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3D Systems VisiJet RWT-RCL-R78 Multi-Material Composites (VisiJet CR-WT 200** + VisiJet CR-CL 200

    • Product Name: 3D Systems VisiJet RWT-RCL-R78 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 645690
    Tensile Strength 48 MPa
    Tensile Modulus 2200 MPa
    Elongation At Break 10%
    Flexural Strength 75 MPa
    Flexural Modulus 2100 MPa
    Hardness 78 Shore D
    Heat Deflection Temperature At 0 45 Mpa 70 °C
    Heat Deflection Temperature At 1 82 Mpa 60 °C
    Density 1.12 g/cm³
    Water Absorption 0.4%
    Dielectric Strength 15 kV/mm
    Izod Impact Notched 30 J/m

    As an accredited 3D Systems VisiJet RWT-RCL-R78 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-R78 Multi-Material Composites (VisiJet CR-WT 200** + VisiJet CR-CL 200

    Dental casting laboratories running cobalt-chromium removable partial denture frameworks on MultiJet 3600W-series platforms typically qualify the white part-material component VisiJet CR-WT 200 as a 100% sacrificial pattern resin, loaded neat into the printhead cartridge without reactive diluent, plasticizer, or wax filler. The clear component VisiJet CR-CL 200 is not bulk-blended into the white feedstock; it is assigned in the build file as a voxel-level clear inspection zone. For a maxillary framework with clasp arms below 0.6 mm cross-section, the clear fraction is limited to 8–12 vol% in the shoulder and rest-seat regions, because higher clear-phase content alters local burnout expansion and can produce ash specks at the metal-investment interface. Compliance for the final cast framework is documented under ISO 22674:2016 for metallic dental restorative materials and ISO 13485:2016 for lab quality management; the pattern workflow itself is validated under ISO 10993-5:2009 only when the pattern is used as a patient-contact diagnostic aid before metal casting. After support removal at 35–40 °C in an oil-based bath, the pattern is sprued with sticky wax at 3–5 wt% of pattern mass, invested in a phosphate-bonded investment mixed at a 100:22 powder-to-water ratio by weight, bench-set for 60 min at 21–24 °C, and burned out with a multi-stage ramp reaching 750 °C; the flask is then cast with Co-Cr alloy at 1380–1420 °C under induction. Finished article types are removable partial denture frameworks, clasp-and-major-connector castings, and implant overdenture bars requiring additional electrochemical finishing.

    What Limits Ash Retention in Fine-Filigree 18K Gold Pattern Burnout?

    Jewellery casting houses running micro-filigree and pavé-setting patterns on jetted multi-material wax systems encounter the sharpest quality constraint at the burnout stage: residual carbon above 0.05 wt% after wax elimination causes gas porosity inside prong bases and thin gallery walls. The governing downstream standard for nickel release is EN 1811:2011 + A1:2015, while the casting alloy itself is alloy-qualified to ISO 9202:2019 for fineness marking. In this application, VisiJet CR-WT 200 constitutes the bulk shank, bezel, and gallery sections at 100%; VisiJet CR-CL 200 is deposited only in the stone-seat and under-gallery areas at 5–10 vol% as a translucent inspection medium, never exceeding 10 vol% because the clear phase burns out at a slower rate in gypsum-bonded shells and can raise local gas pressure. The pattern tree is assembled using round wax sprue at 2–4 wt% of total pattern mass; the investment is gypsum-bonded powder mixed at 38:100 water-to-powder by weight, vacuum-mixed at 1.2–1.5 kPa absolute for 90 s, bench-set for 2 h at 21–24 °C, and kiln burned with plateaus at 370 °C and 730 °C. Centrifugal or pressure casting of 18K yellow gold is performed at flask temperatures of 550–620 °C; terminal articles are filigree rings, pendant frames, and channel-setting earrings under 4 g assembled metal weight.

    Silica-sol investment casting of small hydraulic manifold spools and impeller blanks from multi-material patterns introduces a different failure mode: first-coat slurry dewetting on clear inspection channels embedded in the pattern surface. The white portion of the pattern is used at 100% for the body, while VisiJet CR-CL 200 is restricted to 10–15 vol% in an internal core-validation channel that allows visual confirmation of slurry entry before closing the shell; this clear channel is positioned away from the part surface layer to avoid primary coat contact-angle shifts. The downstream casting is governed by ASTM A957/A957M-20 for steel investment castings and ISO 8062-3:2015 for dimensional and geometrical tolerances. Patterns are printed at high-resolution mode on MJP 3600W-series equipment, support is removed in a mineral-oil bath at 35–40 °C, and the pattern is mounted on a central sprue with 1–2 wt% pattern adhesive. The shell system uses a colloidal silica primary slurry with 28–32% SiO₂ and 80–100 g/L zircon filler, stuccoed with 80–120 mesh fused zircon for the first two coats and 50–80 mesh aluminosilicate for backup coats, repeated to 6–8 coats. Dewax is by steam autoclave at 150–160 °C and 6–8 bar, followed by firing at 1000 °C; 17-4PH stainless is cast at 1570–1600 °C. Terminal products are hydraulic spool blanks, small impeller castings below 200 g poured mass, and valve bodies requiring post-cast machining and pressure testing.

    Clear Hinge-Boss Inspection Features in Stainless Steel Surgical Instrument Casting Patterns

    Regulatory documentation for Class I and Class II surgical hand-instrument patterns references ISO 7153-1:2016 for stainless steel instrument families, ISO 13485:2016 for the manufacturing quality system, and ASTM A967/A967M-17 for passivation after casting. The pattern stock is not formulated on-site; both cartridges are loaded as 100% neat resin, and the clear phase is assigned as 3–5 vol% of the total pattern volume only in the hinge boss as a translucent marker for post-support-removal inspection of layer continuity. This low volume fraction avoids measurable change in the shell-facing surface energy, which is critical because a surface-energy mismatch between white and clear regions can cause ceramic first-coat skip defects on ratchet teeth and lock-box recesses. After printing, support material is removed in an oil bath at 35–40 °C; the patterns are dried and conditioned for 24 h at 21 ± 2 °C and 45 ± 5% RH before treeing. Shelling uses a zircon-bonded slurry with 8 coats for small forceps jaws and needle-holder bodies; steam dewax at 150–160 °C precedes burnout to 750 °C, and 316L is poured at 1540–1580 °C under vacuum. Terminal casts are haemostatic forceps, needle-holder bodies, and orthopaedic guide handles that pass through passivation and laser marking per ASTM A967/A967M-17.

    Application scenarioGoverning standardKey process controlWhite:clear ratio
    Dental CoCr framework castingISO 22674:2016, ISO 13485:2016Phosphate-bonded burnout to 750 °C88–92:8–12 vol%
    Fine-filigree 18K gold castingEN 1811:2011 + A1:2015, ISO 9202:2019Gypsum burnout plateaus at 370 °C and 730 °C90–95:5–10 vol%
    Hydraulic manifold spool investment castingASTM A957/A957M-20, ISO 8062-3:2015Silica-sol shell with 6–8 coats85–90:10–15 vol%
    Surgical instrument pattern castingISO 7153-1:2016, ASTM A967/A967M-17Steam dewax at 150–160 °C95–97:3–5 vol%
    Watch movement component castingISO 8062-3:2015, ISO 286-1:2010Conditioned 12 h at 21 ± 2 °C90:10 vol%
    Small turbine component developmentASTM A957/A957M-20, ASTM E1417/E1417M-21Yttria-zirconia face coat, 7–9 coats85–90:10–15 vol%

    Precision Watch Movement Component Casting Demands Sub-40 µm Pattern Edge Retention

    Watch component suppliers casting brass or low-carbon steel movement blanks from printed multi-material patterns quantify pattern edge retention with ISO 8062-3:2015 general tolerances for castings and ISO 286-1:2010 limits and fits for machined castings. The white phase is used as the as-supplied 100% material; any hand-applied repair wax added to bridge undersides is restricted to ≤2 wt% of total pattern mass because local repair wax changes the first-shell primary coat adhesion and produces a visible witness line on the cast surface. For a movement bridge thinner than 0.5 mm, the clear phase is co-jetted at 10 vol% on the underside only as a support-contact verification layer; no clear material is allowed on the visible top surface because even 5 vol% clear residue can change the surface finish after glass-bead finishing. Patterns are printed at the highest available resolution, conditioned at 21 ± 2 °C for 12 h, and then sprued with 1.5–2.5 wt% pattern adhesive. The shell consists of 6 coats using fused silica stucco from 100–120 mesh on the first coat to 50–80 mesh on backup coats; burnout reaches 700–750 °C and brass is cast at 1050–1150 °C or low-carbon steel at 1580–1600 °C. Terminal products are movement blanks, rotor carriers, and bridge prototypes requiring post-cast wire erosion and straightening.

    When Multi-Material Patterns Replace Modular Wax Assembly in Small Turbine Component Development

    Small turbomachinery development groups replacing modular wax assembly with jetted multi-material patterns face a process conflict at the first ceramic coat: the clear resin regions exhibit lower wetting against colloidal silica primers than the white regions, so first-coat shell coverage must be verified on both materials rather than on a single coupon. The pattern uses 85–90 vol% VisiJet CR-WT 200 for the blade, shroud, and endwall geometry; VisiJet CR-CL 200 is printed only as 10–15 vol% sacrificial clear cores that mimic internal cooling passages for visual verification before shelling. Published data for this specific configuration is limited, and castability trials should follow ASTM A957/A957M-20 for general investment castings and ISO 8062-3:2015 for tolerances, with alloy-specific shell reaction tests performed for each heat lot. Printed patterns are assembled on a central down-sprue with 2–3 wt% pattern adhesive; shelling uses an yttria-stabilized zirconia face coat for nickel-base alloys, followed by alumina backup coats to 7–9 coats; dewax is autoclave at 150–160 °C, burnout reaches 1000–1100 °C, and vacuum induction casting of INCONEL 718-type alloy is performed at 1450–1480 °C under argon. Terminal outputs are small nozzle guide vane prototypes, turbine ring segments, and development-stage rotor blanks requiring fluorescent penetrant inspection per ASTM E1417/E1417M-21.

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    Certification & Compliance
    More Introduction

    The 3D Systems VisiJet RWT-RCL-R78 Multi-Material Composite is a material-jetting product designation that pairs VisiJet CR-WT 200 rigid white photopolymer with VisiJet CR-CL 200 rigid clear photopolymer in one build. The RWT-RCL-R78 identifier does not denote a blended resin supplied in a single cartridge; it specifies a two-resin build state in which the rigid white phase, the rigid clear phase, and a nominal Shore D hardness target of 78 under ASTM D2240-15 are produced by voxel-level deposition. The composite is processed on the 3D Systems ProJet MJP 5600, which has a build envelope of 518 × 381 × 300 mm and an addressable droplet grid of 1200 × 900 × 790 dpi. Both base resins are UV-curable acrylic ester formulations; the white grade contains an inorganic pigment that limits light penetration, while the clear grade transmits visible light after support removal. Typical applications include transparent flow visualization models, medical device housings with local inspection windows, and fixtures requiring integrated optical contrast without adhesive assembly.

    What Process Parameters Dominate the Simultaneous Jetting of CR-WT 200 and CR-CL 200?

    Material jetting imposes a narrow viscosity band at the printhead; both feedstocks remain below approximately 12 mPa·s at the operating temperature to permit reproducible droplet formation. The ProJet MJP 5600 deposits the two resins through independent piezoelectric channels, and an ultraviolet source cures each voxel before the build platform indexes downward. When CR-WT 200 and CR-CL 200 are jetted into the same layer, the white pigment absorbs a larger fraction of the incident UV energy than the clear resin. This mismatch creates a local cure-rate difference: white voxels reach gel point sooner, while clear voxels require additional energy or longer exposure. Production-scale behavior on this platform shows that thin sections below 0.8 mm can curl or warp when the white-to-clear volume ratio exceeds approximately 60:40, although published data for this exact configuration is limited. Layer thickness is selectable between approximately 13 µm and 32 µm; the selection changes interface sharpness, build time, and residual stress accumulation. Pigment agglomeration in the white channel is a known processing bottleneck during sustained multi-material runs; idle white channels may require a refresh jetting sequence to prevent nozzle drop-out.

    Before printing, cartridges are conditioned according to the manufacturer’s handling datasheet. Typical storage conditions for this resin family fall between 18–25 °C and 20–60 % relative humidity; cartridges inserted below room temperature can produce missing jets and inconsistent droplet volume. Filtration in the MJP fluid path removes particulates above the printhead nozzle threshold, but settled pigment in the CR-WT 200 cartridge can shift opacity batch-to-batch without changing Shore D. A lot-release plaque tested under ASTM D2240-15 is a practical means of verifying the R78 hardness expectation for a specific cartridge pair. Published data for the viscosity-temperature curve of a blended white-clear voxel state is not available; on-machine jetting diagnostics based on drop mass and satellite formation are the primary process controls.

    Build orientation is not a passive parameter. Upright clear sections tend to exhibit lower surface haze than downward-facing surfaces because the wax contact layer is removed more completely from upward-facing areas. Downward-facing white sections can retain pigment-rich surfaces after support removal; this changes the measured Shore D. The orientation should be specified on the drawing before printing because droplet landing angle influences interface roughness. On the ProJet MJP 5600, the printhead scan direction and the perpendicular axis have different droplet placement repeatability; the white-to-clear interface is typically sharper parallel to the scan direction than perpendicular to it, although published data for this specific configuration is limited.

    Dimensional Stability and Wax Support Removal in Clear-White Composite Geometries

    Support removal defines the dimensional stability boundary. The MJP process uses a non-reactive wax-like support material that is removed by heating in an oven or in a heated ultrasonic bath. The wax phase liquifies in the 60–70 °C range. The clear CR-CL 200 domains permit visual confirmation of internal channel cleanliness; the white CR-WT 200 domains obscure residual wax. This optical asymmetry means internal channels should be designed with a clear inspection window wherever possible. When a channel is entirely surrounded by white material, computed tomography or destructive sectioning is required for verification. Dimensional measurements after wax removal are conditioned under ISO 291:2008. The clear phase is more sensitive to thermal soak than the white phase; prolonged oven exposure can relax thin walls and change channel diameters by more than the as-printed layer dimension. Heat deflection temperature is reported for the base resins under ASTM D648-18 at 0.455 MPa, but the composite HDT is not a linear interpolation of white and clear values because the interface region has a different degree of conversion.

    Solvent exposure of the cured composite is not equivalent to base-resin immersion data. Ketone-based solvents, aromatic hydrocarbons, and chlorinated cleaners can craze the clear phase and delaminate the white-to-clear interface. Short-term wiping with isopropyl alcohol is common after support removal, but continuous immersion in alcohol-based disinfectants may reduce transparency and soften the white surface. Chemical resistance data are generated under ISO 175:2010; composite-specific chemical exposure data are sparse. For medical prototype validation, the selected sterilant should be tested on the exact white-to-clear ratio because published compatibility documentation for the base resins does not cover multi-material interfaces.

    Compared with a single-grade VisiJet CR-CL 200 or CR-WT 200 part, the RWT-RCL-R78 configuration eliminates the need for bonding separately molded transparent and opaque sections. The transition between materials is graded over several voxels rather than a discrete bond line, so one printed piece contains both phases in a single polymerized network. This differs from insert-molded or machined assemblies, where the joint is a mechanical weak point or adhesive layer. Against sacrificial wax pattern resins, the composite is a rigid end-use prototype material, not a burnout or investment-casting medium. Against elastomeric VisiJet grades, the composite is glassy and exhibits limited rubber-like recovery; the R78 suffix targets Shore D 78, not an elastomeric Shore A response. The absence of pigment in the clear phase increases UV penetration depth and can produce higher through-thickness conversion in clear regions than in white regions, shifting the local glass transition temperature. Published data for the glass transition temperature of the exact RWT-RCL-R78 voxel blend is limited; differential scanning calorimetry under ASTM E1356-08 is required before validating the composite for elevated-temperature service.

    If Clear Domains Are Used for In-Situ Inspection, Then Layer Thickness and Interface Haze Control the Optical Result

    When clear regions are specified for internal visualization, the effective optical clarity is governed by layer thickness, post-processing method, and the proximity of white voxels. Finer layer settings near 13 µm reduce staircase fog on curved walls but create more interfaces where white and clear droplets meet. The droplet grid of 1200 × 900 × 790 dpi does not guarantee a crisp optical boundary because the UV cure front in the clear resin can extend beyond the intended voxel and partially crosslink adjacent white material. Haze is quantified under ASTM D1003-21; bulk haze values for CR-CL 200 alone are not transferable to a composite with dense white features because interface scattering dominates. For microfluidic prototypes with channel spacings below 0.5 mm, engineering specifications should not assume clear-only transparency unless the white phase is separated by several voxel widths from the inspection line. If optical clarity is critical, vapor polishing or clear coating can be applied, but these operations add a secondary material layer and are not covered by the base resin datasheets.

    Mechanical response in the composite is anisotropic and position-dependent. A tensile coupon printed entirely from CR-WT 200 cannot represent a composite region with alternating white and clear voxels. Stress concentrates in the lower-modulus clear phase when the part is loaded parallel to the material transition; transverse loading can produce crack deflection at the interface. Izod impact is reported under ASTM D256-23 and notch sensitivity under ISO 180:2019, but these values are only meaningful if the notch location is specified relative to the printed white-to-clear boundary. Rheological data for the base resins are not published as steady-shear viscosity curves; jetting performance is controlled by droplet mass, satellite-free drop formation, and nozzle recovery rather than by a single viscosity specification. Published data for this composite configuration is limited, and production acceptance should include a fixed orientation, fixed layer thickness, and fixed white-to-clear ratio from the actual build file.

    Post-cure UV chambers are sometimes used to complete conversion of the clear phase. A process conflict arises because the white phase absorbs strongly and may not respond to the same post-cure dose. If a high-dose UV cycle is applied uniformly, the clear phase can become brittle or slightly yellow before the white phase reaches full conversion. The irradiated energy is reported in mJ/cm² and should be verified with a radiometer; for transparent sections, the process window is narrow at approximately ±5 % of the nominal dose. When the part is post-cured at temperatures above 50 °C, wax residue in blind channels can soften and reflow, contaminating clear optical windows. This is a critical threshold risk in production.

    Safety Data Sheets for the individual feedstocks are maintained under REACH and RoHS obligations. The composite printed part is a fabricated article, not a separately registered mixture; regulatory compliance is assessed on the final article configuration. If the part is intended for medical device contact, ISO 10993-1:2018 evaluation is the responsibility of the device manufacturer, and published data for this specific multi-material configuration is limited.

    Using the Compliance Matrix for CR-WT 200 and CR-CL 200 Documentation

    The following matrix identifies the test methods commonly referenced for the base resins and the limitations when applying them to a blended multi-material state. The absence of a single composite value in the manufacturer’s published datasheets does not indicate non-compliance; it indicates that the composite state is variable across voxel ratios and build orientations.

    Verification matrix for the VisiJet RWT-RCL-R78 composite build state
    PropertyTest methodApplication boundary
    Tensile strength and elongationASTM D638-14; ISO 527-2:2012Valid for base resins only; composite values are blend-ratio dependent
    Flexural modulusISO 178:2019; ASTM D790-17White-clear interface stiffness requires a printed sandwich coupon
    Shore D hardnessASTM D2240-15Nominal R78 target; surfaces must be flat and at least 6 mm thick
    Heat deflection temperatureASTM D648-18Use 0.455 MPa condition; composite HDT is not a linear blend value
    Light transmittance and hazeASTM D1003-21Clear phase only; adjacent white domains increase interface haze
    Izod impactASTM D256-23Notch position must be recorded relative to the material transition
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