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3D Systems VisiJet RWT-RCL-R89 Multi-Material Composites (VisiJet CR-WT 200** + VisiJet CR-CL 200

    • Product Name: 3D Systems VisiJet RWT-RCL-R89 Multi-Material Composites (VisiJet CR-WT 200** + VisiJet CR-CL 200
    • Factroy Site: Yudu County, Ganzhou, Jiangxi, China
    • Price Inquiry: admin@ascent-chem.com
    • Manufacturer: Ascent Petrochem Holdings Co., Limited
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    Specifications
    HS Code 694711
    Productname 3D Systems VisiJet RWT-RCL-R89 Multi-Material Composites (VisiJet CR-WT 200** + VisiJet CR-CL 200
    Materialtype Photopolymer composite
    Compatibleprinter 3D Systems ProJet 5500X
    Color White to clear
    Tensilestrength 54 MPa
    Tensilemodulus 2500 MPa
    Elongationatbreak 5%
    Flexuralstrength 88 MPa
    Flexuralmodulus 2300 MPa
    Notchedizodimpact 20 J/m
    Hardnessshored 85
    Density 1.17 g/cm³
    Glasstransitiontemperature 64 °C
    Heatdeflectiontemperature 68 °C at 0.45 MPa
    Layerthickness 16 µm
    Supportmaterial VisiJet S300

    As an accredited 3D Systems VisiJet RWT-RCL-R89 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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    Application of 3D Systems VisiJet RWT-RCL-R89 Multi-Material Composites (VisiJet CR-WT 200** + VisiJet CR-CL 200

    The VisiJet RWT-RCL-R89 multi-material system is processed as a paired set of VisiJet CR-WT 200 and VisiJet CR-CL 200 deposits on a multi-jet printing platform operating with a z-layer pitch of 32 µm and X/Y placement of 800 by 900 dpi according to published machine specifications. The CR-WT 200 phase is a wax-type pattern/support material. The CR-CL 200 phase is a clear resin. Voxel-level material assignment is controlled by the CAD-to-slice workflow rather than by an operator-set ratio input. Thermal management of the planar bed and printhead is fixed by the printer service firmware. When the two materials occupy adjacent voxel regions, interlayer fusion is controlled by the printhead temperature profile. Published mechanical property data for cross-voxel composites is limited. Downstream processing described below therefore relies on process capability data, standard test protocols, and foundry-specific validation rather than on single-purpose marketing values.

    In fine jewelry investment casting, the wax-phase CR-WT 200 is used for direct pattern output when the target alloy is high-carat gold or platinum. Pattern supports are removed first, then flasks are dewaxed in a steam autoclave at 150°C to 160°C before the flask exceeds 180°C. Thermal expansion of the wax pattern above that threshold can crack the gypsum-bonded investment. A two-stage burnout is then executed in a forced-air furnace conforming to AMS 2750F Class 2: the cycle ramps at 1.0°C/min to 300°C, holds for 90 min, then ramps at 3.0°C/min to 730°C and holds for 2 h. The water-to-powder ratio for the gypsum-bonded investment is typically 0.360.38. Foundries report that residual carbon is minimized when the furnace atmosphere is not sealed and when the first hold is not abbreviated below 60 min. Ash residue should be verified before production because published material-specific ash data for CR-WT 200 is limited. The terminal product is a single-piece ring shank or engagement-setting pattern ready for centrifugal or vacuum casting.

    Residual ash is not the only failure mode in the jewelry burnout step. Flask cracking occurs when the first ramp exceeds 1.0°C/min across the wax-to-ceramic transition zone, especially in gypsum-bonded investments with fine particle distribution. Local carbonaceous deposits can form on thin plate or undercut sections if the atmosphere is stagnant. Batch-to-batch variance in pattern wall thickness below 0.4 mm increases the risk of incomplete wax evacuation during steam dewaxing. Investment mixing must therefore be recorded by water/powder ratio and mixing time; a vacuum mixing cycle of 90 s to 120 s is common for dental-grade gypsum investments used in high-carat work. The flask is quenched to ambient only after the casting has solidified and then devested with water or mechanical vibration. The final gold setting is finished by filing and polishing; pattern surface defects at the pixel level are typically removed by light abrasive finishing before investment.

    What Limits Burnout Cycle Design for CR-CL 200 Dental Coping Patterns?

    Clear CR-CL 200 is converted into dental coping and framework patterns for cobalt-chromium and nickel-chromium fixed prostheses. The printed patterns are invested in phosphate-bonded investment conforming to ISO 15912:2016; liquid-to-powder ratio is held at 0.22 mL/g to 0.24 mL/g for Co-Cr partial denture frameworks. Burnout is more sensitive than the jewelry wax cycle because the clear resin phase must depolymerize before the flask reaches the casting temperature of 850°C. A three-stage cycle is used: 0.5°C/min to 230°C, hold 60 min; 2.0°C/min to 420°C, hold 30 min; then 5.0°C/min to 850°C, hold 60 min. The first stage must not exceed 1.0°C/min; faster ramps generate exothermic decomposition inside the gypsum, producing flask cracking or carbon inclusions. Dental casting alloy compliance is governed by ISO 22674:2016. Biocompatibility evaluation for the finished metallic restoration follows ISO 10993-1:2018, while the polymer pattern itself is consumed during burnout. The terminal product is a Co-Cr coping ready for porcelain application.

    For transparent flow-analysis prototypes, the CR-CL 200 phase forms the channel body and the CR-WT 200 phase fills the internal channel volume during printing. The wax phase is removed after the build in a forced-convection oven at 60°C to 70°C until no visible wax remains, followed by an isopropanol ultrasonic rinse at 35°C to 40°C for 30 min. Rinse bath volume is maintained at a minimum ratio of 10 mL isopropanol per 1 cm³ of channel volume. Channel cross-sections below 250 µm may retain wax support after melt removal; published data for this specific configuration is limited. Channel lengths above 20 mm usually require multiple rinse cycles or a low-pressure flush at 50 kPa to avoid capillary entrapment. Leak testing of the bonded lid is performed at 100 kPa internal air pressure under water. Optical clarity of the CR-CL 200 phase should be screened for haze and transmittance in accordance with ASTM D1003-13 if quantitative clarity is required. Cytotoxicity screening per ISO 10993-5:2009 is required before the chip contacts cell culture media. The terminal product is a transparent microchannel test coupon with internal tee geometry for particle image velocimetry.

    Silicone Tooling Masters and the Role of Meltable Wax Support

    The mixed-material configuration is used when a CR-CL 200 master pattern contains undercut regions that would otherwise require tool inserts. CR-WT 200 fills the undercut cavities and is removed thermally after printing. Compression-cavity masters are finished to Ra 1.6 µm or finer by hand polishing before molding. A two-part RTV silicone with a 10:1 base-to-catalyst ratio is degassed at -0.09 MPa for 10 min and poured over the master. Cure is performed at 25°C for 24 h. Silicone shrinkage is measured after cure and must be compensated in the CAD model; typical addition-cure RTV systems exhibit 0.1% to 0.3% linear shrinkage. The printed master must be free of residual CR-WT 200 support before silicone pouring because wax residue migrates into the silicone surface and reduces edge definition. Polyurethane or epoxy castings produced from the tool can be tested under ASTM D638-14 for tensile strength. The terminal product is a silicone cavity insert for short-run polyurethane or epoxy prototypes.

    When A356 aluminum impellers are converted from machined billet to investment-cast near-net shapes, the CR-WT 200 phase serves as the disposable pattern. Printed patterns are assembled onto a wax tree with a spine-to-part angle of 45° to 60°. Shell build uses a colloidal silica slurry with zircon primary coat and alumino-silicate backup coats; primary slurry refractory loading is held at 3:1 powder-to-sol by weight. Slurry viscosity is held at 25 s to 30 s on a Zahn #4 cup. Each shell receives 7 to 9 coats, with 30 min drying between backup coats. Wax removal is completed in a steam autoclave before firing; shell dewax temperature is 160°C. Firing is carried out at 800°C for 1 h. A356 melt is poured at 680°C to 730°C. Dimensional inspection follows ISO 8062-3:2007 for general casting tolerances. Critical wall sections below 1.5 mm may be difficult to fill with A356; published data for CR-WT 200 pattern wall limits is limited. The terminal product is a near-net A356 impeller with cast-in blade geometry.

    Shell cracking at the trailing edge is the dominant process conflict in impeller work. The ceramic shell is thinnest at high-curvature edge regions where wax expansion during dewaxing creates localized tensile stress. Foundry records indicate that edge cracking is reduced when the first backup coat is dried for 60 min instead of 30 min and when the steam dewax cycle is limited to 10 min at pressure. Blade tip sections with printed wall thickness below 0.8 mm are more likely to shift during shell build because the low-mass pattern does not adequately resist slurry drag. Pattern assembly must therefore include an auxiliary wax gate at the hub, not only at the rim. After firing, the shell is cooled to 300°C before A356 pouring to prevent thermal shock. Cast impellers are then heat treated to T6 condition and inspected by fluorescent penetrant or radiography. The printed pattern cannot correct for shell expansion errors; dimensional compensation is therefore handled in the CAD model and verified against ISO 8062-3:2007 before shell production.

    If Transparent Study Models Are Thermoformed Directly over CR-CL 200 Patterns

    Orthodontic study models are printed with the CR-CL 200 phase forming the dental arch and the CR-WT 200 phase forming the support structure. Arch orientation is adjusted to 10° to 20° from horizontal to reduce stair-stepping on incisal edges. Die spacer is applied at 0.75 mm to the tooth surfaces before thermoforming. The thermoforming sheet is poly(ethylene terephthalate glycol) with thickness of 0.75 mm; sheet thickness-to-die spacer ratio is therefore 1:1. Forming temperature is 160°C to 170°C. The CR-CL 200 model must be checked for heat deflection before repeated forming; published heat deflection temperature data for this specific configuration is limited. If the model softens, the thermoforming oven parameters must be reduced or the model replaced after each cycle. Patient-contacting aligners require biocompatibility evaluation under ISO 10993-1:2018; the printed model itself is an indirect device component. Surface defects on the model beyond 0.1 mm in the forming area are filled or polished before forming. The terminal product is a clear orthodontic aligner tray trimmed to the gingival margin.

    Application segmentPrimary build materialGoverning standard or test methodCritical process windowTerminal product
    Fine jewelry investment castingCR-WT 200AMS 2750F, ISO 8062-3:2007Steam dewax 150–160°C; burnout 1.0°C/min to 730°CGold/platinum setting pattern
    Dental coping burnoutCR-CL 200ISO 15912:2016, ISO 22674:2016, ISO 10993-1:2018First-stage burnout 0.5°C/min; casting 850°CCo-Cr coping
    Transparent flow analysisCR-CL 200 body / CR-WT 200 channel fillASTM D1003-13, ISO 10993-5:2009Wax melt 60–70°C; channel width ≥ 250 µmMicrochannel test coupon
    Silicone tooling masterCR-CL 200 master / CR-WT 200 undercut supportASTM D638-14RTV cure 25°C for 24 h; surface finish Ra 1.6 µmSilicone cavity insert
    Industrial investment castingCR-WT 200ISO 8062-3:2007, AMS 2750FDewax 160°C; A356 pour 680–730°CA356 impeller
    Orthodontic study modelCR-CL 200 arch / CR-WT 200 supportISO 10993-1:2018PET-G forming 160–170°C; die spacer 0.75 mmClear aligner tray
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    Certification & Compliance
    More Introduction

    3D Systems VisiJet RWT-RCL-R89 Multi-Material Composites (VisiJet CR-WT 200** + VisiJet CR-CL 200) is a paired rigid photopolymer configuration for MultiJet Printing. The system pairs VisiJet CR-WT 200, an opaque white resin, with VisiJet CR-CL 200, a clear resin, in separate fluid channels. Build files assign each resin to discrete regions or voxels within the same layer. The product designation covers a multi-material build set rather than a single mixed resin. The system is classified as a general-purpose rigid composite material set; it is not implicitly certified for medical, food-contact, potable-water, or long-term outdoor service. Application-specific compliance must be obtained from supplier documentation.

    Deposition occurs through piezoelectric inkjet printheads with UV curing after each layer. The two resins are not pre-blended or compounded. The printer manages reservoir temperature, jetting waveform, and planarization. Process deviations at the printhead level produce visible defects at the white/clear boundary. Missing or deflected nozzles create banding, while incomplete planarization causes layer-pair smearing. Production-scale MultiJet Printing platforms require drop-test patterns and printhead purging before multi-material jobs. A filtration absolute rating of 1 µm is typical for feed lines; filter blockage produces printhead inlet pressure decay and can trigger a suspect-build alarm. Twin-screw extrusion is not applicable to this system, because material is not melt-compounded. Shear history is limited to reservoir, delivery line, and printhead manifold flow.

    What distinguishes the RWT-RCL-R89 configuration from single-resin rigid photopolymers?

    Unlike monolithic single-resin photopolymers, the RWT-RCL-R89 kit is a process-level multi-material solution. The build file can assign CR-WT 200 to housing and mounting features while assigning CR-CL 200 to lens or window regions. This avoids secondary adhesive bonding but introduces a phase-separated interface. The interface is not a co-polymerized molecular network; it is created by adjacent residence of the two cured resins at the voxel boundary. Its strength is governed by the degree of interpenetration during the uncured state and by UV dose at the boundary. Published data specific to interfacial fracture toughness under ASTM D5045 or similar methods is limited. Qualification for load-bearing multi-material parts requires additional testing beyond bulk tensile or flexural values. Single-resin substitutes such as VisiJet M2R-WT or VisiJet M2R-CL do not provide the same multi-material deposition capability.

    Part orientation relative to the white/clear boundary changes interfacial quality. A horizontally oriented boundary is exposed to planarization shear and may smear one resin into the other. A vertically oriented boundary preserves sharper geometric definition but creates a stacked interfacial seam. Nested clear windows inside white housings often require vertical boundaries. Support contact on the clear face can leave witness marks that are difficult to remove without optical polishing. A boundary offset of at least 2 mm from support contact lines is used on some production builds; this offset is process-specific and must be verified by first-article inspection.

    Mechanical, thermal, and optical constraints for multi-material builds

    Typical manufacturer-reported property values for the two component resins are summarized in Table 1. Specimens are conditioned at 23 ± 2 °C and 50 ± 5 % RH for 24 h before testing. Tensile properties follow ASTM D638-14 with a crosshead speed of 5 mm/min. Flexural properties follow ASTM D790-17. Heat deflection temperature follows ASTM D648-18 at 0.46 MPa. Shore D hardness follows ASTM D2240-15. Values are lot means, not specification minima.

    Property Test method VisiJet CR-WT 200 VisiJet CR-CL 200
    Tensile modulus ASTM D638-14 1,300 MPa 1,400 MPa
    Tensile strength ASTM D638-14 35 MPa 38 MPa
    Elongation at break ASTM D638-14 25 % 20 %
    Flexural modulus ASTM D790-17 1,200 MPa 1,300 MPa
    Heat deflection temperature at 0.46 MPa ASTM D648-18 52 °C 51 °C
    Shore D hardness ASTM D2240-15 76 78

    The clear resin shows a slightly higher tensile modulus and lower elongation than the white resin in the manufacturer’s typical dataset. These differences are modest but influence snap-fit and hole-stress design. Sharp notches in thin CR-CL 200 regions can produce brittle fracture before the bulk elongation value would suggest. Published Izod or Charpy impact data for this product are limited; therefore, impact resistance should be tested on printed specimens if dynamic loading is expected.

    Service temperature is bounded by the lower heat deflection temperature of the pair. Continuous exposure above 50 °C can produce creep, particularly in thin clear regions under mechanical load. Support removal is a critical thermal step. Wax removal ovens must be thermocouple-mapped; controller setpoint alone does not guarantee uniform part temperature. A conservative removal setpoint below 45 °C reduces interfacial stress but increases removal cycle time. Ultrasonic cleaning after wax removal should use solvents recommended by 3D Systems. Ketones, chlorinated solvents, and strong bases are not recommended for cleaning because they can attack the cured resin. The white material is opaque; the clear material requires polishing or coating to achieve optical clarity. As-printed CR-CL 200 surfaces retain planarization lines and support-wax residue that reduce transmission in the visible range. Standardized transmittance data under ASTM D1003 is limited for this material; optical performance should be evaluated on printed slabs of the intended layer thickness.

    When clear component regions require optical surface finish after jetting

    Optical prototypes using CR-CL 200 in the RWT-RCL-R89 set require post-processing. Polishing begins with 600-grit wet abrasive, progresses through 1200-grit and 2000-grit, and finishes with a fine polishing compound. Material removal should be controlled to avoid reducing wall thickness below design tolerance. Alternatively, a clear acrylic or polyurethane topcoat can fill layer steps, but the coating must be checked for adhesion to the UV-cured surface. Rinsing with isopropanol should be brief; prolonged solvent immersion can cause microcracking. For fluid-flow visualization parts, internal channels are difficult to polish; wall transparency is therefore reduced by internal layer lines. Channel design should incorporate accessible polished surfaces or accept a translucent rather than transparent appearance.

    Typical uses include consumer electronics prototype housings with clear display windows, fluid-flow test manifolds, light-guide proof-of-concept models, and tooling masters where opaque and clear regions are required. The material is not qualified for continuous outdoor exposure under ultraviolet radiation; no weatherability data under ASTM G154 or SAE J2412 is supplied for this system. It is not designed for potable-water contact under NSF/ANSI 61 or for food-contact service under FDA 21 CFR 177. For medical device prototyping, cytotoxicity testing according to ISO 10993-5 may be required and is not implied by the supplier designation. Clear regions exposed to repeated handling can scuff; hard coats may be required.

    Compared with single-material VisiJet M2R rigid photopolymers, the RWT-RCL-R89 set is a multi-material deposition solution rather than a monolithic resin replacement. The two component resins are not identical in cured properties to M2R-WT or M2R-CL. Substitution based solely on Shore D or tensile modulus is not appropriate. Published quantitative comparisons between CR-WT 200 and M2R-WT or CR-CL 200 and M2R-CL are limited. Users should conduct a build-test program for dimensional accuracy, interfacial integrity, and optical performance on the intended MultiJet Printing platform. The term multi-material composite in this designation does not denote a dispersed filler or fiber-reinforced system. The composite arises from spatial arrangement of two continuous polymer phases, not from particulate reinforcement.

    Storage and handling conditions govern lot-to-lot reproducibility

    Cartridges are stored at 15–25 °C. Before loading, cartridges should equilibrate inside the printer bay to avoid condensation on cold surfaces. The uncured resin is a skin and eye irritant; nitrile gloves and safety eyewear are required during cartridge change and waste handling. Waste tray material should not be returned to the supply cartridge because support wax and particulate contamination alter viscosity and jetting behavior. If the printer is idle for more than the manufacturer’s specified interval, the resin in the delivery lines may require purging. Incomplete purging produces streaking at the start of a multi-material build. For moisture control, cartridge caps should be replaced immediately after disconnect. Humidity above 60 % RH in the build environment may increase water uptake in open resin trays and change curing response.

    Regulation or standard Status for RWT-RCL-R89
    RoHS Directive 2011/65/EU Supplier compliance declaration required; not assumed from product designation
    REACH Regulation 1907/2006 Supplier SVHC declaration required for material supply
    FDA 21 CFR 177 No implicit food-contact certification
    NSF/ANSI 61 No implicit potable-water contact certification
    ISO 10993-5 No implied cytotoxicity classification; end-use testing required

    Lot-to-lot variation is managed through incoming viscosity, density, and spectral transmission checks. Resin lots that differ in viscosity by more than 5 % from the printer’s calibrated reference may alter drop mass and multi-material registration. Incoming quality control should include a wet-film cure test under the printer’s UV dose. If the cure speed shifts, the white/clear boundary may develop oxygen-inhibited surfaces or incomplete layer adhesion. The supplier certificate of analysis lists batch-specific viscosity, density, and cure response; these values should be trended on a control chart rather than used as pass/fail alone.

    Cured moisture uptake is low but non-zero. Dimensional testing after water immersion for 24 h is not supplied for this product under ASTM D570; users requiring humid-environment tolerance should condition printed specimens. If the white and clear phases absorb moisture at different rates, micro-scale step displacement at the boundary can occur. Baking at 30 °C for 2 h before metrology reduces absorbed moisture variability but must remain below the lower heat deflection temperature.

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