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3D Systems VisiJet S300

    • Product Name: 3D Systems VisiJet S300
    • 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 318045
    Productname 3D Systems VisiJet S300
    Manufacturer 3D Systems
    Materialtype Photopolymer resin
    Color Black
    Compatibleprinter ProJet 3500 HD Max
    Printingtechnology MultiJet Printing (MJP)
    Tensilestrength 47 MPa
    Tensilemodulus 2000 MPa
    Elongationatbreak 10%
    Flexuralstrength 65 MPa
    Flexuralmodulus 2000 MPa
    Hardness 80 Shore D
    Heatdeflectiontemperature 58 °C at 0.45 MPa
    Density 1.12 g/cm³
    Waterabsorption 0.4%
    Applications Functional prototyping, master patterns, rapid tooling

    As an accredited 3D Systems VisiJet S300 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 S300

    VisiJet S300 enters jewellery manufacturing as an unblended, ash-controlled pattern feedstock loaded directly into the heated reservoir of a MultiJet Printing platform operating at 32 µm layer thickness. The material is not compounded at the foundry with paraffin diluents, stearic acid modifiers, or resinous tackifiers; any attempt to reduce melt viscosity through solvent or low-molecular-weight wax addition shifts the volatilisation curve upward in the 250–350 °C burnout band and increases carbonaceous residue on the inner surface of gypsum-bonded investment moulds. Prior to tree assembly, the sacrificial support wax is removed by thermal dissolution in a dedicated wax-dissolving bath, followed by a warm surfactant and deionised water cycle, because oil carryover onto the pattern surface acts as a barrier to investment wetting and generates gas porosity during casting. For precious-metal casting, the pattern is printed at 100 % feedstock concentration, wax-welded onto a central sprue with a 3–5 mm contact neck, and invested under vacuum in accordance with the final article verification requirements of ISO 9202:2019 and the nickel-release restrictions of REACH Regulation (EC) No 1907/2006, Annex XVII, Entry 27. Burnout is conducted in a vented two-stage kiln with a first plateau in the 150–200 °C range to discharge liquid wax without shell bursting, followed by a controlled ramp of 1–2 °C/min to 730 °C and a soak of 2–4 h to oxidise residual organics. Terminal finished product types include hollow filigree rings, micro-pave settings, thin-wall pendant frames, and bracelet links in gold, silver, platinum, or palladium white-gold alloys where polish-compensated layer steps must be below 10 µm after finishing.

    What burnout residue limits apply to castable patterns for cobalt-chromium and nickel-chromium dental frameworks?

    Under ISO 15854:2007 for dental casting wax and ISO 22674:2016 for metallic dental restorative materials, a castable pattern destined for cobalt-chromium or nickel-chromium removable partial denture frameworks must exhibit residual ash no greater than 0.01 wt% after exposure to the investment-specific thermal schedule. S300 is processed in dental laboratories at 100 % as-supplied feedstock without addition of liquid wax plasticisers, because dilution alters the solidification shrinkage vector and increases marginal misfit in thin lingual bars with wall thicknesses down to 0.5 mm. Printed patterns are connected to a central bar with wax cylinders of 2.5–4.0 mm diameter, then invested in phosphate-bonded material under vacuum to prevent air entrapment at the pattern surface. Burnout is performed in a multi-zone laboratory kiln with a maximum temperature of 900 °C and a hold of 60 min; furnace validation records show that the critical control point is the oxygen partial pressure in the 350–550 °C zone, where incomplete oxidation of long-chain wax esters generates soot that contaminates the metal-ceramic interface. After casting, frameworks are finished to meet the yield strength and percentage elongation requirements of ISO 22674:2016 for Type 5 alloys. Terminal products include removable partial denture frameworks, implant-retained bars, and crown copings.

    Application trackCritical thresholdReference standard or method
    Precious-metal jewellery castingResidual ash ≤ 0.01 % at 730 °CISO 9202:2019, REACH Annex XVII Entry 27
    Dental framework castingResidual ash ≤ 0.01 wt% at 900 °CISO 15854:2007, ISO 22674:2016
    Aerospace turbine airfoil castingAsh residue below shell contamination limit; dimensional verification at 32 µm layer compensationAS9100D clause 8.4.1, OEM shell specification
    Automotive turbocharger castingResidual mass ≤ 0.01 % at 750 °CIATF 16949:2016 clause 8.6.1, ASTM D3418-21
    Orthopedic investment castingRH ≤ 50 % during patterning; two-stage burnout to 950 °CISO 13485:2016, ISO 5832-3:2016, ASTM F75

    In superalloy investment casting foundries producing turbine airfoils, VisiJet S300 is selected as a fugitive pattern because the material is specified to leave a residue below the 0.01 % ash threshold commonly applied in shell burnout validation and embedded in AS9100D clause 8.4.1 supplier-controlled pattern fabrication and engine OEM ceramic shell leaching requirements. The wax is printed at 100 % feedstock in a MultiJet Printing cell with dimensional verification by 3D laser scanning at 32 µm layer compensation, then assembled onto wax runner systems using heated tools rather than solvent adhesives, because chlorinated solvent residues persist through shell drying and initiate cobalt-aluminide oxide inclusions during single-crystal solidification of nickel-base superalloys. Ceramic shell building follows a seven-layer slurry schedule with stucco grits increasing from 80 mesh to 220 mesh; shell thickness is matched to a thermal expansion mismatch between S300 and the fused-silica shell of less than 0.2 % at 95 °C. Autoclave dewaxing is conducted at 150 °C and 5.5 bar for 10–15 min, followed by a burnout ramp of 2 °C/min to 1,000 °C with a 2 h hold to eliminate wax-derived volatiles from blade trailing-edge cooling passages. Published thermogravimetric curves for S300 in specific shell configurations are limited; foundries therefore validate each campaign by differential scanning calorimetry against the shell preheat specification. Terminal products include equiaxed nickel-base high-pressure turbine blades, cobalt-base vanes, and structural nozzle guide vanes that conform to customer-specific macroetch and X-ray inspection criteria.

    Turbocharger impeller patterns and IATF 16949 process control

    IATF 16949:2016 clause 8.6.1 release criteria require foundries to document pattern dimensional stability for turbocharger compressor wheels intended for investment casting in 17-4PH stainless steel or TiAl intermetallics. S300 is printed at 100 % input concentration without mixing with recycled foundry wax, because recycled paraffin can carry silica shell fines that raise printhead nozzle clogging frequency and shift the ash signature outside the validated window. The printed impeller pattern moves through support removal, coordinate measuring machine audit, and tree assembly before application of 6–8 ceramic shell layers and autoclave dewaxing at 150 °C. Burnout of S300 in the shell is validated by differential scanning calorimetry (ASTM D3418-21) and thermogravimetric analysis to confirm a residual mass of less than 0.01 % at 750 °C. Terminal finished product types include compressor wheels with inducer vane-tip thicknesses of 0.4–0.8 mm, turbine wheels, and bearing housing patterns used for rapid foundry validation runs.

    When low-ash patterns enter orthopedic investment casting cleanrooms

    Where cobalt-chromium or titanium investment castings are produced for orthopedic implants under ISO 13485:2016 quality systems and material requirements of ISO 5832-3:2016 for Ti-6Al-4V or ISO 5832-4:2014 for cast cobalt-chromium-molybdenum, the fugitive pattern must not contribute endotoxin, pyrogen, or non-biocompatible residue to the ceramic shell. S300 is used at 100 % concentration from sealed cartridges in cleanroom environments with relative humidity controlled below 50 % because adsorbed surface water increases hydrogen-induced porosity risk in titanium castings. The printed acetabular shell or tibial tray pattern is attached to a face-fed sprue system, invested in yttria-stabilized slurry for titanium or phosphate-bonded zircon slurry for cobalt-chromium, and subjected to a two-stage burnout of 200 °C for 1 h followed by 950 °C for 2 h. Finished terminal products include ASTM F75 cobalt-chromium condylar plates, Ti-6Al-4V acetabular shells, and porous-coated femoral components requiring subsequent sintering. Final device validation remains subject to ISO 10993-1:2018 biological risk assessment rather than any claim arising from pattern material composition alone.

    General industrial precision casting facilities producing hydraulic valve bodies and thin-wall stainless steel impellers use S300 where dimensional tolerance bands of ±0.15 mm are specified by ISO 8062-3:2007 general dimensional and geometrical tolerances for castings. The pattern feedstock is not blended with foundry wax reclaim; each print run is dedicated to 100 % S300 to maintain a stable viscosity window and ash signature below 0.01 %. After MultiJet Printing layer generation, patterns are post-processed in thermal support removal equipment, mounted on trees by hot-wax adhesion, and shelled with colloidal silica slurry. Burnout is executed with a maximum ramp of 2 °C/min to prevent steam expansion from moisture trapped under shell layers. Terminal finished product types include internal-flow hydraulic manifolds, multi-vane diffusion nozzles, pump casings, and impellers in 316L and duplex stainless steel where near-net geometry reduces machining stock to less than 1 mm per surface.

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    Certification & Compliance
    More Introduction

    The 3D Systems VisiJet S300 is a melt-removable wax support material formulated for use with wax-pattern MultiJet Printing platforms, principally the ProJet MJP 2500W series and ProJet MJP 3600W in investment casting workflows. The material is jetted alongside castable pattern wax to fill negative draft, internal cavities, and unsupported overhangs; after build completion the support phase is removed by controlled heating rather than aqueous dissolution. Unlike pattern wax, S300 is not designed to remain in the investment casting tree through burnout, although trace films may persist if removal is incomplete and must be accounted for in dewax and burnout schedules. Published data for this specific configuration is limited; lot qualification under ASTM D3418 and ASTM D482 is therefore a prerequisite for critical casting applications.

    What Distinguishes a Phase-Change Support Wax from Solvent-Soluble Supports?

    The primary distinction is removal mechanism. S300 functions by melting at a lower temperature than the castable pattern wax, allowing support extraction in a forced-air oven or mineral oil bath while the pattern remains solid. Solvent-soluble supports rely on chemical dissolution and introduce a liquid infiltration step that may plasticize wax patterns or create surface etch. Process windows are thermal rather than solvency-driven; therefore the dominant control variables are oven temperature uniformity, ramp rate, and load geometry. Because the phase-change route does not require drying after support removal, water uptake in hydrophilic pattern waxes is reduced, but the thermal cycle adds a residual stress component that can affect thin-walled patterns. Equipment behaviour on production lines shows that tightly packed build plates with low airflow clearances can produce condensate re-deposition near cool chamber walls if extraction temperatures are raised too quickly.

    In jewelry service bureaus operating ProJet MJP 2500W systems, support removal is typically integrated with the casting tree assembly step. The S300 phase is removed before spruing and investing, because any residual support wax inside a cavity creates a non-vented pocket during investment pouring. In production practice, wax patterns are placed on non-wicking trays in a forced-air convection oven with programmable ramp-and-soak capability. The oven should be equipped with active fume extraction compliant with NFPA 86 and local fire codes, because wax volatiles, not aqueous vapour, constitute the exhaust stream. Temperature setpoints are selected below the flash point published on the safety data sheet; for S300, the safety data sheet and technical datasheet must be consulted for the current flash point because formulations are subject to change. A practical upper limit for daily operation is often derived from the material’s flash point minus a safety margin, not from anecdotal shop practice.

    Melt Removal Profiles in Forced-Air and Mineral Oil Support Extraction

    Support extraction in a forced-air oven proceeds by a low-temperature hold at approximately 5 K to 15 K above the wax’s congealing point to mobilize the bulk, followed by a slow ramp to the final extraction setpoint. The melt pool drains from the build plate through perforated stainless-steel grates into a collection pan. Failure modes observed in actual manufacturing lines include entrapped wax in blind cavities when the oven ramp exceeds the capillary drainage rate, and thermal shadowing on large build plates where edge regions reach the setpoint before the centre. To reduce temperature differentials, the load should be placed away from direct radiant elements and the oven should maintain a minimum air circulation rate, typically specified by the oven manufacturer, with a chamber temperature uniformity of ±2 K or better over the working volume. Mineral oil extraction is used when higher heat transfer is required; the build plate is immersed in a temperature-controlled bath at a setpoint below the pattern wax softening point. Oil extraction removes S300 by convective contact rather than radiant oven heat, but it introduces a subsequent detergent or solvent wash step to remove oil films, which is a processing cost and a potential source of contamination if the wash is not fully dried.

    Because wax is a poor thermal conductor, the support removal step is governed by transient heat transfer through the part cross-section, not simply by the oven setpoint. Thin-walled patterns may clear quickly; thick sprues with encapsulated S300 require hold times that scale with the square of the diffusion path. Production technicians monitor for surface blooming, which indicates that support wax is migrating through the pattern rather than draining from the open face. In a phase-change system the separation between support melting point and pattern softening point is the critical property; if the two overlap by more than a few kelvin, the pattern will slump under its own mass before support removal is complete. Published data for this specific configuration is limited, so differential scanning calorimetry under ASTM D3418 should be performed on both the support and pattern materials from the same lot to establish the actual separation.

    When Post-Processing Conditions Exceed the Pattern Wax Softening Point

    Process conflicts arise when the extraction setpoint or the thermal ramp overshoots the pattern material’s softening point. The result is not a sudden collapse but a gradual loss of fine detail: filigree features begin to bend, thin cuff walls lose circularity, and stone-setting prongs may drift from their printed positions. Because S300 is removed before investment, any distortion induced during support removal is transferred directly into the investment mould and cannot be corrected by burnout. This is a distinct limitation compared with solvent-removable supports, which impose little or no thermal load but may alter the surface condition of the pattern. Engineering controls include thermocouple-instrumented dummy patterns placed at the centre and corners of the build plate, repetitive temperature mapping of the oven, and a locked ramp profile that does not exceed the safe separation differential. Some facilities separate support removal into two stages: a low-temperature gravity drain to remove the bulk, followed by a short hot-air blow-off for residual films. The second stage must be applied at a distance and at an air velocity low enough to avoid local viscous heating or mechanical deformation.

    In high-volume casting operations, the accumulated S300 wax collected from extraction trays is not typically reused as a pattern material because its thermal history and potential metal particulate contamination alter viscosity and ash behaviour. Recycled support wax may be processed through a filtration loop, but the recycle ratio must be validated by ASTM D482 ash testing and ASTM D3236 viscosity testing to ensure that the melt remains within the printhead’s allowable range. Printhead failure modes associated with off-spec support wax include clogged nozzle plates, jetting instability, and build plate delamination at the support-pattern interface. On production equipment, batch-to-batch variation can be tracked by recording the cartridge lot number, oven setpoint, drain time, and visual inspection result; this is the minimum data set for correlating support removal defects with raw material variation.

    Ash Content, Oxygen Sensitivity, and Wax Condensate Handling

    Investment casting burnout of wax patterns is commonly conducted under oxidizing conditions to leave minimal carbon residue; support wax residues must be viewed as part of the total ash budget. A pattern tree carrying S300 remnants will release additional volatile matter during the initial burnout ramp, and if the furnace load is too dense or the air exchange rate too low, the vapours may not fully oxidize, leaving carbonaceous contamination on the mould wall. The relevant test method for ash is ASTM D482. Condensate handling is a separate maintenance requirement: support wax volatiles condense on cool ductwork and downstream surfaces. In production, exhaust ducts should be heated or have removable drip trays because wax condensate solidifies and can restrict airflow. Facilities should implement a maintenance interval based on measured duct temperature, not solely on visual inspection. Oxygen sensitivity is not typically a direct property of the solid wax itself, but the removal process must not be conducted in sealed non-ventilated ovens because the flash point can be approached in stagnant air pockets. Use of inert-gas ovens is generally unnecessary and may complicate fume extraction; if used, the lower oxygen content does not change the phase-change temperature but may alter the degradation pathway.

    Support material selection is therefore not a direct substitution for soluble supports; the thermal budget, pattern geometry, and casting tree orientation determine whether S300 can be used without secondary cleaning operations. In dental press-to-metal frameworks with thin margins, the residual S300 film left after gravity draining may require a final hot-air blow-off, but the air velocity must be verified on a sacrificial lot to avoid deforming thin wax margins. Unlike solvent-removable supports, which can dissolve inside blind pockets if circulation is adequate, a melt-removable support depends on an unobstructed drainage path; blind cavities with no vent hole will retain molten wax even when the oven setpoint is raised. This geometric limitation must be accounted for during CAD preparation by adding vent holes or orienting the part so that each support-filled cavity has a gravity drainage exit.

    Test methodPropertyProcess control purpose
    ASTM D3418Transition temperatures by differential scanning calorimetryConfirm support melt onset and pattern separation
    ASTM D3236Apparent viscosity of hot melt materialsVerify melt viscosity for jetting stability
    ASTM D92Flash point, Cleveland open cupSet maximum oven setpoint with safety margin
    ASTM D482Ash from petroleum productsEstimate burnout residue and recycle limits
    ASTM D87Melting point of petroleum waxQuality control of support congealing range

    Compared with the castable pattern material used on the same printer, S300 exhibits a lower melting or congealing temperature and is not formulated for direct lost-wax casting. Its purpose is mechanical support during the build; it does not duplicate the dimensional accuracy or surface finish of the pattern material after burn-out. Compared with solvent-removable supports from photopolymer MJP platforms, S300 requires no aqueous wash station and therefore reduces water-induced swelling of wax. However, it introduces thermal extraction equipment and a fire-code-compliant exhaust stream. Compared with breakaway supports in vat polymer systems, S300 is not mechanically removed by hand tools; its removal is a thermal process. These differences place the product in the melt-removable wax support class, which is applicable only where the build material is a wax-like phase with a higher thermal stability window.

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