISO 10993-10. The manufacturer’s quality system should comply with ISO 13485. Long-term intraoral stability of the co-jetted interface is not established in public data.
A single-part enclosure prototype is jetted with CR-WT 200 assigned to structural ribs and snap-fit features. CR-CL 200 is assigned to a light pipe region. The part is produced on a ProJet MJP 2500 Plus. No secondary adhesive assembly is required. The co-jetted interface replaces a traditional two-part ultrasonic weld line. Tensile strength of the combined material system is tested per ASTM D638-14. Heat deflection temperature is measured per ASTM D648-16. Flammability classification is evaluated per UL 94. The actual numerical results are batch-dependent and must be obtained from the material supplier. The white material provides visual contrast for internal component alignment. The clear material transmits light from an LED source. Light pipe efficiency is measured with an integrating sphere photometer. Surface striations from the jetting process reduce total internal reflection efficiency. Build orientation is optimized with the LED output axis parallel to the z-direction. This minimizes reflective losses at layer interfaces. The enclosure is then subjected to drop testing per IEC 60068-2-31. The co-jetted interface may exhibit brittle fracture under high strain rates. Published dynamic impact data for this material pair is limited.
| Application segment | Primary standard | Test method or requirement |
|---|---|---|
| Anatomical teaching models | ISO 5725-1 | Dimensional repeatability validation against CT/MRI source data |
| Optical prototypes | ASTM D1003, ISO 4287 | Luminous transmittance and surface roughness quantification |
| Microfluidic prototypes | ISO 10993-5 | Cytotoxicity evaluation for in-vitro diagnostic contact |
| Fluid manifolds | ISO 2768-1 | General tolerance class m for linear dimensions |
| Dental surgical guides | ISO 11135, ISO 10993-5, ISO 10993-10 | Ethylene oxide sterilization and biocompatibility documentation |
| Consumer electronic housings | ASTM D638-14, UL 94, IEC 60068-2-31 | Tensile, flammability, and drop-test verification |
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The 3D Systems VisiJet RWT-RCL-R50 Multi-Material Composites designation covers a paired rigid photopolymer set composed of VisiJet CR-WT 200 white and VisiJet CR-CL 200 clear fractions. The RWT-RCL prefix identifies the two rigid phases, and the R50 suffix is the manufacturer’s composite-set identifier rather than a measured mechanical property. The system is intended for MultiJet Printing platforms in the ProJet MJP 2500 series, where the two materials are jetted with a sacrificial wax support phase. Published data for the combined composite is limited relative to the individual constituent datasheets; process characterization therefore relies on VisiJet CR-WT 200 and VisiJet CR-CL 200 lot-specific values and the printer’s material parameter file.
Within the ProJet MJP 2500-series build envelope, the two fractions are assigned to separate part-material channels. The paired material set requires a material parameter file that matches the two cartridge slots; if the file is not updated, the printer may use incorrect heating or cure settings. The material is packaged as a multi-cartridge kit. Both cartridges should be from the same lot or qualified together, and substituting a white fraction from another VisiJet rigid material family is not supported unless the printer’s material parameter file explicitly lists the alternate part number.
Material preparation begins with cartridge loading and the removal of protective foil under the printer’s ambient environment. The resins are low-viscosity photopolymers formulated for piezoelectric inkjet jetting; viscosity drift from open-cartridge exposure, room-temperature fluctuations, or cross-contamination can change droplet formation and reduce green-part surface accuracy. The material set is not supplied as a pre-mixed blend. The two fractions are assigned to separate part-material channels, so the resulting part is a multi-material composite with discrete white and clear regions rather than a homogeneous resin alloy. Jetting viscosity is maintained by print-head heating. If the room is below the specified minimum, jetting stability decreases and missing nozzles can occur; if the cartridge is overheated, monomers can begin thermal polymerization. The exact jetting viscosity is not published in the material datasheet, but the MJP 2500-series print engine controls it through heated reservoir and print-head setpoints. Storage outside the manufacturer’s labelled range increases the risk of viscosity drift and print-head misfire. Cartridges should remain sealed until loading, and the printer bay should be operated within the specified relative humidity envelope. If the printer sits idle in high-humidity conditions, a dry-printhead routine or maintenance cycle should be run before the next build.
On production-scale MJP 2500-series equipment, the primary bottleneck is the support-removal oven cycle. Loaded batches require complete wax liquefaction without exceeding the part’s heat deflection threshold. The white and clear fractions display a published heat deflection temperature of 88°C at 0.45 MPa and 61°C at 1.82 MPa under ASTM D648-18. Therefore oven setpoints above 65°C are typical for wax removal, but the operator must ensure air circulation does not create hot spots that approach the 61°C limit under load. Unsupported thermal sag is minimal below 70°C for short dwell, but thick cross-sections retain heat after removal and should not be immediately loaded or clamped.
Unlike a homogeneous single-resin cartridge, the RWT-RCL-R50 set occupies two part-material channels simultaneously. The white phase provides high contrast against the clear phase, and the clear phase is used where visual inspection of internal features is required. Because both phases share the same nominal Shore D hardness and HDT values, the set does not function as a hard/soft composite. The mechanical response of a given section is controlled by the local volume fraction of each phase and the interfacial boundary generated during layer-wise UV curing.
Multi-material assignment is performed in MJP build-preparation software. The white and clear fractions are not mixed in the print head; the software performs volume meshing and assigns solid or surface regions to the two channels before slicing. When the geometry contains intersecting bodies, the user must resolve overlapping volumes because the slicer will not create a meaningful composite at ambiguous intersections. The software must also reference the correct material parameter file for the two cartridge slots; an incorrect file can apply the wrong jetting, heating, or cure settings and produce off-ratio interfaces.
Interface morphology is the primary unknown in the composite. Each jetting pass deposits discrete droplets of white or clear resin adjacent to droplets of the other material; the UV cure then polymerizes the exposed surface. The resulting interfacial boundary is not a molecularly mixed blend, but a cured acrylate network with a composition gradient limited by droplet spreading and subsequent hatch overlap. Published tensile data for the white/clear interfacial plane within RWT-RCL-R50 geometries is limited; design of load-bearing boundaries should therefore include a validation coupon printed in the same orientation and with the same two-material assignment as the production part. Thermal history can also shift the clear fraction’s color. The clear phase is sensitive to cumulative UV dose and oven temperature; builds that remain in the support oven for extended cycles can develop a slight amber cast. If optical neutrality is critical, the entire thermal and UV history should be validated on a representative coupon before production.
Single-colour VisiJet M2R-BK and M2R-GRY produce homogeneous parts with uniform optical density. The RWT-RCL-R50 set permits internal cavities, fluid channels, or witness lines to be rendered in clear resin against a white body. The individual fractions share the same Shore D hardness and HDT values, so the set does not replicate the elastomeric recovery of VisiJet CE-BK or the castability of VisiJet M2Cast. Representative published values for the individual fractions are given below; values for the combined RWT-RCL-R50 composite require end-user confirmation because the interface volume fraction changes mechanical response.
| Property | VisiJet CR-WT 200 | VisiJet CR-CL 200 | Test method |
|---|---|---|---|
| Tensile strength, ultimate | 42.4 MPa | 49.9 MPa | ASTM D638-14 |
| Tensile modulus | 2160 MPa | 2160 MPa | ASTM D638-14 |
| Elongation at break | 7.5% | 7.5% | ASTM D638-14 |
| Flexural strength | 49.3 MPa | 65.1 MPa | ASTM D790-17 |
| Flexural modulus | 1870 MPa | 2100 MPa | ASTM D790-17 |
| Notched Izod impact | 22 J/m | 22 J/m | ASTM D256-10 |
| HDT at 0.45 MPa | 88°C | 88°C | ASTM D648-18 |
| HDT at 1.82 MPa | 61°C | 61°C | ASTM D648-18 |
| Shore D hardness | 85 | 85 | ASTM D2240-15 |
The two resins have identical Shore D hardness and HDT values, which means the composite set does not introduce elastomeric damping or a low-temperature phase. Published data for tensile strength across the white/clear interfacial plane is limited; parts with large planar boundaries should not be designed as if the interface exhibits bulk isotropic strength. Designers working in the MJP 2500-series environment generally orient critical loads perpendicular to the build plane only after validation, because MJP laminates can show anisotropic mechanical response.
Solvent exposure must be controlled. The rigid acrylate fractions can craze in contact with aggressive solvents such as acetone, methylene chloride, or aromatic hydrocarbon blends. Cleaning should be limited to isopropyl alcohol or mild aqueous detergent, with no prolonged soak. Alkaline cleaning solutions above pH 10 can etch the clear fraction and reduce optical clarity. The material is not certified for food-contact use under FDA 21 CFR unless the end user completes migration testing for the specific geometry and post-cure recipe. Biocompatibility under ISO 10993-1:2018 is not established in the public datasheets; laboratory evaluation is required for any medical-device prototype that contacts tissue or bodily fluid.
After the build is removed from the MJP 2500-series platform, the sacrificial support wax is liquefied in a circulating oven. The standard support-removal temperature is 65°C; higher setpoints accelerate wax drainage but approach the 61°C HDT limit at 1.82 MPa only if the part is under load or if stacked parts create pressure points. The support wax selected from the MJP support material family has a melting profile matched to the rigid fractions, but residual wax in blind channels is a known production issue. Pressurized air or low-pressure solvent flushing is used for internal channels after oven removal, followed by drying before UV post-cure.
Following wax removal, parts are rinsed in a post-processing bath to remove residual wax from internal channels; the clear fraction’s visual quality is highly sensitive to residual wax films, which require complete rinsing and, where permitted, a final UV-cure cycle. UV post-cure equipment should provide uniform irradiance in the UVA band, with dose logged per batch. Under-cured parts exhibit lower HDT and reduced chemical resistance; over-cure can produce yellowing in the clear fraction, especially when irradiance exceeds the material’s recommended band or when the part temperature rises above 60°C during cure. Both fractions undergo additional conversion during UV post-cure, producing volumetric shrinkage. Differential shrinkage between the white and clear phases can generate residual stress at interfaces; thicker white sections shrink more volumetrically than thin clear walls, leading to curl or delamination if the part is not adequately supported during cure.
Lot-to-lot variation is assessed by printing a standardized test coupon set and measuring tensile strength under ASTM D638-14, flexural modulus under ASTM D790-17, and Shore D hardness under ASTM D2240-15. Conditioning before testing follows ASTM D618-21: 23°C ± 2°C and 50% ± 5% relative humidity for at least 24 hours. Failure modes observed on MJP production lines include delamination at the white/clear interface when the post-cure dose is applied unevenly, cracking of thin clear sections during support-wax expansion, and clear-phase yellowing after exposure to UV flood irradiance above the manufacturer’s recommended band.
Application documentation for the MJP 2500-series identifies the paired set for mock-ups, fluid-path visualization aids, training models, and design-verification parts where the clear fraction provides visibility and the white fraction provides contrast. It is not a castable resin; foundry burnout processes should use VisiJet M2Cast unless the specific ash and thermal expansion profile of CR-WT 200 and CR-CL 200 has been validated for the shell system. The RWT-RCL-R50 set also differs from VisiJet M2G-DUR and VisiJet CE-BK engineering materials: the former targets engineering-toughness applications, and the latter targets elastomeric recovery, neither of which is replicated by the white/clear rigid composite. The clear fraction as printed has a translucent appearance; high optical clarity requires progressive abrasive polishing or clear-coating, and internal surfaces are not easily polished. Published data for total light transmittance is limited.
Because it is an acrylate photopolymer, the finished part is not suitable for thermoforming or machining in the same manner as a thermoplastic such as ABS or polycarbonate. Machining is possible with sharp, low-speed tools and coolant, but heat buildup can smear the surface. Continuous service temperature should remain below the HDT value of 61°C under load. Unloaded parts can tolerate short excursions above 61°C, but long-term exposure above 88°C can cause creep and dimensional distortion. Strong acids, strong bases, and polar solvents can reduce interlayer adhesion; no long-term chemical immersion rating is provided in public datasheets.