| HS Code | 811218 |
| Product Name | 3D Systems VisiJet RWT-ENT-A50 Multi-Material Composites (VisiJet CR-WT 200 + VisiJet CE-NT) |
| Material Type | Multi-material composite photopolymer |
| Composition | VisiJet CR-WT 200 rigid white + VisiJet CE-NT elastomeric natural transparent |
| Blend Ratio | A50 (approximately 50% rigid / 50% elastomeric) |
| Color | White/translucent |
| Tensile Strength | 14.5 MPa (typical) |
| Elongation At Break | 45% (typical) |
| Flexural Modulus | 600 MPa (typical) |
| Hardness | 70 Shore D (typical) |
| Heat Deflection Temperature | 55°C at 0.45 MPa (typical) |
| Density | 1.10 g/cm³ (typical) |
| Water Absorption | 0.4% (typical) |
| Tear Strength | 25 kN/m (typical) |
| Izod Impact Strength | 50 J/m (typical) |
As an accredited 3D Systems VisiJet RWT-ENT-A50 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 RWT-ENT-A50 multi-material route pairs VisiJet CR-WT 200 as the jetted build phase and VisiJet CE-NT as the sacrificial support phase. Downstream application behaviour is governed not by generic part type but by the process boundary where the support phase is removed, the pattern is burned out, and the resulting cavity is filled with alloy, ceramic, or polymer. Dimensional stability during investment expansion, lot-to-lot melting range, and burnout residue are the controlling variables. Where a product-specific value is not public, the validation requirement is stated instead of a fabricated performance figure.
Removable partial denture frameworks are cast in cobalt-chromium-molybdenum alloys under ISO 22674:2016. The printed set consists of CR-WT 200 clasps, lingual plates, and major connectors with CE-NT support placed on polishing and non-tissue surfaces. On production lines, the first relevant failure mode is thermal yielding of thin clasp tips during support melt-out because a static oven can show more than 5 °C tray gradient across a batch. A circulating bath with an immersion rack is therefore used, and dwell time is determined by the largest support-connected cross-section rather than by part count. After removal, each framework pattern is inspected at 10x stereomicroscopy for residual CE-NT; a retained support film at the tissue side of a lingual bar becomes a gas defect during casting. The wax pattern is invested in vacuum-mixed phosphate-bonded investment, poured under vibration, and allowed to set for 45–60 min. Burnout is a two-stage ramp in a digitally controlled furnace: the first plateau at 250–300 °C eliminates the bulk of the pattern under oxygen, and the second plateau at 850–950 °C conditions the mold for casting. Ash residue is the lot acceptance criterion most likely to vary between CR-WT 200 lots; if the supplier certificate lacks a specific residue figure, a blind test flask is run before production. Castings are devested and blasted with 110–125 µm alumina at 3–4 bar, then adapted to the master die. A batch-to-batch shift in CE-NT melting range of a few degrees can alter support removal dwell by 5–10 min; thermocouple verification of the bath set-point is therefore part of the morning line check.
Jewellery microcasting imposes a stricter surface-defect threshold than dental frameworks because final acceptance is judged on polished rail surfaces, pavé seat geometry, and thin gallery wire. In this application, CR-WT 200 is used for filigree rings, pendant frames, and stone-set bars, while CE-NT is jetted into internal undercuts. Support removal is the first critical step: filigree sections under 0.4 mm can deform if the bath is set too close to the pattern softening point, and retained support in gallery wire is the dominant source of gas porosity during direct flask casting. A circulating melt-out bath is preferred over an oven because the liquid medium removes support wax from narrow cavities while keeping the part below deformation temperature. After melt-out, the pattern is cleaned with 99.8% isopropanol and inspected at 10x before tree assembly. The tree is mounted on a central wax sprue with stick wax and invested in a gypsum-bonded investment formulated for precious metals. Burnout is typically ramped to 730 °C and held 2–4 h for small-to-medium flasks; the hold time must be validated for multi-flask benches and heavy trees. Casting of 18 ct gold, 925 silver, or platinum group alloys is performed by vacuum-assisted torch or centrifugal casting; palladium white gold requires inert cover gas. Precious metal fineness and assay are handled under ISO 9202:2019; dimensional acceptance of stone seats is verified with gauge pins and setting burrs. The material set is not appropriate for enclosed hollow pieces with restricted drain holes because CE-NT evacuation cannot be optically confirmed.
Pressed lithium disilicate and other heat-pressed ceramic restorations use the jetted pattern as a positive sacrificial form for the press investment cavity. The pattern is fabricated from CR-WT 200 with CE-NT supports placed away from marginal and incisal edges. After support melt-out, the pattern is seated on a die and invested in a phosphate-bonded press investment mixed under vacuum; the expansion of the investment is matched to ceramic ingot shrinkage, and the burnout ramp must remove pattern material without leaving carbon in narrow embrasures. Pressing furnaces for lithium disilicate operate above 900 °C; the pressed restoration is evaluated under ISO 6872:2015 for flexural strength and chemical solubility. A recurrent production defect is marginal over-expansion from a non-uniform burnout ramp, which opens the cervical edge; production control uses a flask thermocouple profile rather than furnace set-point alone. Because ceramic pressing requires a clean internal cavity, residual CE-NT in interproximal embrasures is not acceptable. The MJP route is selected where hand waxing cannot reproduce 0.3 mm axial wall thickness across multi-unit anterior cases or where calibrated cutback is needed for veneering ceramic. Published data for this specific RWT-ENT-A50 combination in pressable ceramic systems is limited; each investment brand and pressing furnace combination is qualified with a single-unit test pattern before multi-unit production.
Master patterns for room-temperature-vulcanising silicone molds are a low-volume segment where surface chemistry and inhibition dominate. CR-WT 200 and CE-NT residues can interfere with platinum-catalysed RTV cure, so the pattern is cleaned with 99.8% isopropanol and dried with filtered air below 40% relative humidity before mold construction. The surface is checked for tack-free condition; any uncured support film must be removed because it inhibits the silicone at the pattern interface. The silicone is vacuum-degassed in a chamber capable of 5 mbar absolute pressure and poured over the pattern in a controlled stream to avoid entrapped air at inverse draft features. After cure, the mold is cut on parting lines, and the CR-WT 200 original is removed; the pattern may be retained as a master if stored below the material softening point and away from pressure. Final parts cast from the RTV mold are often rigid polyurethane or epoxy, with hardness checked under ASTM D2240-15 and tensile properties under ASTM D638-14. Published data for this RWT-ENT-A50 configuration in platinum-silicone tooling is limited; a lab-scale inhibition coupon is mandatory before a full mold. The principal bottleneck is not MJP build time but cleaning of undercuts where CE-NT can lodge and prevent silicone wetting.
Low-volume surgical instrument components—forceps jaws, hemostat bodies, and laparoscopic dissector tips—are investment cast in austenitic stainless steel grades under ASTM F899-20. The RWT-ENT-A50 set produces sacrificial patterns for trial batches before hard tooling; printed CR-WT 200 geometries are assembled on a wax tree with 6–10 mm spacing between small parts. CE-NT is removed before the first ceramic slurry coat because any residual support in joint recesses expands during shell firing and creates voids. The shell is built with 6–8 coats of colloidal silica slurry and alumina or zircon stucco, with drying controlled by humidity and air velocity. The dewax step uses a steam autoclave or flash furnace; pattern material must not expand faster than the green shell at thin edges. After dewax, the shell is fired at 850–1,050 °C, then cast with induction-melted alloy. As-cast fit is checked by gauge dimensions, and surface integrity is evaluated by penetrant inspection under ASTM E1417/E1417M-21. Passivation is carried out in citric or nitric acid according to ASTM A967/A967M. The main limitation of the jetted-wax route in this segment is part size and shell process compatibility: larger instrument bodies may exceed the build envelope or require wax-welded sectioning. Product-specific expansion data for CR-WT 200 under rapid autoclave dewaxing has not been published; a sacrificial shell trial is necessary for each new geometry family.
| Application zone | Standard | Inspection/control target |
|---|---|---|
| Co-Cr removable partial denture frameworks | ISO 22674:2016 | Metallic dental restorative material requirements |
| Jewellery precious-metal casting | ISO 9202:2019 | Fineness ranges for gold, silver, platinum alloys |
| Pressed lithium disilicate restorations | ISO 6872:2015 | Flexural strength and chemical solubility of dental ceramics |
| RTV silicone tooling | ASTM D2240-15, ASTM D638-14 | Hardness and tensile control for final polyurethane/epoxy parts |
| Surgical stainless steel investment casting | ASTM F899-20, ASTM E1417, ASTM A967 | Alloy designation, penetrant inspection, passivation |
| Prototype turbine blade shell casting | ASTM E192-20 | Radiographic acceptance of investment castings |
Prototype nickel-based turbine blades and nozzle guide vanes are investment cast from jetted wax when production wax injection tooling is not yet committed. In this application, CR-WT 200 forms the airfoil, platform, and root geometry; CE-NT supports overhanging shroud and serration regions. The ceramic shell system is usually a colloidal silica-alumina or zircon-based shell of high green strength, and pattern removal is carried out by steam autoclave dewaxing. Industrial autoclave cycles in this segment commonly operate at 150–170 °C and 5–7 bar; however, the specific RWT-ENT-A50 pattern expansion behaviour under those conditions is not fully covered in open literature, so the first article must be run with a slower pilot ramp. Shell cracking at trailing-edge ceramic edges and core shift in internally cooled configurations are the dominant failure modes. Once dewaxing is complete, the shell is fired at 1,000–1,100 °C and cast with nickel-based superalloy. Final casting soundness is evaluated radiographically under ASTM E192-20 and by penetrant inspection after heat treatment. The jetted wax route is limited to prototype and short-run castings where the pattern count does not justify hard injection tooling; full production turbine hardware remains in conventional wax injection because of cycle time and pattern cost. Dimensional data for this specific material combination in high-pressure turbine geometries is not available publicly; surface finish and shell strength acceptance are therefore validated per casting house practice.
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Within the MultiJet Printing materials portfolio, the 3D Systems VisiJet RWT-ENT-A50 Multi-Material Composites is not a single resin but a paired cartridge set. The order code combines VisiJet CE-NT, an elastomeric natural-translucent part material, with VisiJet CR-WT 200, a melt-away wax support. The trailing A50 designation is aligned with a target indentation hardness of 50 Shore A for the CE-NT part after post-processing, as measured under ASTM D2240-15. The support material is mechanically sacrificial and is formulated for the low-modulus CE-NT part rather than for rigid MJP photopolymers. The material set is intended for MultiJet Printing platforms that accept dual-material elastomer/wax cartridges, including the ProJet MJP 2500 Plus class of equipment. In this configuration, the wax and elastomer are jetted through separate printhead channels and cured by integrated ultraviolet exposure.
The CE-NT part material produces flexible, translucent sections with Shore A hardness in the 50 range. Candidate geometries include soft-touch grips, gaskets, bellows, sealing surfaces, flexible duct prototypes, and overmold-like covers. Because the material is translucent, optical clarity depends on wall thickness and internal stress distribution; abrupt cross-section changes can create visible stress-whitening and non-uniform light transmission. Parts produced from the A50 set should be evaluated as elastomeric structures, not as rigid acrylic or epoxy-like MJP components. The published mechanical data for CE-NT is generated from test prints produced on the recommended platform using the manufacturer’s defined print profile.
CE-NT is characterized under tensile, tear, and indentation-resistance protocols. The primary standard for tensile strength and elongation is ASTM D638-14; tear strength is evaluated under ASTM D624-00, and hardness under ASTM D2240-15. Datasheet values for CE-NT typically place tensile strength in the low single-digit megapascal range, with elongation-at-break exceeding 200% and tear strength in the 15–20 kN/m range. The exact values depend on print orientation, wall thickness, post-processing temperature, and the age of the material cartridge. Published data for this specific RWT-ENT-A50 bundle configuration is limited to the manufacturer’s controlled material-profile dataset; users should verify properties on printed coupons at the intended orientation and layer thickness. The CR-WT 200 support is not rated for mechanical performance. Its functional properties are melt-removal temperature, ash or residue after removal, dimensional compatibility with CE-NT during thermal processing, and storage stability under ultraviolet-shielded conditions. The wax support is not a substitute for the VisiJet M2 SUP support system used with rigid M2R materials.
On a ProJet MJP 2500 Plus platform with a build envelope of 294 mm × 211 mm × 144 mm, the A50 set is installed as separate heated material cartridges. The printer’s resolution is specified as 800 dpi × 900 dpi in the X/Y plane, with a native Z-resolution of 790 dpi and a layer thickness on the order of 32 µm for fine-profile rigid materials. The CE-NT profile may use a different layer height selected automatically by the printer firmware. Build chamber temperature, printhead temperature, and ultraviolet output are controlled by the machine profile and are not user-adjustable. Because CE-NT is a soft elastomer, ejection forces during part removal can induce local deformation. Operators should allow the build tray to reach the prescribed removal temperature before separating parts from the wax mass. Cartridge handling should minimize exposure to ambient ultraviolet lighting and moisture; the wax support is sensitive to prolonged temperatures above its storage specification. The manufacturer’s cartridge shelf-life and storage temperature limits should be followed to avoid viscosity drift and jetting channel blockage.
Material handling and compliance boundaries for the A50 set are governed by the safety data sheets and the printer manufacturer’s cartridge lifecycle documentation. Unprocessed CE-NT and CR-WT 200 should be stored in shielded containers at temperatures within the manufacturer’s range, typically between 15 °C and 30 °C, and should not be returned to production after exposure below recommended minimum transport temperatures. Part material that exhibits gelation, separation, or color shift should be rejected. The support wax can settle if stored motionless for extended periods; cartridge agitation may be specified but should follow the manufacturer’s cartridge preparation procedure. In mixed-material machine cells, cross-contamination between the wax support and M2 SUP support can be detected by melt-point shift or by residue accumulation in post-processing baths. Industrial material declarations may reference RoHS 2011/65/EU and REACH 1907/2006; the user must verify that the specific lot carries the required declaration for the target market. The uncured material is not rated for food-contact end use, and users requiring medical, food-contact, or skin-contact compliance must verify the final printed article under application-specific regulations such as ISO 10993-5 or FDA 21 CFR 175.300 as applicable. The base MJP material declarations generally support industrial use; they do not automatically confer end-use medical-grade status.
CR-WT 200 is removed by thermal melt-out and not by manual breakout in the RWT-ENT-A50 workflow. The recommended post-processing sequence typically begins with a heated oven or wax-removal unit set below 60 °C, followed by a warm ultrasonic bath using a process oil or aqueous detergent specified by the printer manufacturer. The required dwell time is influenced by part cross-section, support mass, and the density of internal channels. Thick elastomeric sections with embedded support retain heat differently than thin walls and may require staged heating to prevent localized swelling or surface marring. CE-NT parts can recover as-printed dimensions after support removal if thermal exposure is controlled; however, parts that are stretched or scraped during warm-wax extraction may retain residual strain. Solvent cleaning should avoid ketone-based and chlorinated solvents, which can swell the low-crosslink-density elastomer. Alcohol-based surface cleaning may be used only after verification on a non-critical part. The support removal equipment must be dedicated or thoroughly cleaned because wax carryover into other post-processing tanks can change bath surface tension and contaminate rigid MJP parts in mixed-production cells.
Comparative property data for the A50 elastomer and a representative rigid MJP material are shown in Table 1. The ranges are based on published datasheet values and test coupons printed under default manufacturer profiles.
| Property | VisiJet CE-NT / RWT-ENT-A50 | VisiJet M2R-WT reference | Test method |
|---|---|---|---|
| Indentation hardness | 50 Shore A target | 80 Shore D range | ASTM D2240-15 |
| Tensile strength | 2–3 MPa range | 40–50 MPa range | ASTM D638-14 |
| Elongation at break | 200–300% | 8–10% | ASTM D638-14 |
| Tear strength | 15–20 kN/m | Not applicable or not stated | ASTM D624-00 |
| Support material | VisiJet CR-WT 200 wax | VisiJet M2 SUP | Product-specific |
Design rules for the A50 elastomeric grade follow from the low tensile modulus and Shore A 50 hardness. Snap-fit tabs, press-fitting pins, threaded bosses, and self-tapping screw features that perform adequately in rigid M2R-WT frequently fail or loosen when produced in CE-NT because the material deforms at lower insertion force and does not retain thread engagement in the same manner. Thin sections below approximately 1 mm may collapse or deform under their own mass unless supported by the wax during printing and post-processing. Sharp internal corners and notches concentrate tear energy; tear strength under ASTM D624-00 becomes a more relevant design limit than tensile strength in such geometries. Multi-cycle flexural fatigue performance of CE-NT is not fully covered by published datasheets. Users intending dynamic flexing or repetitive compression should run production-like coupon tests under the intended displacement or force control. Continuous exposure to hot water, steam, or polar solvents above ambient temperature should be avoided because the elastomer matrix has lower thermal and hydrolytic stability than rigid MJP grades.
Build orientation directly affects mechanical anisotropy in CE-NT. Parts built with tensile axes parallel to the X/Y plane typically show higher elongation and tear resistance than parts built perpendicular to the print plane, because interlayer interfaces function as weak planes for tear propagation. Supports are more difficult to remove from downward-facing surfaces; operators should design sacrificial surfaces and orient critical sealing faces away from the support-prone side. The tear energy required to propagate a crack along a layer interface may be below the bulk tear strength measured on standard dogbones. Published data for this specific configuration is limited; orientation-specific testing under ASTM D624-00 is required for critical applications. The wax support’s thermal expansion can create differential stress during the melt-out stage if large elastomeric pads are surrounded by confined wax reservoirs. A staged thermal ramp rather than direct immersion into a preheated bath is used in some production cells to reduce warpage.
Under continuous production, the CE-NT and CR-WT 200 combination introduces operational failure modes not seen with rigid MJP materials. The most frequently reported issues are wax entrapment inside blind elastomeric channels and localized wall collapse during heated support removal. Blind channels without a drainage path can retain wax even after the standard melt-out cycle because the low modulus of CE-NT does not permit aggressive manual wax removal without surface damage. Production layouts should provide multiple melt-out openings and avoid fully enclosed hollow volumes unless the part is intended to be cut open. Ultrasonic tanks with high cavitation intensity can erode the outer skin of thin elastomer walls; this is more pronounced when the bath is operated above the manufacturer’s recommended temperature range. Mixed-lot parts that combine thick and thin sections in one basket may experience non-uniform cleaning because the thick sections shadow the thin sections from cavitation.
Incoming lot validation for the A50 set should include a fixed build job containing horizontal and vertical tensile specimens. Horizontal and vertical specimens can detect orientation-dependent strength loss before production parts are committed. For each lot, the Shore A hardness under ASTM D2240-15 should remain within the manufacturer’s acceptance band around 50; excursions above the upper bound may indicate premature crosslinking, while excursions below the lower bound may indicate incomplete cure or contamination. The CR-WT 200 support lot can be evaluated for melt-out time and residue mass using a standardized coupon block. Increases in melt-out time beyond the established control limit can indicate batch-to-batch variation or moisture intrusion.
The operational difference between the A50 composite set and rigid MJP materials is not limited to hardness. A rigid VisiJet M2R-WT part under ASTM D638-14 typically fails at low elongation with a brittle or semi-brittle fracture surface. In contrast, a CE-NT part reaches large strains before rupture, and the dominant design failure is usually tear propagation from a notch or surface defect. This shift in failure mode means that fillet radii, gate vestige removal, and surface scoring from post-processing tools have a greater effect on CE-NT part life than on rigid MJP components. Support selection is equally distinct: the CR-WT 200 wax in the A50 set is matched to the CE-NT elastomer’s thermal expansion and surface energy, whereas the M2 SUP support used with M2R rigid materials is not validated for the elastomer/wax build profile. Attempting to interchange support cartridges can produce jetting anomalies, poor layer coalescence, and difficult support removal. In low-volume production of soft grippers or sealing prototypes, the A50 set can replace cast silicone tooling for form-and-fit evaluation, but it does not replicate the long-term dynamic properties of compression-molded silicone elastomers. Direct substitution of compression-molded Shore A 50 silicone parts without verification is not recommended because crosslink density, filler content, and strain-rate response differ from the photopolymer network.
For sealing components in automated equipment, compression set testing under ASTM D395 or comparable methods is performed on production-run coupons after conditioning. Published data for this specific configuration is limited, and part performance varies with print orientation, post-processing history, and section thickness. Coupons should be printed at the intended production orientation and section thickness rather than as isolated test slabs, because wall thickness and interlayer boundaries influence compressive recovery. The measured compression set and Shore A 50 hardness are then applied as acceptance limits for the specific seal geometry and operating temperature.