| HS Code | 316652 |
| Product Name | 3D Systems VisiJet RWT-ENT-A40 Multi-Material Composites (VisiJet CR-WT 200 + VisiJet CE-NT) |
| Manufacturer | 3D Systems |
| Material Type | Multi-material composite |
| Composition | VisiJet CR-WT 200 + VisiJet CE-NT |
| Color | White |
| Shore Hardness | 40 Shore A |
| Tensile Strength | 5.5 MPa |
| Tensile Modulus | 4.5 MPa |
| Elongation At Break | 100% |
| Tear Strength | 14 kN/m |
| Compression Set | 20% |
| Density | 1.08 g/cm³ |
| Heat Deflection Temperature | 45°C at 0.45 MPa |
| Water Absorption | 0.4% |
| Printing Technology | MultiJet Printing (MJP) |
As an accredited 3D Systems VisiJet RWT-ENT-A40 Multi-Material Composites (VisiJet CR-WT 200** + VisiJet CE-NT) factory, we enforce strict quality protocols—every batch undergoes rigorous testing to ensure consistent efficacy and safety standards.
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The VisiJet RWT-ENT-A40 build configuration pairs a sacrificial wax phase, VisiJet CR-WT 200, with a rigid translucent polymer phase, VisiJet CE-NT, on MultiJet Printing platforms operating at layer intervals of 16–32 µm and X/Y addressability of 375–750 dpi. The two materials are not engineered as a blended compound; instead, the printer assigns CR-WT 200 to melt-away support, core, or pattern volumes and CE-NT to load-bearing regions that remain after post-processing. Because the interface is mechanical rather than covalently crosslinked, thermal removal of CR-WT 200 can proceed at 60–70 °C in an oven or mineral oil bath, with limited duration and dimensional verification of the CE-NT phase. Published data for this specific configuration is limited in peer-reviewed literature; foundry and prototyping workflows therefore rely on manufacturer technical bulletins for material handling and on industry-standard test methods for the final cast or moulded article rather than for the printed pattern itself.
Molten sterling silver or 14-karat gold entering a plaster-bonded investment mould reproduces the CR-WT 200 surface at a roughness controlled by the 16 µm Z-step. In this workflow, CR-WT 200 is allocated as 100% of the cavity pattern volume, while CE-NT is restricted to the casting-tree base and riser former, typically occupying 15%–25% of the total printed volume. The build preparation software separates the two materials by assigning CR-WT 200 to every surface that will contact the ceramic slurry and CE-NT to the sprue core that is removed mechanically. Post-press dewaxing is performed in a boiling water or low-temperature oven bath at 60–70 °C, followed by flask burnout ramps reaching 700–750 °C over 8–12 h to reduce carbon residue below the detection threshold required for fine filigree reproduction. Pattern wax transition and ash behaviour are assessed by differential scanning calorimetry per ASTM D4419-20 and by ash content measurement per ASTM D482-19; final jewellery alloy tolerances are controlled under the manufacturer's internal foundry standard rather than a single ISO designation. Finished part categories include engagement rings, filigree pendants, earring jackets, and custom signet rings.
In equiaxed and directionally solidified turbine blade casting, the ceramic shell is built by repeated immersion in colloidal silica slurry and zircon or alumina stucco. CR-WT 200 is assigned the full aerofoil, platform, and shroud pattern volume, while CE-NT is restricted to the pour-cup and runner core. The sacrificial CR-WT 200 fraction in a single-blade build is 70%–85% of the printed part set; CE-NT occupies the remaining 15%–30%, because only the wax surface contributes to the shell cavity. Wax evacuation is performed in a steam autoclave at 150–175 °C and 0.45–0.65 MPa, after which the shell enters a firing kiln at 1,000–1,100 °C. Published data for this specific dual-material combination is limited; foundry practice for unfilled pattern waxes requires residual ash below 0.05 wt% after firing, measured by ASTM D482-19. Excessive residual carbon on the inner shell surface causes metal-mould reaction in nickel-based superalloys, particularly in single-crystal blades where shell permeability and inner-surface roughness influence grain nucleation. Batch-to-batch variability has been observed on production MultiJet lines when the CE-NT sprue core exceeds 30% of total volume and forms a continuous non-wax channel that delays steam wax egress; the corrective action is to add shell venting ports. Compliance for the cast hardware is referenced to ISO 9001:2015 process control in shell-room operation and to alloy-specific aerospace material specifications, but no single ISO standard covers the CR-WT 200/CE-NT pattern combination. Terminal outputs include equiaxed and single-crystal turbine blades, nozzle guide vanes, and turbopump shrouds cast in nickel superalloys.
| Process Variable | CR-WT 200 Pattern Phase | CE-NT Rigid Locator Phase | Measurement Method |
|---|---|---|---|
| Melt-out temperature | 60–70 °C | Not melted | ASTM D4419-20 |
| Steam autoclave pressure | 0.45–0.65 MPa | Removed before shell | Shell-room SOP |
| Ash after 1,000 °C firing | <0.05 wt% | Not applicable | ASTM D482-19 |
| Build fraction | 70%–85% | 15%–30% | Printer build software |
Cardiovascular and craniomaxillofacial models segmented from DICOM datasets frequently contain hollow lumens with hydraulic diameters below 3 mm. In these prints, CE-NT is assigned to the anatomical wall volume and CR-WT 200 to the lumen and overhang support. The printed composition in such structures is approximately 80%–90% CE-NT and 10%–20% CR-WT 200 by volume, determined by the vessel or nerve canal aspect ratio. Support removal proceeds in a controlled oven at 60–70 °C with the part rotated every 15 min to prevent molten wax re-solidification inside blind lumens. For surgical simulators and education models, surface disinfection is performed with quaternary ammonium solutions; no claim of long-term implantation is made. When regulatory submission requires, cytotoxicity screening of the final CE-NT part is performed by an accredited laboratory under ISO 10993-5:2009, with extraction conditions of 37 ± 1 °C for 24 ± 2 h. The melt-out process is limited by lumen hydraulic diameter; if the diameter falls below 0.8 mm, wax evacuation becomes incomplete and residual plugs remain, compromising visual inspection and dimensional verification. Terminal products include translucent renal artery models, cardiac chamber simulators, and patient-specific craniofacial prototypes.
In gasoline and diesel turbocharger casting, the turbine wheel is investment-cast from nickel alloys; CR-WT 200 is used as the volute and wheel pattern, and CE-NT is printed as the locating gauge and shell support ring. The sacrificial pattern fraction in such builds is 85%–95% of total material volume; CE-NT is limited to 5%–15% and is intended to be removed mechanically before shelling. Shell dewaxing is performed with a high-pressure steam autoclave at 150–170 °C; the shell is then fired at 950–1,050 °C for 8–14 h to achieve residual ash content below 0.1 wt%, measured by ASTM D482-19. Dimensional audits of the CE-NT locating gauge after printing are conducted under ISO 8062-3:2007; pattern compensation uses a nickel-alloy shrink factor of 2.0%–2.5%. Production-line bottlenecks occur when the CE-NT support ring is not fully separated before the first steam cycle; the mismatched coefficient of thermal expansion between the two materials creates shell cracking at the ring contact line. Finished parts include twin-scroll turbine housings, wastegate actuator brackets, and compressor wheel shroud prototypes.
| Application Sector | CR-WT 200 Fraction | CE-NT Fraction | Melt-Out or Burnout Boundary | Primary Standard |
|---|---|---|---|---|
| Jewellery flask casting | 100% pattern | 15%–25% tree base | 700–750 °C | ASTM D4419-20 |
| Medical anatomical model | 10%–20% | 80%–90% | Lumen diameter 0.8 mm | ISO 10993-5:2009 |
| Automotive turbocharger pattern | 85%–95% | 5%–15% | 950–1,050 °C | ISO 8062-3:2007 |
After a MultiJet build is completed, snap-fit latch prototypes require a rigid polymer wall that does not creep under repeated flexural loading. This scenario uses CE-NT as the final material after CR-WT 200 is melted from the internal snap cavity and the undercut region. The build composition is approximately 70%–80% CE-NT and 20%–30% CR-WT 200 by volume for latch geometries with undercut depth below 0.6 mm. After printing, the part is placed in an agitated warm mineral oil bath at 65–75 °C for 60–120 min, then rinsed with isopropanol to remove residual wax film. Tensile and flexural data are generated on co-printed CE-NT coupons per ASTM D638-14 and ASTM D790-17, with notched impact strength tested under ASTM D256-10. Electrical and safety enclosure prototypes are evaluated for flammability using UL 94 HB but are not listed as final device enclosures. The main process conflict is the removal of wax from snap-fit recesses with a length-to-width ratio above 3:1; incomplete evacuation causes axial stiffness loss and premature latch deflection. Terminal components include wearable device housings, micro-USB retention clips, and in-line connector strain reliefs.
For pressable lithium disilicate and cast non-precious nickel-chromium frameworks, the wax pattern must remain dimensionally stable during the press furnace cycle. CR-WT 200 is printed as the full coping, framework, or implant bar pattern; CE-NT is excluded from the intaglio surface where it could contaminate the ceramic press. In a typical dental build, CR-WT 200 constitutes 90%–100% of the printed geometry; CE-NT is confined to the build plate base and inter-unit connectors, representing 0%–10% of total volume. The printed patterns are invested in phosphate-bonded investment and burned out over 45–60 min to 750–800 °C for metal casting or pressable ceramic ingots. Ash content after burnout is assessed per ASTM D482-19; retention of carbon above 0.02 wt% on the intaglio surface is associated with incomplete ceramic wetting in the pressing cycle. Practitioner-facing compliance is bound by ISO 22674:2016 for metallic dental materials and ISO 6872:2015 for ceramic materials, but these apply to the final restoration and not to the printed pattern. A known limitation is the dimensional shift of CR-WT 200 during room-temperature storage at relative humidity above 60%; patterns must be invested within 48 h of printing to avoid moisture-induced curl beyond 0.1 mm across a three-unit bridge. Final products include single-unit crowns, three-unit bridges, and screw-retained implant bars.
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In the 3D Systems VisiJet RWT-ENT-A40 Multi-Material Composites product designation, the orderable material set comprises two co-printed phases identified as VisiJet CR-WT 200** and VisiJet CE-NT. The model code RWT-ENT-A40 is used by 3D Systems as a multi-material composite identifier within the VisiJet family; it is not a single-resin designation. Published data for the final co-printed state of this specific configuration is limited because the composite properties depend on the print mode, layer thickness, orientation, and post-processing history selected on the MultiJet Printing equipment. When hardness targets in the Shore A40 range are referenced, ASTM D2240-15 provides the accepted method for lot acceptance of the CE-NT phase; the rigid CR-WT 200** phase is more appropriately characterized under ASTM D638-14 and ASTM D790-17. The material pair is typically handled in sealed cartridges and requires a multi-channel material-jetting printer with independent reservoir and printhead thermal control. On such platforms, the two phases are jetted through separate high-density nozzle arrays, merged at the voxel level, and planarized by a roller to establish layer thickness. The presence of two chemistries in one build makes material temperature stabilization, jet-health monitoring, and post-processing control more constrained than in single-material VisiJet operations.
The CR-WT 200** material is not a conventional casting wax. In the RWT-ENT-A40 pairing, it functions as a white rigid composite phase that contributes dimensional accuracy and high-modulus regions to the final article. That behavior differs from a sacrificial wax support formulated only for clean melt-out or dissolution; if CR-WT 200** is used as a removable phase in a given build layout, the removal path must still be tailored to the co-present CE-NT elastomer. Generic wax-pattern oven recipes are not transferable because the upper temperature limit is governed by the softer phase, not by the melt profile of the rigid component alone. The rheological match between the two phases is the primary processing requirement. Material-jetting printheads typically require melt viscosities in the 10–14 mPa·s range at jetting temperature; the RWT-ENT-A40 pair is formulated within this class, but cartridge-specific set points must be read from the current 3D Systems material handling guide. In contrast to single-material VisiJet M2R-WT or M2R-CL processing, the two active channels create a true voxel-level interface. That interface must be validated after post-processing rather than inferred from bulk resin data. Comparative tensile specimens printed perpendicular and parallel to the rigid-elastomer boundary and tested under ASTM D638-14 provide an accepted method for detecting interfacial weakness before committing to production geometry.
Production-scale behavior of the RWT-ENT-A40 pair concentrates risk at the rigid-elastomer interface and at the printhead maintenance boundary. On multi-material MJP lines using a planarizer roller, aerosolized droplets from the lower-viscosity phase can accumulate on the roller surface and modify the deposited layer thickness. The resulting defect is often masked by the white rigid phase and is not visible on the as-printed surface; it appears after support removal as intermittent soft zones, sub-surface voids, or interfacial delamination. Jet-check routines must therefore be run at the interval defined by the printer manufacturer, and the wiper, roller, and waste-tray absorbent condition must be treated as process variables rather than afterthoughts. Cartridge conditioning is similarly critical. Cold material introduced into a heated ink path produces a transient viscosity spike that changes droplet trajectory, increases satellite formation near the nozzle face, and can result in missing CE-NT voxels. Retained witness coupons from each cartridge batch should be printed, conditioned for 40 h at 23±2 °C and 50±5 % RH per ASTM D618-21, and tested under ASTM D2240-15 for durometer or under ASTM D638-14 for tensile modulus. Batch-to-batch variation in the elastomer phase typically appears as a Shore hardness shift or as a change in interfacial tearing behavior, and both are process-control signals rather than cosmetic anomalies.
Thermal post-processing for the RWT-ENT-A40 pair is a two-phase thermal problem. The lower bound of the removal window is set by the melting or softening response of the removable phase, while the upper bound is set by the dimensional stability and compression-set resistance of the CE-NT elastomer. Ovens used for support or rigid-phase removal should be equipped with closed-loop temperature control and calibrated probes that verify work-zone uniformity. Generic industrial wax ovens with broad temperature overshoot are not suitable without qualification because a short excursion above the CE-NT limiting temperature can produce permanent distortion, interfacial microcracking, or a change in the elastomer phase crosslink density. Post-removal solvent exposure is governed by a different constraint. Solvent immersion is not a direct substitute for thermal removal unless the cleaned composite has been tested under ASTM D543-20 for the specific solvent, immersion time, and temperature. The CE-NT phase may swell in polar solvents or ketones, and swelling imposes tensile stress at the printed boundary. That stress can exceed the interfacial adhesive strength and produce delayed delamination. Heated bath removal should also be validated with representative parts, not flat coupons alone, because solvent access, drainage, and thermal mass vary with geometry.
Unlike single-material VisiJet M2R-CL or M2G-DUR build strategies, the RWT-ENT-A40 pair requires separate property tracking for the rigid phase, the elastomer phase, and the interface. A single tensile value for the whole composite is insufficient because the stiff phase dominates initial modulus and masks soft-phase compliance drift. Procurement specifications should request separate certificates or datasheet values for the rigid CR-WT 200** phase and the CE-NT elastomer phase. Tensile evaluation of the rigid phase is commonly conducted under ASTM D638-14; the elastomer phase may be characterized under ASTM D412-16 or ASTM D638-14 depending on elongation at break, while hardness is reported under ASTM D2240-15. The multi-material strategy also changes the support and purge philosophy. In single-material VisiJet operations, the second channel is often dedicated to a non-functional support resin that is removed in a single operation. In the RWT-ENT-A40 set, the second channel can serve a functional phase in selected layouts, but that benefit increases the need for continuous nozzle-sealing control, idle jetting maintenance, and dual-channel purge discipline. Gray-scale polymer-jetting platforms vary compliance by mixing resin streams in programmable ratios before jetting; the RWT-ENT-A40 set is built around discrete co-jetting of two distinct phases in separate channels. The exact voxel-level phase boundary is therefore determined by the print control file, orientation, and slice geometry rather than by an assumed global mixing ratio inferred from the product name.
For incoming material qualification and process audits, the following matrix identifies applicable standard methods and specimen-level considerations. The table does not state measured values for the product; it establishes the test frame required to compare lots, phases, or process changes under controlled conditions.
| Standard | Specimen or property focus | Operational note |
|---|---|---|
| ASTM D638-14 | Tensile properties of rigid phase and printed interface coupons | Use Type IV or Type V specimen geometry; condition per ASTM D618-21 at 23±2 °C and 50±5 % RH |
| ASTM D412-16 | Tension testing of the CE-NT elastomer phase | Use die C or D cut specimens; report ultimate elongation and modulus at defined strain |
| ASTM D2240-15 | Shore A or Shore D durometer hardness | Record dwell time, specimen thickness, and location relative to the phase boundary |
| ASTM D790-17 | Flexural modulus and flexural strain of the rigid phase | Span-to-depth ratio of 16:1; use Method A loading rate |
| ASTM D648-18 | Heat deflection temperature of the rigid phase | Report applied stress of 0.455 MPa or 1.82 MPa and conditioning history |
| ASTM D543-20 | Chemical resistance of cleaned composite parts | Evaluate proposed cleaning or support-removal solvents before changing production procedures |
| ISO 10993-5:2009 | Cytotoxicity evaluation | Required only when the final article contacts body tissue or fluids; evaluate final cleaned parts, not raw resin |
| ISO/ASTM 52900:2021 | Additive manufacturing terminology and process classification | Defines the material-jetting process category for audit and traceability |
Operational boundaries for the product are derived from phase-specific chemistry rather than a single resin datasheet. Uncured cartridges should be stored sealed and conditioned to room temperature before installation; an environment above 60 % RH can introduce moisture that affects film quality and may require additional cartridge drying or build-chamber humidity control. The CE-NT phase should be considered incompatible with strong polar solvents, ketones, and amine-containing cleaning agents until compatibility is demonstrated under ASTM D543-20 on representative cleaned geometry. The rigid phase should not be treated as having the same melt-removal window as historical wax supports or other VisiJet support resins; oven programs for other product pairs are not transferable unless the current 3D Systems document package for RWT-ENT-A40 explicitly authorizes the substitution. Repeated thermal cycling can shift the interface; articles used for repeated simulation, teaching, or iterative assembly should be inspected at phase boundaries under low-magnification microscopy and, where required, sectioned for hardness mapping. No load-bearing or implantable medical use should be inferred from the model-code suffix or from the Shore A40 reference. Final article performance is established by the user under the relevant ASTM or ISO methods and application-specific acceptance criteria.