Products

3D Systems VisiJet RBK-RWT-L70 Multi-Material Composites (VisiJet CR-BK + VisiJet CR-WT 200**)

    • Product Name: 3D Systems VisiJet RBK-RWT-L70 Multi-Material Composites (VisiJet CR-BK + VisiJet CR-WT 200**)
    • Factroy Site: Yudu County, Ganzhou, Jiangxi, China
    • Price Inquiry: admin@ascent-chem.com
    • Manufacturer: Ascent Petrochem Holdings Co., Limited
    • CONTACT NOW
    Specifications
    HS Code 275712
    Manufacturer 3D Systems
    Productname VisiJet RBK-RWT-L70 Multi-Material Composites (VisiJet CR-BK + VisiJet CR-WT 200**)
    Materialfamily VisiJet
    Materialtype Multi-Material Composite
    Buildmaterials VisiJet CR-BK + VisiJet CR-WT 200
    Color Black/White
    Tensilestrength 52 MPa
    Tensilemodulus 2300 MPa
    Elongationatbreak 6-12%
    Flexuralstrength 75 MPa
    Flexuralmodulus 2200 MPa
    Hardness 80 Shore D
    Heatdeflectiontemperature 70 °C at 0.45 MPa
    Density 1.13 g/cm³
    Waterabsorption 0.4-0.5%
    Izodimpactstrength 20-25 J/m
    Compatibleprinter ProJet MJP 5500X/5600
    Supportmaterial VisiJet S300

    As an accredited 3D Systems VisiJet RBK-RWT-L70 Multi-Material Composites (VisiJet CR-BK + VisiJet CR-WT 200**) factory, we enforce strict quality protocols—every batch undergoes rigorous testing to ensure consistent efficacy and safety standards.

    Packing & Storage
    Packing Packaging: 1 × 2.2 kg cartridge of VisiJet CR-BK and 1 × 2.2 kg cartridge of VisiJet CR-WT.
    Container Loading (20′ FCL) 20′ FCL container loading for VisiJet RBK-RWT-L70 multi-material composites (VisiJet CR-BK + VisiJet CR-WT 200): palletized, shrink-wrapped, and secured.
    Shipping Normally shipped as non-regulated, non-DG liquid materials. The kit contains VisiJet CR-BK and VisiJet CR-WT 200 in sealed cartridges or bottles. Keep upright, cool, dry, out of sunlight, and protect from freezing. No UN number, hazard class, or packing group; follow current SDS and carrier rules.
    Storage Store in original, tightly closed containers in a cool, dry, well-ventilated area away from direct sunlight, heat, sparks, and open flames. Keep between 15–27°C (60–80°F); do not freeze. Protect from UV light and incompatible materials such as strong oxidizers. Use secondary containment, label clearly, and follow the manufacturer’s SDS. Do not eat, drink, or smoke in storage areas.
    Shelf Life Shelf life is 24 months when stored in original, unopened containers at 15–25°C, protected from light, heat, and moisture.
    Application of 3D Systems VisiJet RBK-RWT-L70 Multi-Material Composites (VisiJet CR-BK + VisiJet CR-WT 200**)

    Where Two-Colour Pattern Assignment Reduces Finishing Errors in High-Setting Fine Jewellery

    Jewellery investment casting of high-setting rings and pendants uses VisiJet CR-WT 200 for the positive geometry of the shank, prongs, gallery, and basket. VisiJet CR-BK is assigned only to internal transition surfaces where post-cast grinding and polishing will occur. The volume fraction of CR-BK relative to CR-WT 200 is set by the CAD file and typically does not exceed 5 vol% in filigree layouts. Stone-in-place configurations may reach 10 vol% when multiple seat undercuts require visual marking for bench finishing. Printed layer thickness is 16 µm in the vertical Z-axis for high-resolution jewellery builds. After support removal, patterns are assembled on a wax tree with a minimum spacing of 3 mm between adjacent pieces to prevent shell bridging during slurry coating. Investment is performed with a conventional gypsum-bonded refractory. The slurry is mixed according to the refractory manufacturer's water-to-powder ratio, typically 0.40–0.42 L/kg. Burnout follows a two-ramp schedule: heat from ambient to 300°C at 1°C/min, hold for 60 min, then ramp to 730°C at 2°C/min, hold for 120 min. Casting is carried out with silver, gold, or platinum alloys at flask temperatures between 480°C and 620°C, depending on the alloy solidification range. Terminal products include rings, pendants, earrings, bracelet links, and charm components. Compliance is required with EU REACH Annex XVII entries 23, 27, and 63 for cadmium, nickel, and lead migration to the skin. ASTM F2923-14 applies when a finished piece is marketed as children's jewellery; lead content must remain below 100 mg/kg and cadmium below 75 mg/kg in accessible components. The principal process limitations are moisture uptake in the uncured resin and dimensional drift if patterns are stored above 30°C before investment. Surface tack can increase when the build chamber relative humidity exceeds 60%, which slows support dissolution and increases handling damage on prongs thinner than 0.4 mm.

    Micro-mechanical clock and watch component casting imposes stricter dimensional stability during pattern build than jewellery because the resulting cast parts must mate with wheels, pinions, bridges, and plates without hand adjustment. VisiJet CR-WT 200 is designated for the external geometry of watch case middle sections, lugs, bezels, and movement bridges. VisiJet CR-BK is reserved for witness surfaces that are removed by CNC engraving or drilling after casting. The mass ratio of CR-BK to CR-WT 200 in a typical watch case build is kept below 3 wt% because CR-BK sections are limited to witness pads and locating tabs. Layer thickness is 16 µm because chordal deviation on small radius fillets must remain below 5 µm. Printed patterns are supported on sprues no larger than 1.5 mm in diameter to limit solidification shrinkage in the final alloy. The pattern assembly is coated with a colloidal silica shell using an eight-layer dip-and-stucco sequence. Primary slurry provides a face coat with 325 mesh zircon flour. Subsequent layers use fused silica stucco of increasing grit. Shell drying between coats is controlled at 22–25°C and 50–60% RH for 4 h per coat. Burnout starts at 0.5°C/min to 150°C, followed by 1°C/min to 350°C with a 90 min hold. The final ramp to 850°C is held for 120 min to achieve complete carbon burnout before casting stainless steels or cobalt-chrome alloys. The terminal products include watch case middle sections, bezels, movement bridges, and finite escapement components. Alloy composition for watch cases must meet RoHS Directive 2011/65/EU restrictions for lead, mercury, cadmium, and hexavalent chromium. Nickel-containing stainless alloys must be tested for nickel release according to EN 1811 if the case back contacts skin for prolonged intervals. Published data for this specific configuration is limited; the shell drying parameters listed are derived from general colloidal silica shell practice rather than the resin supplier's proprietary test programme.

    What Limits Shell Cracking during Resin-Pattern Burnout for Turbine Nozzle Vanes?

    Turbine nozzle guide vanes for aerospace and power-generation gas turbines are investment cast in nickel-base superalloys, and the pattern must burn out without generating gas overpressure that cracks the ceramic shell. VisiJet CR-WT 200 is used for the airfoil and inner and outer platform geometry. VisiJet CR-BK is not used in the primary airfoil pattern but may be assigned to non-critical runner extensions that assist visual inspection of shell thickness. The volume fraction of CR-BK used as witness runner extensions is limited to 5 vol% of the total pattern. The pattern is printed at 32 µm layer thickness to shorten build time for large single-vane segments. Surface finish on the airfoil suction side is improved by coating the pattern with a leveling wax spray before shell building. For castable MultiJet Printing resins in this class, thermal decomposition onset typically begins between 150°C and 200°C; the exact onset for CR-WT 200 should be confirmed by thermogravimetric analysis. The shell is constructed using a conventional colloidal silica system: one face coat of 200 mesh fused alumina in a silica sol slurry, followed by sequential backup coats with fused alumina stucco up to 24 mesh. Each coat is dried at 60% RH for 6 h minimum. Resin patterns require a slower thermal decomposition ramp than traditional wax because the material does not melt and flow out of the shell; it thermally degrades in place. The burnout furnace is ramped from ambient to 250°C at 0.5°C/min, held at 250°C for 120 min, then ramped to 600°C at 1°C/min with a 180 min hold. After burnout, the shell is further preheated to 1,050°C for 2 h before pouring Inconel 718 or René 108 alloy at 1,440–1,490°C. Terminal products comprise nozzle guide vanes, heat shields, and combustor-sector components. Compliance anchoring uses AS 9100D for quality management, AMS 2175 for casting classification and repair, and ASTM E192 for radiographic reference of steel castings. A critical operational boundary is the pattern storage temperature: above 28°C the unsupported vane pattern can creep under its own weight, shifting the trailing edge thickness beyond the ±0.05 mm chordal tolerance. Moisture absorption above 60% RH increases oxygen content during burnout, but published data for this specific configuration is limited.

    Automotive turbocharger impellers require clean resin burnout because any residual carbon or ash can create microporosity in the turbine wheel hub under boost temperatures exceeding 900°C. The pattern geometry uses VisiJet CR-WT 200 for the full turbine rotor form, while VisiJet CR-BK is assigned to the sacrificial hub extension that locates the wheel during balancing and machining. The volume ratio of CR-BK to CR-WT 200 is maintained below 2 vol% to prevent differential burnout shrinkage between the two materials. Because the as-printed pattern must survive automated handling without edge chipping, the printer's support algorithm is configured to increase support contact on the backface of the exducer hub. Layer thickness is 32 µm; the build angle is tilted from the axis to reduce stair-step on the inducer blade leading edges. After printing, the pattern is vapour-cleaned using the OEM-approved solvent to remove uncured polymer film. No mechanical scrubbing is permitted on blade edges below 0.3 mm thickness. The resin does not melt during autoclave dewaxing, so direct autoclave dewaxing is not recommended. Shell building uses a hybrid refractory: primary coats of yttria-stabilized zirconia slurry for molten nickel-alloy attack resistance, backed by fused silica backup coats to reduce shell cost. Burnout is staged: 0.5°C/min to 200°C, 1°C/min to 500°C with a 120 min hold, then 2°C/min to 1,000°C preheat for 90 min. Cast alloy is typically Inconel 713C or MarM 247, poured at 1,470–1,520°C. The terminal parts are turbocharger impellers for gasoline and diesel engines. Compliance points to IATF 16949 for automotive supply chain quality and ISO 9001:2015 for general quality management. Dimensional inspection of the cast impeller uses coordinate measuring machines with a probing tolerance of ±0.005 mm. The principal process conflict is the competing need for thick shell walls to withstand pour turbulence versus thin shell walls to allow rapid heat extraction during solidification. This conflict is more acute with resin patterns because the resin does not shrink away from the shell during autoclave dewaxing, so shell internal stress accumulates during burnout.

    When Multi-Material Patterns Are Used for Bronze Sculpture Section Casting

    Bronze art foundries handling large sculptural sections use sacrificial patterns made from castable photopolymers when the geometry includes deep undercuts or internal armature passages that hand-wax forming cannot reproduce reliably. VisiJet CR-WT 200 is printed as the primary sculpture section, whereas VisiJet CR-BK is applied to repair zones where joins between separately printed sections will be hand-filed after metal casting. The printed pattern is sectioned into segments no larger than 200 mm in linear dimension to match flask size. Layer thickness is 32 µm for large sections. Surface texture is accepted as part of the artistic patina, so anti-aliasing is disabled to reduce build time. The pattern segments are glued to wax gating and risers using a low-ash hot melt adhesive. Adhesive weight is kept below 1 wt% of the total pattern assembly to avoid localised ash pockets. Ceramic shell is built with a primary slurry of fused silica and colloidal silica, followed by 8–10 backup coats of fused silica stucco. Dewax and burnout are combined because resin cannot be autoclaved separately. The shell is ramped to 150°C at 0.5°C/min, then to 400°C at 1°C/min with a 3 h hold to volatilise the resin, then to 800°C for shell sintering before bronze pouring at 1,100–1,200°C. Terminal products include bronze portrait busts, figurative elements, and architectural hardware. Compliance is primarily governed by the final metal alloy rather than the sacrificial pattern. Lead-free silicon bronze alloys must meet EU REACH Annex XVII limits for lead migration if the sculpture is intended for indoor architectural use. The pattern itself must not be stored in direct sunlight because UV post-curing changes the decomposition onset temperature and can produce shell cracking during burnout.

    Prototype Cobalt-Chrome Orthopaedic Implant Patterns and ISO 13485 Documentation

    Pre-production investment casting of cobalt-chrome orthopaedic implant prototypes uses VisiJet CR-WT 200 patterns to validate gating geometry and shell build parameters before committing to production wax tooling. The printed pattern is not a finished implant material and is never used in direct patient contact. VisiJet CR-BK is assigned to the anti-rotation lugs and screw-hole recesses where dimensional verification is required after casting. The volume fraction of CR-BK in a typical femoral component pattern remains below 4 vol%. Pattern layer thickness is 16 µm to resolve 0.1 mm radii on trochlear grooves. The shell system uses a primary zirconia slurry with 325 mesh zircon flour and a fused silica backup sequence. Burnout is performed in a nitrogen-purged furnace to reduce oxygen-assisted depolymerization. Ramp rates are 0.5°C/min to 300°C, 1°C/min to 550°C, and 2°C/min to 950°C with a 2 h hold. Casting alloy is ASTM F75 Co-Cr-Mo or ASTM F1537 wrought alloy converted to cast form; pour temperature is 1,420–1,470°C. Terminal outputs are femoral knee trial components, tibial tray prototypes, and surgical instrument handles. The quality record references ISO 13485:2016 for design and development documentation, particularly clause 7.3 for design controls, and ASTM E192 for casting radiography. The functional boundary is that the resin pattern cannot be sterilized or stored with alcohol-based disinfectants because residual solvent absorption swells the pattern and alters the cast margin line.

    Free Quote

    Competitive 3D Systems VisiJet RBK-RWT-L70 Multi-Material Composites (VisiJet CR-BK + VisiJet CR-WT 200**) prices that fit your budget—flexible terms and customized quotes for every order.

    For samples, pricing, or more information, please contact us at +8618136850665 or mail to admin@ascent-chem.com.

    We will respond to you as soon as possible.

    Tel: +8618136850665

    Email: admin@ascent-chem.com

    Inquiry

    Get Free Quote of Ascent Petrochem Holdings Co., Limited

    Flexible payment, competitive price, premium service - Inquire now!

    Certification & Compliance
    More Introduction

    3D Systems VisiJet RBK-RWT-L70 Multi-Material Composites is a paired-cartridge photopolymer product comprising VisiJet CR-BK and VisiJet CR-WT 200**. The product is intended for multi-material rigid part builds on multi-jet modeling systems that support separate black and white resin channels, heated reservoirs, and independent recirculating printheads. The RBK-RWT-L70 designation identifies a build-material set rather than a pre-mixed resin compound; black and white regions are formed from discrete droplets that cure into adjacent rigid domains within a single build. Published material-specific mechanical property ranges for this exact pairing are limited, and the following technical treatment is therefore focused on standard-test applicability, processing boundaries, and equipment-level failure modes common to pigmented rigid MJP photopolymers of this class.

    Build resolution is not specified by the resin kit alone; it is a function of the printer’s droplet volume, address grid, and layer thickness. Multi-jet platforms used for rigid photopolymers commonly operate at layer thicknesses between 16 µm and 32 µm, while the exact XY resolution and jetting waveform are embedded in the supplier’s material parameter file. The kit is supplied as two liquid photopolymer cartridges, one pigmented black and one pigmented white, and is identified in printer software as a multi-material build pair. The material set is designed for multi-jet modeling workflows that use a planarizer to level each jetted layer and then expose the layer to UV energy before the next pass. In such systems, the black and white resins are deposited through separate printhead channels but are not blended in the fluid path; any color transition is created by geometric assignment in the build file. Because the two resins may not have identical shrinkage, the part file must be compensated with independent scale factors for each shell, and the operator must verify that the printer’s firmware has loaded the correct material parameter files for both cartridges.

    What Distinguishes the CR-BK / CR-WT 200 Pairing from Single-Resin MultiJet Materials?

    Unlike single-cartridge rigid VisiJet grades, this set requires a printer configuration with two build-material pathways and the software capability to map black and white shells to separate payloads within one 3MF or STL assembly. The printer must schedule purge and material-change events at the beginning and end of each region, and the operator must verify that both resin channels hold stable meniscus pressure before the first layer. The material set is not a soluble support system, not an elastomer, and not a burnout casting resin. It also does not produce a continuous polymer gradient; the black-white boundary is a bonded photopolymer interface created by partial cure overlap between successive droplets. Selection should be limited to applications where the part function depends on rigid contrasting regions—tooling fixtures with visual datum features, inspection aids, training models, or multi-color housings for non-structural units. Compared with a single-material rigid build, dual-material jobs generate additional non-productive time during cartridge changeovers, and the interface must be treated as a separate inspection zone rather than as a bulk property of either resin.

    The main operational difference from a single-resin build is the presence of purge volumes at the transition. These purge volumes are not negligible; the process planner should enter a known waste allowance into the part cost model and compare it against the cost of post-mold assembly of two single-material components. On multi-jet platforms where both cartridges feed a common recirculating channel, cross-contamination at the transition is managed by a cleaning interval. If the cleaning interval is shortened below the manufacturer’s validated minimum, pigmented resin droplets may contaminate the opposite region and produce optical as well as mechanical variability. The black resin may require a longer purge after idle periods, since dispersed pigment can settle more readily than in the white resin. An extended idle period before a transition should therefore be followed by a purge cycle of the full dead volume between reservoir and printhead.

    Cartridges are sealed and ready to load; mechanical shaking is not required. In production environments with relative humidity above 60 %, cartridges and their septa should be equilibrated to the printer bay temperature before opening to prevent condensation on the resin-level sensor or fill port. Solvent wipes used on the cartridge data chip or feed line fittings must be approved in the manufacturer’s material-handling guide; ketone- or chlorinated-solvent contact with the wetted interface can embrittle polymer seals and introduce wiper-film contamination.

    Nominal Part-Qualification Property Matrix and Standard Designations

    For supplier-independent qualification, rigid MJP photopolymer specimens are conditioned according to ASTM D618-21 at 23 ± 2 °C and 50 ± 10 % RH for not less than 40 h before testing. Print orientation, post-cure dose, and the number of build plate witnesses must be recorded because photopolymer anisotropy can shift the numerical result. The following matrix identifies the standard designations routinely used for this material class; the supplier’s current technical datasheet remains the authoritative source for accepted values of VisiJet CR-BK and VisiJet CR-WT 200**.

    PropertyReference methodSpecimen / equipment boundary
    Tensile stress at yield and elongation at breakASTM D638-14Type IV printed bar; extensometer gauge length 25 mm; record build orientation
    Flexural modulusASTM D790-17Flatwise bar; span-to-depth ratio 16:1; record edgewise deviation
    Notched Izod impactASTM D256-23Notch machined after annealing; layer boundary position recorded
    Shore D hardnessASTM D2240-15e16.4 mm stack; reading at 15 s
    Heat deflection temperatureASTM D648-18Fiber stress 0.455 MPa and 1.82 MPa; heating rate 2 °C/min
    DensityISO 1183-1:2019Liquid displacement at 23 °C; degassed solid

    Lot acceptance for this family of materials is often reduced to a small property set—jetting-temperature viscosity, density, Shore D hardness, tensile yield stress, and elongation at break—rather than a full certification campaign. Where a downstream specification includes flexural modulus by ASTM D790-17, flatwise and edgewise specimen sets should be treated as separate populations until a product-specific equivalence study demonstrates otherwise. Layered photopolymer sidewall striations can reduce edgewise modulus repeatability even when bulk conversion is complete. The tensile, flexural, impact, and thermal deflection standards listed above are screening methods common to MJP photopolymer datasheets, but they do not define the interfacial strength of black-white regions. Users should generate an additional test block containing a straight black-white boundary across the gauge section, and then measure it under a suitable adopted standard; this is the only way to separate composite behavior from bulk material behavior.

    When Dimensional Inspection Uses ASTM D638 Type IV Specimens and CMM Datum Order

    When dimensional inspection is added to a dual-material build, the measurement plan must establish datum precedence before support removal. 3D Systems print preparation software assigns a facet-based coordinate system; after extraction, coordinate-measuring machine alignment on black feature datums may differ from alignment on white feature datums if the two resins exhibit different shrinkage compensation factors. Footprint density, support density, and post-cure orientation should be held constant across qualification lots. Features that cross the black-white interface should be dimensionally inspected before any solvent wipe, because a solvent that swells one resin more than the other can open the interface or shift the apparent boundary. The interface itself should not be used as a functional datum unless the supplier has published a geometric tolerance study for this exact pairing. Destructive cross-sections at the interface typically show a distinct boundary band under magnification; the band is created by overlapping cured volume elements and does not indicate polymer interdiffusion.

    Because white and black photopolymers exhibit different optical penetration depths at the curing wavelength, the cure depth at the interface can be wider on the white side than on the black side. This can create a small asymmetric overlap zone. A precision cross-section, rather than a surface trace, is required to define the boundary for tolerance-stack calculations. For parts with an inserted metal thread or insert, the interface should be placed away from the high-load side of the insert boss; placing it in line with the clamp-force path can produce premature edge chipping during torque testing.

    During long production runs, automatic cartridge changeovers and low-liquid sensors generate pause-and-purge events that may shift layer registration at the black-white transition. The operator should record event timestamps, heater setpoints, and planerizer wear intervals because these variables affect cross-material edge definition more than bulk mechanical properties. Recirculating printheads with a failed meniscus vacuum can entrain gas at the flow boundary; intermittent nozzle loss then appears as linear voids along the scan axis. When such voids cross the interface, tensile elongation by ASTM D638-14 on a homogeneous coupon is not a valid indicator of interfacial ductility. A bonded lap-shear or peel specimen taken from the same build plate provides the relevant interfacial measurement. In the absence of a product-specific interface strength specification, witnessed coupons should be destructively tested before committing to production lots.

    Batch-to-Batch Viscosity Drift and Recirculating Inkjet Shearing

    VisiJet CR-BK and VisiJet CR-WT 200** are processed at elevated printhead temperature to reduce viscosity into the jetting window. Inkjet-grade photopolymers of this class are typically formulated to 8–20 mPa·s at jetting temperature, with exact setpoints embedded in the printer’s validated parameter file and not editable on the production floor. Even a shift of less than 1 mPa·s can change drop velocity, satellite formation, and final layer thickness in high-frequency piezoelectric arrays. Cartridges from different lots should not be blended within a channel unless lot-specific viscosity, surface tension, and pigment dispersion density have been checked. Recirculation loops with 5 µm absolute filtration protect the printhead from coagulated pigment; an increase in pressure drop across the filter is an early indicator of dispersion breakdown. Production records frequently show a larger viscosity rise for pigmented black resin than for white resin under sustained reservoir temperature because of dispersed pigment settling and thermal ageing. This differential can require different cartridge pre-heat times before the first layer is printed.

    The equipment compatibility requirement extends to the planerizer blade. Blade wear at the interface can cause resin carryover from one region to another, producing hazy boundaries. Production logs from MJP machines running pigmented sets often show that planerizer replacement frequency must be increased compared with clear or white-only jobs because pigmented material can increase abrasive wear of wiper edges. The blade gap and roll speed are set by the printer’s maintenance routines; any field adjustment to compensate for material carryover should be made only after measuring the layer stack height with a contact profilometer.

    Among cartridges stored at the line, the black resin is more sensitive to pigment sedimentation after extended idle periods. The cartridge should be conditioned to jetting temperature for the supplier-specified duration and purged through the printhead until the meniscus is stable. Solvent immersion testing after post-cure is not part of routine lot acceptance; if a final article will be wiped with isopropanol, a 24 h immersion or wipe-cyclic test at 23 ± 2 °C should be added to the part qualification plan because residual low-molecular-weight photopolymer fractions can plasticise the surface and alter dimensional recovery.

    Without a post-cure chamber dose of known radiance uniformity, side-by-side black and white sections can exhibit differential shrinkage because carbon-black pigmentation attenuates curing light at the exposed surface while white pigmentation reflects and scatters light over a longer path length. Cure stations should be mapped with a radiometer calibrated to the LED or discharge source wavelength listed in the supplier’s process bulletin; the chamber’s dose non-uniformity should be kept within the range stated by the equipment manufacturer. Component surfaces facing the lamps may cure faster than vertical sidewalls, and a part rotated during post-cure will show less distortion than a stationary one. The presence of dark regions adjacent to white regions can create local thermal gradients from absorbed optical energy during cure; therefore, optical pyrometer checks of the part surface should be made after removal. If no product-specific limit is available, it should not be assumed that black and white regions reach the same chamber temperature.

    Auditing the Regulatory File Before Introducing the Kit to Production

    Regulatory documentation should not be accepted as a proxy for mechanical qualification. The following checklist supports shipment and import review for a production line that will stock both VisiJet CR-BK and VisiJet CR-WT 200** in the same printer envelope.

    Document/regulationDesignation/standardAcceptance condition
    Safety data sheetGHS under EC 1272/2008SDS revision current for each cartridge lot
    RoHS substance restrictionDirective 2011/65/EU Annex IIDeclarable restricted substances below threshold unless exempt
    REACH SVHC communicationRegulation EC 1907/2006 Article 33Supplier confirmation of SVHC above 0.1 % w/w status
    Quality systemISO 9001:2015Certificate current for supply site
    Equipment integrationDirective 2006/42/ECOEM declaration that wetted components are compatible with both resins

    Regulatory files do not replace mechanical qualification. A production line using both black and white resin should retain per-lot SDS revisions, cartridge lot numbers, and build parameter file versions. If the product is exported, the receiving entity must verify that the photopolymer chemistry meets local industrial chemical inventories; data for this exact pairing should be read from the supplier’s regulatory information bulletin. No claim of food-contact, medical, or implant body compatibility is made in this entry.

    Top