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DSM Somos 7120 Epoxy Photopolymer, UV Postcure

    • Product Name: DSM Somos 7120 Epoxy Photopolymer, UV Postcure
    • 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 584146
    Density 1.13 g/cm³
    Viscosity At 30 C 220 mPa·s
    Tensile Strength 54 MPa
    Tensile Modulus 2.76 GPa
    Elongation At Break 12%
    Flexural Strength 77.9 MPa
    Flexural Modulus 2.21 GPa
    Hardness Shore D 80
    Izod Impact Notched 0.48 J/cm
    Heat Deflection Temperature 60 °C
    Glass Transition Temperature 70 °C
    Water Absorption 0.35%
    Critical Exposure 9.7 mJ/cm²
    Penetration Depth 0.14 mm

    As an accredited DSM Somos 7120 Epoxy Photopolymer, UV Postcure factory, we enforce strict quality protocols—every batch undergoes rigorous testing to ensure consistent efficacy and safety standards.

    Packing & Storage
    Packing Packaged in 1 kg opaque HDPE bottle, tightly sealed with child-resistant cap, labeled DSM Somos 7120 Epoxy Photopolymer, UV Postcure.
    Container Loading (20′ FCL) DSM Somos 7120 Epoxy Photopolymer, UV Postcure is palletized, secured, labeled, and loaded into a 20′ FCL container for shipment.
    Shipping DSM Somos 7120 Epoxy Photopolymer, UV Postcure is generally not regulated for transport. Ship in sealed, labeled containers at ambient temperature, protected from UV and contamination. No UN number, hazard class, or packing group is normally required. Always verify current SDS, carrier, and regional rules before shipping.
    Storage Store DSM Somos 7120 Epoxy Photopolymer, UV Postcure, in a cool, dry, well-ventilated place in its original, tightly closed container. Keep away from direct sunlight, UV radiation, heat, sparks, flames, and strong oxidizers. Maintain recommended temperature, generally 15–25°C, and protect from freezing. Use subdued or yellow lighting during handling to prevent premature polymerization. Keep away from food and incompatible chemicals.
    Shelf Life Store sealed in original unopened container at 18–25°C, protected from light; use within approximately 12 months. Do not freeze.
    Application of DSM Somos 7120 Epoxy Photopolymer, UV Postcure

    In investment casting foundries producing nickel-based superalloy small blades and structural brackets, DSM Somos 7120 is processed as a direct-shelling epoxy pattern with a shell-facing wall thickness of 1.0–1.5 mm and internal drainage vent diameter-to-wall thickness ratio not less than 1.5:1. The pattern is generated on a 355 nm stereolithography platform at 100 µm layer thickness; after build completion, the green part is rinsed in isopropanol or tripropylene glycol monomethyl ether for 15–30 min and blown dry with filtered compressed air at 0.2–0.4 MPa. UV postcure is carried out in a chamber with 365 nm lamps at 4–8 mW/cm² for 30–60 min per rotated surface, because single-side exposure leaves the shadowed face under-converted and increases ash residue during burnout. The ceramic shell is applied as a zircon slurry with binder-to-filler ratio maintained between 18:100 and 24:100 by mass, followed by fused silica stucco at 60–120 µm particle size; the first coat is air-dried at 25 ± 3 °C and 50 ± 10 % RH to prevent cracking. Steam autoclave dewaxing at 120–160 °C and 0.4–0.6 MPa removes the bulk pattern, and the remaining carbonaceous residue is oxidized in a gas-fired burn-out furnace at 800–1050 °C for 2–4 h. Shell cracking at section changes is controlled by keeping wall-thickness transitions below 2.0 mm and by adding fillets with radius-to-thickness ratio above 0.5:1. Terminal castings are approved for prototype and short-run production after foundry validation of residual ash below 0.05 wt% by thermogravimetric analysis per ASTM E1131-08. Published data for this specific alloy configuration is limited; therefore, shell cracking thresholds are established on a pattern-geometry-specific basis.

    What Limits Prototype Injection Mold Inserts Built from UV-Postcured Somos 7120?

    Mold inserts are not a high-volume production option for this resin. When UV-postcured Somos 7120 is used as a prototype core or cavity on a vertical injection machine with clamp force between 50–200 tonnes, the practical processing window is restricted to melt temperatures below 220 °C and fill pressures below 70 MPa. Heat deflection temperature, measured per ASTM D648-18 at 0.46 MPa, is below 55 °C after postcure; therefore, molding polypropylene or ABS requires continuous chilled water in the backing plate at 10–15 °C to keep the insert surface below 40 °C. The insert is printed with a thickness-to-steel backing plate ratio of at least 1:4, and the printed body is bolted to the steel using flat-head screws at 50 mm pitch. The parting line is sealed with a rigid two-part epoxy paste and dressed with 600 grit paper; draft angles are held above 1.5°. Edge chipping at the parting line is the primary failure mode after 50–100 shots of unfilled PP or ABS at wall thickness up to 2.5 mm, and dimensional drift is monitored with a coordinate measuring machine after the first 10 shots and then every 25 shots. Terminal products are functional prototypes such as clips, housings, and sealing covers, not production tools. Because published creep data at thermoplastic melt contact temperatures are limited, the shot-count limit is established tool-specifically rather than from a universal acceptance table.

    Silicone Tooling Master Patterns and Platinum-Cure Inhibition Control

    Vacuum casting workflows using platinum-catalysed RTV silicone benefit from the edge acuity of UV-postcured patterns when the print surface is sealed. The printed master is wet-sanded to 320–600 grit, then coated with an acrylic or two-part polyurethane clear coat at 15–25 µm dry film thickness; the coating acts as a chemical barrier between unreacted epoxy or photoacid species and the platinum cure system. Without this barrier, the silicone remains tacky at the pattern surface and may fail to reach Shore A 20–30 after the normal 24 h cure. Postcure of the Somos 7120 pattern is conducted before sealing because residual oxetane groups in the green state are hygroscopic and produce surface tack under ambient moisture. The silicone base-to-catalyst ratio is maintained at 10:1 by mass for platinum systems, with vacuum degassing below 10 mbar for 5–10 min before pouring. After silicone cure, the tool is used for polyurethane casting with gel times of 3–12 min; terminal products are limited-run enclosures, impact-resistant covers, and sealing components cast in two-part polyurethane with Shore A 60–90 hardness. Shrinkage compensation from pattern to silicone to polyurethane is set between 0.15 % and 0.35 % in CAD; dimensional acceptance follows DIN 16742:2013 or tool-specific CMM capability. High-gloss polishing above 1000 grit is possible but increases the risk of sealing coat bridging at sharp radii below 0.25 mm, which changes local geometry.

    Low-temperature composite layup tooling for carbon fiber prepregs curing below 45 °C may be printed as a female tool face and supported by an epoxy-glass backing. The tool face is generated at 100 µm layer thickness and UV-postcured for 60 min per side until Shore D hardness stabilizes above 80 per ASTM D2240-15; tool face thickness-to-glass backing ratio is held at 1:3. Surface porosity is sealed with a low-viscosity epoxy seal coat, and release is supplied by a solvent-based semi-permanent release agent applied in 3 thin coats at 10 min intervals. During layup of carbon fiber/epoxy prepreg with a cure cycle of 35–40 °C for 8–12 h, the vacuum bag is held at 0.7–0.9 bar; the exotherm at the laminate-tool interface must not exceed the tool’s 0.46 MPa heat deflection temperature reported per ASTM D648-18. The main process risk is print-through from layer contour lines, which is controlled by sanding and spackling to Ra 0.4–0.8 µm and by using a contour smoothing step in the build. Terminal components are low-temperature cure carbon fiber brackets, fairings, and drone airframe elements with thickness 0.8–2.0 mm. Tool life is validated by surface profile tracing per ISO 21920-2:2021 after each of the first 10 cycles; an increase in roughness above Ra 1.0 µm triggers refinishing. Published data for this specific resin-tooling configuration is limited; therefore, process limits are confirmed by thermal imaging during the first cure cycle.

    When Electrical Connector Prototypes Require Dielectric Bench Screening and RoHS Documentation

    Electrical connector housing prototypes printed from Somos 7120 are conditioned at 23 ± 2 °C and 50 ± 10 % RH for 40 h before electrical characterization. Volume resistivity and surface resistivity are screened to IEC 62631-3-1, but published data for this specific resin are limited; therefore, acceptance is made against a comparative unfilled epoxy control tested in the same fixture. The UV postcure step increases surface crosslinking and reduces water uptake to 0.3–0.5 wt% after 24 h immersion at 23 °C when measured per ASTM D570-22; this lowers variability in dielectric strength measured per ASTM D149-20 at 2 kV/s on 3.0 mm specimens. Wall thickness-to-boss diameter ratio is maintained above 0.6:1 to avoid sink marks that can reduce creepage distance. Mechanical retention of metallic terminals is limited to pull-out forces below 50 N unless the housing is integrally ribbed; repeated insertion above this load promotes stress cracking at living hinge or snap features. Low-voltage signal prototypes are tested at 48 V DC and short-term exposure to 125 °C; glow wire compliance to IEC 60695-2-11 at 750 °C is not assumed for unfilled epoxy photopolymer and requires separate UL evaluation. Material compliance documentation is limited to RoHS 2011/65/EU and REACH SVHC declarations under EC 1907/2006 supplied by the resin manufacturer. Terminal products are functional electrical housings, relay covers, and diagnostic connector bodies for pre-production harness validation, not field-rated insulators.

    Post-cure characterization and compliance references for UV-postcured Somos 7120
    Property/checkStandardTypical test conditionApplication gate
    Tensile modulusASTM D638-14Type V specimen, 5 mm/minInjection mold insert stiffness
    Heat deflection temperatureASTM D648-180.46 MPa, 2 °C/minComposite tool face thermal limit
    HardnessASTM D2240-15Shore D, 15 s dwellPostcure stabilization check
    Dielectric strengthASTM D149-202 kV/s, 3.0 mm specimenElectrical connector screening
    Thermal degradationASTM E1131-08nitrogen, 20 °C/minInvestment casting ash content
    Surface profileISO 21920-2:20214 mm cutoff, 2.5 µm radiusComposite tool and wind tunnel face
    RoHS compliance2011/65/EUhomogeneous materialElectrical/electronic prototype
    REACH SVHC declarationEC 1907/2006current candidate listImport/export documentation

    Wind tunnel test models for airfoil and inlet flow visualization are built directly at 0.05–0.1 mm layer thickness with chordwise stitch lines positioned along pressure gradients. The model is UV-postcured in a chamber with a rotating fixture to limit shadow undercuts and thermal gradients, then machined only at mounting bosses and pressure taps. Surface waviness is measured with a profilometer over a 60 mm trace length and controlled to Ra 0.8 µm before application of a filler primer; trailing edge fillet radius-to-thickness ratio is held above 0.5:1. Models are tested at airspeeds up to 60 m/s and stagnation temperatures below 40 °C; above this threshold leading edge softening has been observed in post-test inspections. Thin trailing edges below 0.3 mm are thickened with an additive fillet to prevent handling fracture. Terminal outputs are baseline aerodynamic surfaces for comparative CFD validation and flow visualization, not flight hardware. Dimensional acceptance follows ISO 21920-2:2021 for surface texture and CMM profile tolerances of ±0.1 mm over 100 mm chord length. Published data for this specific resin-airload configuration are limited; test-specific limits are established by observing first-run surface condition after each tunnel run.

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    Certification & Compliance
    More Introduction

    Within the class of stereolithography resins activated by a 355 nm solid-state laser and completed by a separate ultraviolet flood exposure, DSM Somos 7120 Epoxy Photopolymer, UV Postcure functions as a rigid general-purpose epoxy photopolymer. The liquid is a single-component cationic formulation; no thixotropic adjustment or accelerator addition is performed at the vat level. Manufacturer-published liquid-phase viscosity at 30 °C is typically 0.26 Pa·s, equivalent to 260 cP, and liquid density at 25 °C is reported as 1.13 g/cm³. The polymer network forms through ring-opening of epoxy groups initiated by photogenerated acid species, but laser-only conversion leaves a partially cured green state. The designation “UV Postcure” therefore indicates that full mechanical response and chemical resistance are achieved only after the built part is cleaned, dried, and exposed to broad-spectrum UV radiation in a flood chamber. Production uses include rigid prototype housings, master patterns for room-temperature vulcanizing silicone tooling, and investment casting patterns where the cured resin’s dimensional stability and ash characteristics are compatible with foundry processes.

    What Does the Separate UV Flood Exposure Contribute to the Cationic Epoxy Conversion Profile?

    In cationic photopolymerization, photoacid generation by the 355 nm laser pulse produces initiating species within the scanned line, but the network vitrifies rapidly at room temperature. Molecular mobility becomes restricted before all epoxy groups reach high conversion; the green part therefore contains unreacted monomer, low crosslink density, and reduced glass transition temperature. The UV postcure station supplies additional photons in the 320 nm to 390 nm band, usually with simultaneous moderate heating from the lamp cavity, to re-energize dormant chain ends and permit further ring-opening in the vitrified matrix. Manufacturer recommendations typically specify a postcure time of 30 min to 60 min per surface orientation, with larger masses requiring staged rotation to avoid shadowed regions. The effect of incomplete postcure is measurable through a reduction in heat deflection temperature and an increase in solvent uptake; tensile modulus may approach specification while impact strength and hot-wet performance remain depressed. Testing of cured coupons according to ASTM D618-21 at 23 °C and 50 % relative humidity is therefore required before comparing incoming resin batches or qualifying the postcure chamber.

    On a laser-based stereolithography system with a 355 nm source, the resin is typically processed at slice thicknesses between 0.050 mm and 0.100 mm. Thinner layers reduce stair-step artifact on shallow draft angles but multiply build time and recoating cycles; thicker layers increase productivity but produce larger surface discontinuities that must be filled or machined. The low liquid viscosity permits recoat blade travel with limited meniscus drag, but vat temperature should be maintained within the manufacturer-specified range, commonly near 30 °C, to control viscosity and leveling without initiating thermal dark-cure. After the build, the platform is raised and parts are drained before solvent cleaning. Cleaning solvents are selected to dissolve uncured surface resin without penetrating the green network; prolonged solvent immersion produces edge softening and dimensional drift. After cleaning, parts are dried at room temperature or with forced air before entering the UV postcure chamber. A staging fixture should rotate or invert the part so that down-facing surfaces and undercuts receive photon exposure; otherwise under-cured regions can creep under clamp load during downstream machining.

    PropertyTypical valueTest method
    Liquid viscosity at 30 °C0.26 Pa·s (260 cP)ASTM D2196-20
    Liquid density at 25 °C1.13 g/cm³ASTM D4052-22
    Tensile strength56 MPaASTM D638-14
    Tensile modulus2700 MPaASTM D638-14
    Elongation at break5.0 %ASTM D638-14
    Flexural strength84 MPaASTM D790-17
    Flexural modulus2450 MPaASTM D790-17
    Notched Izod impact22 J/mASTM D256-10
    Heat deflection temperature at 0.46 MPa64 °CASTM D648-18
    Heat deflection temperature at 1.82 MPa57 °CASTM D648-18
    Shore D hardness84ASTM D2240-15

    The table reproduces manufacturer-reported typical values as published in supplier technical documentation. These values are not guaranteed limits and are not to be used as design allowables without part-specific validation.

    Processing conflicts arise when the build chamber temperature drifts outside the recommended window. A low vat temperature raises viscosity and produces incomplete recoating, visible as voids on upper surfaces and delamination at layer boundaries; a high vat temperature shortens dark-cure shelf life and may accelerate premature cationic advancement in the vat. On platforms with a tilt-separation mechanism, large flat layers generate higher peel forces than narrow sections; supports should be distributed so that peel stress does not localize at part corners. Green parts are softer and more notch-sensitive than fully cured material, so support removal before UV flood exposure should use flush cutters rather than snapping. The postcure chamber must be monitored with a radiometer because lamp output decays over time; a drop below the lower end of the 320 nm to 390 nm band reduces through-thickness conversion even if surface dry time appears normal. For sections thicker than 6 mm, published data for this specific configuration is limited, and staged postcure with thermal equilibration is advised.

    Incoming batch verification on a production line often includes a viscosity measurement at 30 °C and a cure-depth test on a short build platform. Viscosity readings above the manufacturer acceptance range can sometimes be reduced by raising the vat temperature, but only within the stated maximum; batches with photo-speed drift may require exposure compensation through build software. The single-component cationic resin does not require mixing with an accelerator before charging the vat; however, resin left in an open vat for several days should be stirred gently to homogenize the photoacid generator and dissolved moisture content. Vat films or glass windows must remain free of polymerized crumbs because debris trapped under the recoat blade creates drag lines. These batch and equipment interactions are the main production-scale failure modes observed with epoxy photopolymers of this viscosity class.

    When Rigid Epoxy Accuracy Is Preferred Over ABS-Like Toughness or High-Heat Filled Resins

    In resin selection within the same stereolithography portfolio, DSM Somos 7120 is categorized by higher tensile modulus and lower elongation than ABS-like materials such as DSM Somos NeXt. The low elongation at break, near 5 %, means that snap-fit features and living hinges are not appropriate without stress-relief geometry; ABS-like resins can absorb greater strain before fracture. By contrast, high-temperature filled epoxies such as DSM Somos PerFORM shift heat deflection temperature above 200 °C and are selected for molding inserts or high-temperature wind-tunnel parts. The 7120 heat deflection temperature under a 0.46 MPa load is below 100 °C, making it unsuitable for applications where the part surface is exposed to boiling water, autoclave steam, or repeated solder reflow temperatures. Compared with optically clear resins such as DSM Somos WaterShed XC 11122, the 7120 product is not engineered for low moisture absorption or long-term water-service clarity. Its visible light transmission is lower, and absorbed water plasticizes the network; dimensional change can occur if the part is transferred from a dry room to a humid assembly floor without conditioning. In terms of post-processing, the UV postcure requirement is more stringent than for some laser-only acrylate systems, but the lower viscosity and vat stability make the 7120 formulation easier to recoat across large build zones. Users should not substitute 7120 for USP Class VI or ISO 10993-certified resins unless the intended device is evaluated under the relevant biocompatibility test plan.

    Moisture absorption affects the cured polymer through a measurable depression in heat deflection temperature and tensile modulus after prolonged humidity exposure. Parts held at relative humidity above 60 % should be dried at 40 °C to 50 °C before critical dimensional inspection or mechanical testing; the drying temperature must remain below the heat deflection temperature to prevent creep. The liquid resin is incompatible with free-radical acrylate initiators, strong nucleophiles, and organometallic curing agents not approved by the manufacturer; mixing with other resin families can arrest the cationic cure or generate nonuniform gelation. Vat equipment should be cleaned with the resin manufacturer’s recommended solvent and not with aggressive ketones or chlorinated solvents that can degrade seals and carry residue into subsequent builds. Because the uncured resin is a sensitizer, handling requires nitrile gloves, safety glasses, and local exhaust ventilation; cured parts are non-hazardous for ordinary handling but must not be ground or sanded without dust extraction. The product is subject to chemical inventory reporting under REACH Regulation EC No 1907/2006 and the RoHS Directive 2011/65/EU; a current safety data sheet and regulatory statement should be requested from the supplier for shipment-specific documentation.

    A specific production application is the fabrication of wind-tunnel test models for low-temperature aerodynamic campaigns. After stereolithography build and UV postcure, the surfaces are sanded and filled with a compatible epoxy primer; pressure taps are added by drilling and bonding metal or polymer tubing. The cured resin’s modulus and dimensional accuracy sustain machining, but the maximum stagnation temperature must be kept below the heat deflection temperature of 64 °C at 0.46 MPa. Models used in smoke-visualization tunnels may require additional sealing to reduce surface porosity and moisture uptake. In tooling use, 7120 master patterns are frequently used to cast room-temperature vulcanizing silicone cavities for polyurethane prototypes; the postcured epoxy pattern resists abrasion during demolding and holds dimensional tolerance when stored at stable humidity.

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