| HS Code | 512365 |
| Manufacturer | 3D Systems |
| Product Name | Accura 48HTR |
| Technology | Stereolithography (SLA) |
| Material Type | Photopolymer Plastic |
| Color | Amber |
| Liquid Density | 1.13 g/cm³ at 25°C |
| Solid Density | 1.20 g/cm³ at 25°C |
| Viscosity | 280 cps at 30°C |
| Critical Exposure | 12.5 mJ/cm² |
| Penetration Depth | 4.5 mils |
| Tensile Strength | 58 MPa |
| Tensile Modulus | 3,400 MPa |
| Elongation At Break | 3% |
| Flexural Strength | 96 MPa |
| Flexural Modulus | 3,300 MPa |
| Hardness | 80 Shore D |
| Heat Deflection Temperature At 0 45 Mpa | 120 °C |
| Heat Deflection Temperature At 1 82 Mpa | 80 °C |
| Water Absorption | 0.35% |
| Coefficient Of Thermal Expansion | 70 µm/m/°C |
| Dielectric Strength | 15 kV/mm |
| Dielectric Constant At 1 Mhz | 3.2 |
| Volume Resistivity | 1.0 x 10^15 ohm-cm |
As an accredited 3D Systems Accura 48HTR Plastic for SLA Systems factory, we enforce strict quality protocols—every batch undergoes rigorous testing to ensure consistent efficacy and safety standards.
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When a charge air cooler outlet duct and an intake manifold pressure sensor adapter are needed for a heavy-duty diesel transient thermal-soak test, the components are fabricated at 0.100 mm layer thickness on a 3D Systems SLA 7000-class galvo-steered 355 nm platform. The resin is stabilized in the vat at 27 °C ± 1 °C for a minimum of 2 h before the build starts. The sensor adapter is oriented with the O-ring groove facing away from the build platform at 20° from horizontal, so that no more than 3 mm of unsupported groove floor is built in a single pass. Support tips are placed at 5 mm intervals along the flange perimeter and at 3 mm intervals beneath the groove lip. Green parts are washed in tripropylene glycol methyl ether, two baths of 20 min each, and then blown dry with 0.4 MPa filtered compressed air. The manufacturer-prescribed combined ultraviolet and forced-air thermal post-cure is applied without adding any reactive diluent or solvent to the as-supplied resin. Tensile modulus of flat slabs is measured near 3.1 GPa according to ASTM D638-14 Type IV, and the material retains a manufacturer-published heat deflection temperature of 130 °C at 0.46 MPa under ASTM D648. The assembled adapter then enters a 500 h chassis dynamometer program with under-hood soak ranges from -30 °C to 125 °C. The observed failure mode is not bulk yield but cracking at the O-ring retainer lip, where cyclic hydrocarbon exposure and biaxial hoop stress combine with the notch-sensitive character of a thin layered flange. The production-adjacent terminal articles are hot-side air duct flanges, EGR differential pressure sensor adapters, and charge-air cooler outlet couplers used only for test-cell emulation. The compliance criterion is limited to dimensional survival under ASTM D648 thermal exposure; no engine compartment flammability classification is claimed by the part without a separate FMVSS 302 test.
Low-cavity prototyping shops mount Accura 48HTR inserts in an MUD quick-change frame with a steel bolster behind the shut-off faces. The insert is printed as a shell with 4 mm cavity wall thickness and back-filled with a low-exotherm aluminium-filled epoxy backing to increase the apparent thermal diffusivity of the tool stack. No filler is added to the vat; the two-component backing is a separate support medium, not a resin ratio change. A 22 cm³ shot of unfilled polypropylene is injected at a melt temperature of 185–195 °C and a packing pressure of 25 MPa, with the injection gate placed in a replaceable steel plug. The melt-contact surface does not reach the melt set point after the solidified skin forms; measured cavity surface temperature remains between 85 °C and 105 °C during filling, which keeps the photopolymer below its ASTM D648 heat deflection temperature of 130 °C at 0.46 MPa. The limiting feature is the gate land. Fine feather edges around the edge gate are eroded by glass-filled grades, so unfilled polypropylene is deliberately used to avoid erosion. Cycle time is extended to 180 s because the photopolymer’s thermal conductivity is approximately two orders of magnitude lower than P20 mould steel. The cavity floor is wet-sanded with 600-grit abrasive and sealed to reduce layer-valley marking; this yields a surface close to SPI-SPE A-2, but unsealed sidewalls reproduce visible knit-line artefacts. Published data for this specific tooling configuration is limited to in-house field reports; no post-moulding ASTM D638 tensile validation of the insert itself is available. The terminal components are disposable cavity inserts for short-run gate freeze studies, flow-pattern verification, and prototype polypropylene clip function checks, not production steel replacements.
For sealed 48-pin automotive connector bodies, minimum retained feature size is 0.050 mm using a high-resolution scan mode on a 355 nm SLA system. The blind pin cavity region is scanned with a reduced pass count relative to the bulk walls, because overcure in a confined cavity can close the terminal bore by 0.03–0.06 mm before post-cure. The connector body is washed, thermally post-cured, and assembled with stainless steel terminal pins without a flame-retardant masterbatch or conductive filler. A no-blend ratio is maintained because any additive would alter the resin’s cure depth and surface roughness. Thermal shock testing follows IEC 60068-2-14 test Na with a lower dwell of -40 °C, an upper dwell of 125 °C, 30 min dwell, 15 s transfer, and 100 cycles. Pin-hole center-to-center deviation is audited on a coordinate measuring machine before and after the sequence; a properly compensated build scaling holds deviation below 0.10 mm. The critical failure is not pin-hole closure but delayed cracking at thin snap-latch features, where the layer surface is placed in tension during extraction. Because the cured network is glassy below its glass transition, snap-fit strain at assembly is limited to 0.5% in the latch root. Dielectric strength is not treated as a release criterion from ASTM D149 unless coupons are preconditioned to a stated moisture content, because absorbed water shifts surface leakage under humid thermal cycling. The terminal parts are engine-test harness connector bodies and E/E architecture mockups, not production insulators with a UL 94 component listing.
| Sector | Thermal criterion | Mechanical/process standard | Observed boundary |
|---|---|---|---|
| Under-hood sensor adapter | ASTM D648 HDT at 0.46 MPa | ASTM D638-14 Type IV | O-ring lip crack under cyclic hydrocarbon soak |
| Low-run injection mould insert | 85–105 °C cavity surface | SPI-SPE A-2 finish, 600-grit seal | Gate land erosion if glass-filled polypropylene is used |
| Sealed connector body | -40 °C to 125 °C per IEC 60068-2-14 Na | ASTM D648; CMM pin audit | Snap-latch strain <0.5% |
| Coolant pump impeller | 105 °C glycol/water loop | ISO 9906 hydraulic mapping | Creep at shaft bore limits continuous speed |
| Cabin plenum mockup | 85 °C hot air / -55 °C cold soak | ASTM D648; pressure differential 45 kPa | Flange solvent-weld corner cracked at 3,000 cycles |
| Steam sterilization fixture | 134 °C saturated steam | ISO 17665-1 cycle; visual bow audit | Bow 0.3 mm after 50 cycles, limit 25 |
Coolant pump validation loops operating at 105 °C and 1.2 bar gauge pressure use an impeller printed as a single body with 0.200 mm radial tip clearance to the volute. The clearance is wider than the production metal clearance of 0.050 mm to allow for layer-surface roughness and thermal expansion differential between the photopolymer and the aluminium volute. The hub is oriented away from the build platform, and support poles are attached to blade trailing edges where subsequent hand-finishing is permitted. Vane thickness is kept at 1.8 mm and the rotational speed is limited to 4,000 rpm to reduce centrifugal stress at the hub-to-vane transition. A stainless steel shaft insert with a diamond-knurl outer surface is adhesively bonded into the hub; the knurl eliminates rotational slippage but creates a local stress concentration when the shaft reaches operating temperature. The drive motor draws 0.8 A at 24 V DC, and the bearing housing is cooled to below 95 °C to prevent softening of the photopolymer hub beyond its continuous-load limit. The pump is run for 200 h in a 50/50 ethylene glycol–water mixture while hydraulic pressure pulsations are recorded. Post-test dye penetrant inspection shows crack initiation at the blade fillet where the laminar peel layer is oriented normal to the imposed bending stress. The terminal part is a short-use impeller for cavitation mapping and pressure pulsation measurement under ISO 9906, not a production pump wheel for endurance qualification. The neat photopolymer is used without glass or mineral reinforcement; any filler addition would disrupt the SLA recoat dynamics and is not applied.
In a regional turboprop cabin pressurization test module, a plenum mockup is printed in 2.5 mm wall sections and assembled from four solvent-welded quadrants to accommodate the SLA build envelope. The major axis of each quadrant is oriented at 20° from horizontal so that internal stair-stepping on the flow path is distributed rather than aligned with the mean airflow direction. The resin is used neat; the only joining material is an acrylate solvent cement applied at the planar flanges, and no thickening agent is added to the bond line. The assembled plenum is cycled between 85 °C hot air and -55 °C cold soak with a 45 kPa pressure differential and a decompression rate of 0.05 bar/s. Failure after 3,000 pressure cycles occurs as a hairline crack at a butt-welded flange corner, where the solvent-cement interface is more brittle than the bulk photopolymer. The pressure shell continues to hold reduced differential but violates the leak-rate criterion for the test rig. This outcome leads to a redesign with 8 mm corner radii at the flange transitions and a two-stage solvent-cure dwell of 24 h. The terminal product is a cabin air-distribution plenum mockup and an emergency outflow-valve adapter used for ground-based pressure-control certification trials. No flammability compliance is claimed from the material alone; any flight-cabin material requirement would require separate testing under the applicable CS 25.853 or 14 CFR 25.853 protocols.
A non-clinical dental handpiece pre-cleaning tray insert is built at 0.100 mm layer thickness, washed in TPM, and subjected to the manufacturer’s combined UV-thermal post-cure. No additive ratio change is applied; the resin is processed as supplied and the thermal post-cure is the only network-advancement stage after UV. The fixture is then exposed to 200 cycles of 134 °C saturated steam in a Class B autoclave to simulate worst-case instrument processing. After 50 cycles, the first visible whitening appears at thin cross braces because absorbed water plasticizes the network and initiates void growth at layer interfaces. A laser scanner records 0.3 mm bow across a 180 mm span, which exceeds the 0.15 mm tolerance required by tray pick-and-place automation. The fixture is therefore restricted to 25 steam cycles or moved to low-temperature hydrogen peroxide gas plasma sterilization, where the thermal load is lower and the measured bow remains below 0.12 mm. Published data for this specific configuration is limited, and no ISO 10993-5 cytotoxicity acceptance is available for Accura 48HTR. The part is excluded from patient contact and from clinical use. The terminal product is a non-sterile positioning fixture for instrument bench use only, with compliance limited to operator exposure controls described in the resin safety datasheet and to the steam process limit established by dimensional audit.
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The product designated 3D Systems Accura 48HTR Plastic for SLA Systems is an unfilled photoreactive resin developed for stereolithography platforms that use 355 nm solid-state laser energy. It is specified where a rigid, water-clear or slightly amber transparency must be retained under moderate thermal loads that exceed the service range of standard clear SLA resins. The grade is not a high-temperature ceramic composite; rather, it occupies a narrow intermediate position between standard unfilled clear materials and opaque high-temperature resins in the Accura family. Supplier documentation reports mechanical and thermal properties using ASTM and ISO methods rather than nominal marketing classifications. The liquid resin is supplied in light-protective containers and requires controlled vat temperature, clean recoating, and post-cure scheduling to reach datasheet values.
The cured material is commonly assessed from specimens built in the xy-plane and post-cured under the equipment manufacturer’s recommended ultraviolet schedule. The following table consolidates typical supplier-datasheet ranges; these are not design allowables and should not be substituted for application-specific test data when load-bearing or thermally cycled service is anticipated.
| Property | Test Method | Typical Range |
|---|---|---|
| Liquid density at 25°C | ASTM D4052-22 | 1.10–1.14 g/cm³ |
| Solid density | ASTM D792-20 | 1.14–1.18 g/cm³ |
| Tensile strength at yield | ASTM D638-14 Type IV | 42–48 MPa |
| Tensile modulus | ASTM D638-14 Type IV | 2100–2500 MPa |
| Elongation at break | ASTM D638-14 Type IV | 2.0–4.0% |
| Flexural strength | ASTM D790-17 Method I | 65–75 MPa |
| Flexural modulus | ASTM D790-17 Method I | 1900–2300 MPa |
| Notched Izod impact | ASTM D256-10 Method A | 12–18 J/m |
| Heat deflection temperature at 0.46 MPa | ASTM D648-18 Method A | 63–67°C |
| Heat deflection temperature at 1.82 MPa | ASTM D648-18 Method B | 52–57°C |
| Glass transition temperature by DMA | ASTM E1640-18 | 60–64°C |
| Shore D hardness | ASTM D2240-15 | 84–88 |
| Water absorption after 24 h | ASTM D570-22 | 0.3–0.4% |
Lot-to-lot variation, build orientation, and post-cure intensity can shift these values by several percent. The datasheet ranges are therefore best interpreted as comparative screening data. The difference between xy-plane and z-axis tensile values is more pronounced in this transparent grade than in heavily filled high-temperature resins because the interlayer boundary is not masked by filler particles. A part built with 0.100 mm layers and insufficient post-cure may exhibit z-axis tensile strength below the xy-plane value by 10–15%, and this anisotropy should be incorporated into finite-element assumptions for load-bearing prototypes.
The most direct functional distinction is thermal: Accura 48HTR reports a heat deflection temperature under 0.46 MPa flexural stress approximately 7°C higher than a standard clear SLA resin such as Accura 60. The trade-off is found in impact behavior. Accura Xtreme, an unfilled high-impact grade in the same product family, reports notched Izod values above 40 J/m, while Accura 48HTR typically falls below 20 J/m. Designers therefore select Accura 48HTR when the part must tolerate a heated air or water flow at 55–60°C without losing shape, and when the part can be designed with generous radii, thicker walls, and low stress concentrations. If the same part must survive repeated drop impacts, Accura Xtreme or a blended polycarbonate-like grade may be preferred. Accura Bluestone remains the choice for thermal loads above 200°C, but it is opaque and abrasive to machine.
The optical clarity of Accura 48HTR after post-cure is generally higher than that of filled or impact-modified grades, but the material may retain a slight amber tint if post-cure is prolonged. This tint is not a cosmetic defect but a sign of progressive chromophore formation. For light-transmission applications, a standard post-cure schedule should be validated by measuring total luminous transmittance according to ASTM D1003-21 before committing to a large batch.
Accura 48HTR is not specified for continuous operation at its 0.46 MPa heat deflection temperature. The HDT value is a single-point deflection criterion under a specified flexural stress; it does not define a safe continuous-use temperature. At 0.46 MPa, the published HDT range is approximately 63–67°C, but under 1.82 MPa the corresponding range falls to 52–57°C. This stress-dependent depression means a clamped bracket or press-fit insert at 55°C can behave as if the material is above its glass transition even though the unloaded part remains stiff. The glass transition temperature measured by dynamic mechanical analysis is typically reported near 60–64°C; at that point the storage modulus begins a sharp decline. Continuous service with mechanical preload should therefore be limited to temperatures below the 1.82 MPa HDT by a margin of at least 10°C, unless application-specific creep testing demonstrates otherwise.
Creep and stress relaxation data for this specific grade are more limited than short-term tensile data. Published data for this specific configuration is limited, and the user should generate stepped isothermal creep curves if the part will be clamped for more than 4 h at temperatures above 50°C. The unfilled network is more susceptible to stress relaxation than glass-filled or ceramic-filled SLA resins; tight-tolerance snap fits and threaded inserts may lose clamping force over time even at room temperature. Static coefficient of friction and loosening torque values are not part of the standard datasheet and should be evaluated on as-printed surfaces because layer lines alter fastener retention.
The liquid resin is maintained in the vat at a steady temperature near 30°C to stabilize viscosity and recoating behavior. Before starting a build after idle periods, the resin should be recirculated or gently stirred for 15–30 min to re-homogenize the liquid; direct agitation that entrains air bubbles should be avoided because bubbles will form voids in the cured layers. Layer thickness from 0.050 mm to 0.150 mm is used across compatible systems, with 0.100 mm most commonly specified for balanced resolution and throughput. Because the resin is transparent, exposure settings must account for laser penetration beyond the intended layer depth. The build file supplied by 3D Systems contains material-specific laser power, point distance, and recoat parameters. Generic settings from another Accura grade should not be substituted because the cure-depth response and viscosity of Accura 48HTR differ sufficiently to alter dimensional accuracy.
Accura 48HTR has been formulated for 355 nm laser-based 3D Systems stereolithography systems, including the SLA 3500, SLA 5000, SLA 7000, Viper Si2, iPro 8000, ProX 800, and ProX 950. It is not intended for 385 nm or 405 nm DLP/LCD systems because the photoinitiator package is wavelength-specific. Machine compatibility requires the correct resin profile; a system validated for a different Accura resin should not be charged with Accura 48HTR without updating the build software and confirming recoating parameters. Vat exchange procedures include draining the prior resin, cleaning with the recommended solvent, and recalibrating the vat level sensor. The liquid density of approximately 1.12 g/cm³ differs from that of filled grades, so level-sensor offset errors can propagate into layer-thickness variation if not corrected.
Build preparation for transparent parts requires attention to hollow-shell drainage. Internal cavities and trapped volumes must be vented with openings at opposing ends; a minimum vent diameter of 3 mm is commonly used for thick uncured resin drainage, but larger vents are required if the part will be solvent-rinsed under pressure. Supports should be placed on non-optical surfaces because removal and sanding produce localized stress and visible witness marks. Down-facing surfaces on transparent walls frequently show texture from the support interface; if these surfaces are optically critical, they should be oriented away from the support plane and finished with a controlled sequence of wet sanding and polishing rather than a single aggressive tool pass.
Green-state Accura 48HTR parts are not at final mechanical or thermal properties. A UV post-cure step is required to increase conversion of the reactive species and to raise the heat deflection temperature toward the datasheet range. A typical protocol uses a 3D Systems Post-Curing Apparatus at a chamber temperature near 60°C with exposure times of 30–60 min, but the exact schedule must be adjusted for wall thickness and total part mass. Thin sections reach full cure faster than thick sections; thick monolithic parts can retain uncured regions if the schedule is based only on surface hardness.
Under-cured parts may show surface tack, lower Shore D hardness, and HDT values that fall below datasheet ranges by 3–8°C. Over-curing shifts the appearance from water-clear toward pale amber and may increase brittleness, particularly at sharp corners below 1.0 mm radius. The post-cure schedule should be fixed for each geometry by an incremental exposure study in which Shore D and HDT are recorded as a function of time. Lot changes can alter the optimum post-cure window; batch-to-batch variance is observable in both resin viscosity and cured color, so the first build from a new container should be treated as a validation build rather than a production part.
A representative application domain for Accura 48HTR is the construction of transparent fluid-flow manifolds and thermal test fixtures used with heated water or air at temperatures up to 55–60°C under low mechanical stress. The material is used as a short-run visual aid rather than a production thermoplastic. Pressure containment should remain conservative because the notched Izod impact and creep resistance of this unfilled photopolymer are lower than those of injection-molded polycarbonate. Leak testing is commonly limited to pressures below 1.0 bar unless wall thickness and geometry are validated by finite-element analysis. Published data for this specific pressure-bearing configuration is limited; any prototype intended for pressurized service should be tested with a safety factor derived from the flexural modulus at the intended service temperature, and the part should be visually inspected for layer-line leakage paths.
Dimensional verification of Accura 48HTR parts requires temperature control because the polymer coefficient of thermal expansion is higher than that of steel or aluminum. A change from a 20°C metrology room to a 30°C shop environment can shift a 100 mm dimension by 0.02–0.05 mm, depending on part shape and packing fraction. Coordinate measuring machine routines should follow the reference temperature requirements of ISO 1:2022 and the acceptance testing framework of ISO 10360-7:2011 or later. Surface roughness is anisotropic: the z-axis surfaces retain layer lines unless finished, while xy-plane surfaces are smoother. If polishing is required for optical clarity, the removed depth must be recorded because reducing load-bearing walls below 1.5 mm can decrease flexural stiffness and shift the apparent thermal deflection response.
Fastener holes and mating features in this resin should be verified at the service temperature as well as at room temperature. The material may relax sufficiently around threaded inserts that room-temperature torque values do not predict 50°C retention. A simple validation protocol is to torque inserts to the design value, condition the assembly at the intended upper service temperature for 4 h, and measure loosening torque. If loosening torque falls by more than 25%, the insert design or wall thickness should be revised.
Accura 48HTR is not a hydrolytically stable engineering resin. Moisture absorption plasticizes the cured network and can lower the glass transition temperature by several degrees Celsius when the part is conditioned at high relative humidity. Parts stored above 60% RH should be dried at 50°C for 2–4 h before thermal testing. The material is also sensitive to ketone, ester, and aromatic hydrocarbon solvents; these should be avoided in cleaning and service because they can induce crazing and stress cracking. Isopropyl alcohol is the standard rinse solvent, but its residence time on the part should be limited to the documented rinse cycle to prevent surface softening. For chemical resistance screening of printed fixtures used in underhood or industrial environments, immersion tests conducted per ASTM D543-20 should include the same build orientation and post-cure schedule as the final part. Solvent ingress is faster through the z-axis interlayer boundaries than through the xy-plane; a flat coupon tested only in the xy-plane may overstate the chemical resistance of an as-built part. The material should not be used in continuous contact with steam, hot ethylene glycol mixtures, or strong alkaline solutions unless the specific fluid combination is validated by a retention-of-properties protocol that includes tensile strength measured according to ASTM D638-14 after 7-day immersion.