| HS Code | 654360 |
| Product Name | 3D Systems VisiJet SL HiTemp |
| Manufacturer | 3D Systems |
| Material Type | Stereolithography resin |
| Color | Amber |
| Density | 1.12 g/cm³ |
| Viscosity | 500 cps at 25°C |
| Tensile Strength | 59 MPa |
| Tensile Modulus | 2,700 MPa |
| Elongation At Break | 5% |
| Flexural Strength | 95 MPa |
| Flexural Modulus | 2,800 MPa |
| Hardness | 85 Shore D |
| Heat Deflection Temperature At 0 45 Mpa | 120°C |
| Heat Deflection Temperature At 1 82 Mpa | 100°C |
| Glass Transition Temperature | 130°C |
| Notched Izod Impact | 25 J/m |
| Water Absorption | 0.4% |
As an accredited 3D Systems VisiJet SL HiTemp factory, we enforce strict quality protocols—every batch undergoes rigorous testing to ensure consistent efficacy and safety standards.
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During coolant system form-fit validation on passenger vehicle platforms, the resin is applied as a single-component vat photopolymer at a formulation addition ratio of 100% neat resin; no reactive diluent, acrylate blend, or solvent addition is recommended because dilution beyond 0.5 wt% shifts the photopolymerization gel point and leaves tacky, undercured fillets around blind pump volute walls. Lot-to-lot viscosity variation requires recoat blade gap adjustment on production-scale ProX 800 systems; visible recoat streaks at 50 µm layers and increased first-layer peel force can occur when cross-sectional area jumps across the vat, a common failure mode on large automotive housings. Thermal and mechanical compliance for coolant-contacting prototype housings is assessed under ISO 527-2:2012, ASTM D648-18 at 0.46 MPa, REACH Regulation (EC) No 1907/2006, and RoHS Directive 2011/65/EU, Annex II. Downstream processing consists of 355 nm galvanometer-driven laser scanning in a 3D Systems ProX 800 vat; green parts are washed in 99% isopropyl alcohol and UV post-cured in a 3D Systems ProCure 750 chamber until tensile modulus stabilises, with drain holes placed in pump volute hollow sections to avoid trapped solvent vapour and post-cure cracking. Terminal products include coolant pump volute prototypes, thermostat cover test units, EGR coolant bypass housing mock-ups, and coolant reservoir fitment gauges. The operational boundary is strict: published HDT at 0.46 MPa is 65 °C, while continuous contact with ethylene glycol/water at 80 °C is not supported; published data for long-term glycol immersion above 65 °C is limited, and dimensional drift at heat-soak conditions above 60 °C must be monitored by intermittent fixture checks.
A production-scale SLA line producing connector housings for under-dash electronics is typically set to 100% neat resin fill; the formulation addition ratio excludes conductive filler or flame-retardant powder above 0.5 wt% because filler loading beyond this threshold raises vat viscosity into a range that produces recoat artefacts at 50 µm layer intervals. The evaluation protocol aligns with UL 94 at 1.5 mm specimen thickness for flammability classification, ASTM D648-18 at 0.46 MPa for heat deflection, ISO 527-2:2012 for tensile properties, and RoHS Directive 2011/65/EU for restricted substances. Processing consists of stereolithography on a ProJet 6000 HD or ProX 800 platform, followed by immersion in 99% isopropyl alcohol and UV post-cure; hollow connector shells require vent holes to prevent solvent pooling that causes delayed cracking along the shell parting line. Terminal parts include D-sub connector shell prototypes, wire-to-board connector housings, under-dash sensor enclosures, and relay cover test articles. The material is not suitable for solder reflow exposure; published HDT at 0.46 MPa is 65 °C, and continuous service above 60 °C is not recommended without external support ribs to maintain dimensional stability.
Running industrial fluid manifold and impeller prototypes at 40–50 °C water-glycerol flows uses the resin as a 100% neat vat photopolymer; no additional wetting agent or antifoam should be added beyond 0.2 wt%, because surfactant addition disrupts the photoinitiator dissociation path and produces soft undercured sections in blind channels. Relevant standards are ISO 527-2:2012 for tensile modulus, ISO 178:2010 for flexural properties, ASTM D638-14 for comparative plastic tensile data, and REACH Regulation (EC) No 1907/2006 for substance registration. Downstream processing is vat photopolymerization on a ProX 800 using 50 µm layers; after build, the component is solvent-washed, air-dried, and UV post-cured, then internal channels are flushed with low-pressure argon to remove residual isopropanol before flow testing. Terminal parts include test impellers, valve body prototypes, pump casing flow-visualization mock-ups, and manifold split-planes. Cavitation erosion data for this material is limited; impeller prototypes should be restricted to cold-flow tests below 40 °C rather than production pump duty.
In cabin air distribution mock-ups, the principal failure mode is not mechanical yield but dimensional drift after repeated exposure to 55–65 °C dry air. The resin is loaded as the sole reactive photopolymer at 100% vat fill; no flame-retardant powder or brominated additive is introduced at the conversion stage, because a dispersion loading above 1 wt% attenuates UV penetration and produces unbonded internal laminations. Compliance screening uses UL 94 at 1.5 mm thickness for flammability, ASTM D648-18 at 0.46 MPa for HDT, ISO 178:2010 for flexural modulus, and RoHS Directive 2011/65/EU, Annex II for restricted substance concentrations. Downstream production is performed on a 3D Systems ProX 800 stereolithography system at 50 µm layer thickness, with build orientation set to minimise stair-step on curved duct inner walls; after alcohol wash and UV post-cure, the duct sections are assembled with acrylic adhesive and checked for pressure drop. Terminal parts include air distribution plenums, diffuser mock-ups, air mix housing prototypes, and ventilation nozzle test pieces. This material is not FAA smoke density or vertical burn certified; the UL 94 HB classification does not authorise flight use.
Thermoforming fixture inserts printed from the resin encounter cyclic contact with heated tool surfaces rather than continuous part immersion. The resin is applied undiluted at a formulation addition ratio of 100%, with no glass or carbon fibre addition above 2 wt% because high filler content raises viscosity beyond the recoat window and generates edge curl during layer curing. Mechanical verification is conducted under ISO 178:2010 for flexural properties, ASTM D648-18 at 0.46 MPa for thermal deflection, and REACH Regulation (EC) No 1907/2006 for substance registration. Processing consists of stereolithography on a ProJet 6000 HD using 50 µm layers, followed by isopropyl alcohol wash, UV post-cure, and drilling of vacuum holes; the insert is mounted on an aluminium base plate to reduce thermal warpage. Terminal products include vacuum forming fixtures, drill jig inserts, assembly alignment nests, and low-temperature thermoforming tooling for PET and PS sheet. Because the published HDT at 0.46 MPa is 65 °C, sheet temperatures above 80 °C at the insert surface require forced cooling or substitution with a ceramic-filled SLA resin.
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3D Systems VisiJet SL HiTemp is an amber-tinted photopolymer resin formulated for high-temperature stereolithography on 355 nm laser platforms in the ProJet 6000 and ProJet 7000 series. The material is used where short-cycle thermal exposure exceeds the capacity of general-purpose clear SLA resins but full ceramic-filled SLA is not required. Under ASTM D648, a fully post-cured specimen typically exhibits a heat deflection temperature of 130 °C at 0.45 MPa and 65 °C at 1.82 MPa. Tensile testing per ASTM D638 yields a typical ultimate tensile strength of 50 MPa and a tensile modulus of 2,830 MPa. These values are orientation-dependent; SLA builds produced at 100 μm layer thickness retain measurable Z-axis anisotropy in tensile and flexural response. The amber tint reduces optical clarity compared with clear SLA grades but permits visual inspection of internal flow channels during thermal testing. The cured network is a cross-linked thermoset; it does not melt in secondary thermal processes.
| Property | Test Method | Representative Value |
|---|---|---|
| Tensile strength | ASTM D638 | 50 MPa |
| Tensile modulus | ASTM D638 | 2,830 MPa |
| Elongation at break | ASTM D638 | 2–4% |
| Flexural strength | ASTM D790 | 76 MPa |
| Flexural modulus | ASTM D790 | 2,800 MPa |
| Heat deflection temperature at 0.45 MPa | ASTM D648 | 130 °C |
| Heat deflection temperature at 1.82 MPa | ASTM D648 | 65 °C |
| Density | ASTM D792 | 1.18 g/cm³ |
HDT is a short-term thermal mechanical measurement performed at a fixed flexural stress. A specimen is heated at a controlled rate while under three-point bending; the temperature at which deflection reaches a defined strain is recorded. The 0.45 MPa result of 130 °C does not imply that the material can carry structural load continuously at 130 °C. Under sustained load at that temperature, creep and stress relaxation in the cross-linked network may produce dimensional change and eventual fracture. The 1.82 MPa HDT of 65 °C is a more conservative reference for load-bearing applications. For continuous service above 65 °C, the design should include creep testing under the actual stress state and thermal environment, or finite-element verification using temperature-dependent modulus data. The datasheet HDT values are useful for material screening but should not be substituted for long-term heat aging data.
At a clamped metal joint, local compressive stress often exceeds 0.45 MPa due to bolt preload. Even if the bulk temperature is below the 0.45 MPa HDT, localized creep can loosen the joint. In under-hood components subject to thermal cycling between 25 °C and 100 °C, bolt-hole edges exhibit stress concentration. A conservative design uses metal inserts or bonded washers to distribute load and prevent localized deformation. The resin’s glassy-state coefficient of linear thermal expansion is in the range of 70–90 ppm/°C below the glass transition, which is several times higher than aluminum at approximately 23 ppm/°C. Differential expansion over a 75 °C temperature rise can produce sufficient strain to crack thin sections at mechanical restraint points.
Build orientation strongly alters mechanical response. In vertical builds, cured layers lie perpendicular to tensile load; failures typically initiate at interlayer boundaries. In horizontal builds, tensile specimens cut from the XY plane can exceed the datasheet tensile strength by 10–20%, while vertical Z-axis specimens often fall below the datasheet value by a similar margin. The support contact pattern removes material from the down-facing surface, and sanding or polishing can reduce external defects but does not homogenize cross-link density. For structural prototypes, the primary tensile load should be placed in the XY plane. When this is not possible, mechanically critical parts should be tested in the build orientation used for production. Laser exposure and 100 μm layer thickness create finite interlayer boundary regions with slightly lower conversion than the bulk XY plane; this effect is not fully eliminated by UV post-cure.
The resin is often specified for flow rigs and thermal mock-ups because the amber tint permits visual inspection of internal channels while the cross-linked network retains shape at temperatures that soften clear SLA grades. In a heated airflow test at 80 °C, the difference in HDT under 0.45 MPa becomes operationally meaningful; the part retains shape during short-cycle testing. However, wall sections below 1 mm may still distort under clamping loads because local stress concentrates and the thin cross-section cannot distribute bending moment. Mounting fixtures should distribute load with metal backing plates or contoured silicone pads. Use of the material in pressurized flow loops requires hydrostatic pressure validation per ISO 527 or the applicable pressure-vessel standard; published data for this specific configuration is limited. Transparent SLA materials also show light scattering at layer interfaces, so optical access is best through a polished flat window section rather than curved internal walls.
Moisture uptake in cured SLA resins is generally lower than in powder-bed thermoplastics, but dimensional expansion can occur in humid environments. Parts should be stabilized in the intended service humidity before critical metrology. Water absorption per ASTM D570 after 24 h immersion should be verified for the actual post-cure state; published data for this specific configuration is limited. Hydrocarbon and glycol exposure may plasticize the outer surface and reduce glass transition. Compatibility testing per ISO 175 with the actual fluid is required before fluid-contact applications. In engine bay environments, exposure to hot oil mist can cause surface tack and microcrack propagation at sharp internal corners if the part is not sealed or coated. A chemical-resistant coating may improve performance, but adhesion to the cross-linked acrylate surface must be verified by cross-hatch adhesion testing per ISO 2409 or ASTM D3359.
Green-state parts on SLA platforms retain uncured resin films in blind holes and narrow slots. Primary cleaning with isopropyl alcohol in an ultrasonic bath for 5–10 min is standard for amber SLA materials, but long solvent residence can swell the surface and induce microcracking. Pressurized air drying after solvent wash prevents residual solvent from trapping in closed channels. Support nubs are removed before final UV post-cure to avoid locked-in stress at the attachment points. A thermal post-cure is then used to advance cross-linking; residual internal stress may release as minor warpage in long thin sections. Datasheet mechanical values assume a complete post-cure cycle and should not be applied to green-state parts. On production lines, side-wall delamination occurs when solvent remains in deep pockets before UV post-cure; residual isopropyl alcohol vaporizes during the thermal ramp and produces blisters at the down-facing surface.
Post-cure ovens with 365–405 nm fluorescent UVA sources are appropriate when the resin manufacturer’s dose and temperature schedule is followed. The part surface should be dry and free of solvent before post-cure. Rotation during post-cure reduces shadowing, especially in internal channels. Large parts may require staged thermal ramp profiles to prevent residual stress buildup; published data for this specific configuration is limited.
Resin storage in the vat requires controlled temperature and exclusion of ambient UV. Long idle periods allow separation or moisture uptake; the vat should be recirculated or stirred before starting a build. Viscosity at processing temperature influences recoat thickness and surface accuracy. If the resin falls below the supplier’s minimum temperature, recoat thickness becomes inconsistent and the first layers may delaminate from the platform. Heated build chambers with set points near 30 °C are typical on 355 nm SLA platforms, but the operator should follow the machine-specific resin profile loaded by the 3D Systems software.
Compared with optical clear SLA grades, VisiJet SL HiTemp shifts the ASTM D648 heat deflection temperature at 0.45 MPa upward while reducing visible light transmittance. The amber tint excludes it from applications where color neutrality or optical clarity is the primary requirement. Compared with impact-modified SLA matrices, HiTemp exhibits lower elongation at break under ASTM D638, typically in the 2–4% range, while the elevated cross-link density raises thermal deflection. This combination positions the material for under-hood clips, wind tunnel test articles, and mold inserts that experience short thermal spikes rather than high-impact loading. It is not a direct substitute for ceramic-filled SLA grades, which may provide higher heat deflection temperature but with higher viscosity and abrasive wear on recoater blades. Selection should be based on the full property bundle: thermal deflection, tensile modulus, elongation, and dimensional tolerance after post-cure.
High-temperature SLA material selection often begins with the 1.82 MPa HDT because that value reflects the more demanding flexural stress state. If an application is stress-relaxed, the 0.45 MPa HDT can be referenced for short dips in oven temperature. However, if the part is clamped, bolted, or press-fitted, the lower-stress HDT overstates safe operating temperature. The product’s stated 65 °C value at 1.82 MPa is therefore a practical upper reference for mechanically restrained service; unreinforced thermosets under continuous load should not be expected to perform at the 130 °C single-point deflection temperature.
Thermal cycling from −20 °C to 120 °C can initiate microcracks at sharp internal corners in unreinforced SLA thermosets. Adding fillets with a radius of at least 1.5 times the local wall thickness reduces stress concentration. In field-use observations on SLA-built tooling, cracking generally appears first at the junction between a thick boss and a thin web because differential cooling rates during build and post-cure create residual stress. Dilatometric measurements should be performed on test coupons in the intended build orientation before committing to production; published data for this specific configuration is limited. The material is not recommended for continuous exposure to strong alkaline solutions because ester linkages in the cross-linked network can hydrolyze, resulting in surface etching and loss of mechanical strength. Acidic or neutral aqueous environments are less aggressive, but immersion testing per ISO 175 is required.