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3D Systems DuraForm ProX HST Composite Thermoplastic Elastomer for SLS Systems

    • Product Name: 3D Systems DuraForm ProX HST Composite Thermoplastic Elastomer for SLS Systems
    • 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 184066
    Material Type Composite Thermoplastic Elastomer
    Compatible Technology Selective Laser Sintering (SLS)
    Color Black
    Density 1.08 g/cm³
    Shore A Hardness 75
    Tensile Strength 4.8 MPa
    Tensile Modulus 35 MPa
    Elongation At Break 180%
    Tear Strength 25 kN/m
    Compression Set 30%
    Rebound Resilience 45%
    Particle Size 50-60 µm
    Melting Point 175-185 °C
    Heat Deflection Temperature 80 °C at 0.45 MPa
    Moisture Absorption <0.5%
    Chemical Resistance Good to oils and greases

    As an accredited 3D Systems DuraForm ProX HST Composite Thermoplastic Elastomer for SLS Systems factory, we enforce strict quality protocols—every batch undergoes rigorous testing to ensure consistent efficacy and safety standards.

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    More Introduction

    3D Systems DuraForm ProX HST Composite Thermoplastic Elastomer for SLS Systems is a filled powder feedstock for selective laser sintering platforms including the ProX SLS 500 and sPro 140/230. The product is supplied as a dry, free-flowing particulate blend with a particle size distribution and melt-flow profile formulated for counter-rotating roller recoating at layer thicknesses of 100–120 µm. Processing literature supplied with the powder describes the matrix as a thermoplastic elastomer whose filler phase raises the heat deflection response and reduces cold-flow in comparison with unfilled TPU grades. The as-supplied powder must be stored in sealed containers at temperatures below 30 °C and acclimated to the build environment for 6–12 h before loading to avoid electrostatic agglomeration and humidity-induced powder bridging.

    What processing boundaries must be observed when a filled TPE composite is run on a 30 W CO₂ SLS platform?

    On a 30 W CO₂ laser system equipped with a 0.4 mm beam diameter, the usable part-bed temperature window for this powder typically lies between 150 °C and 170 °C, depending on the virgin-to-reclaimed powder ratio and installed thermocouple calibration. The lower boundary is defined by edge curl and delamination, while the upper boundary is limited by part growth, rough sidewalls, and premature consolidation of surrounding powder. Laser fill power is normally set between 24 W and 36 W, with scan speeds of 8–12 m/s and scan spacing of 0.15–0.20 mm. These parameters are not independently tunable; an increase in scan spacing reduces total energy density and may produce porous interlayer fusion unless laser power is raised or scan speed is reduced.

    Nitrogen purge is required to maintain oxygen below 1.5 vol% in the build chamber. Exceeding this threshold during long builds increases the risk of oxidative yellowing, molecular weight breakdown, and reduced elongation at break. After the laser pass, the part cake should be cooled within the build chamber at a controlled rate of 0.3–0.5 °C/min until the surface temperature falls below 45 °C; removal at higher temperatures induces warpage in flat sections and widens the dimensional tolerance band in the Z axis.

    Powder refresh management is critical because the composite filler and elastomer matrix do not degrade at the same rate. Open-loop machines running lightly packed builds may operate with 20–30% virgin powder, while closed-loop systems with dense packing and absorbed moisture from blast media may require 30–50% virgin powder to maintain consistent melt-flow index. The melt-flow index is measured according to ISO 1133-1:2022 at 190 °C with a 2.16 kg load; a shift of more than 15% from the initial powder lot indicates that the reclaimed fraction should be reduced or the sieve mesh should be inspected for openings larger than 150 µm.

    Differential scanning calorimetry of the powder under ISO 11357-1:2023 typically displays a broad melting endotherm between 140 °C and 175 °C, rather than the sharp melt peak observed in unfilled PA12. This broad endotherm means that the part-bed temperature control loop must hold the powder bed in the lower portion of the melting range. If the control thermocouple drifts by ±2 °C, the surface of the feed region may enter the tacky plateau and cause roller slip or non-uniform layer deposition. Production-scale builds on the ProX SLS 500 have shown that periodic infrared thermography of the feed bed reduces this failure mode by identifying cold bands before the roller engages.

    Mechanical anisotropy between the X-Y plane and the Z build direction is intrinsic to laser-sintered elastomer composites and must be treated as a design input rather than a defect. When specimens are printed in the X-Y orientation and tested according to ASTM D638-14 Type IV, the supplier-published representative values for this grade include a tensile modulus near 1,000 MPa, tensile strength near 18 MPa, and elongation at break near 25%. The corresponding Z-orientation values are typically 20–30% lower for modulus and 30–40% lower for tensile strength. Flexural modulus, determined under ASTM D790-17 Method I, is reported near 950 MPa in the X-Y plane. Shore D hardness under ASTM D2240-15e1 is approximately 62. Heat deflection temperature is 95 °C at 0.455 MPa and 55 °C at 1.82 MPa according to ASTM D648-16.

    Notched Izod impact under ASTM D256-10 shows strong retention at low temperature relative to unfilled TPU, but the composite filler reduces the capacity for repeated high-strain flexing. Parts with snap-fit arms or living-hinge features should be derated by a stress concentration factor of at least 1.5 when the bending axis is oriented in the Z direction. Post-build bead blasting with 80–120 mesh glass media at 250–350 kPa is the preferred surface treatment; solvent polishing is not recommended because the elastomeric matrix can swell and release filler particles.

    PropertyTest methodReported value
    Tensile modulus, X-YASTM D638-141,000 MPa
    Tensile strength, X-YASTM D638-1418 MPa
    Elongation at break, X-YASTM D638-1425%
    Shore D hardnessASTM D2240-15e162
    Flexural modulus, X-YASTM D790-17950 MPa
    Heat deflection temperature at 0.455 MPaASTM D648-1695 °C
    Heat deflection temperature at 1.82 MPaASTM D648-1655 °C
    DensityISO 1183-1:20191.10 g/cm³

    Compared with DuraForm ProX PA and DuraForm ProX GF, the filled elastomer grade produces lower flexural modulus and higher notched impact energy, making it less suitable for stiff structural brackets but more capable for vibration-isolating brackets and snap-fit clamps. Against DuraForm Flex TPU, the composite grade provides higher tensile modulus and greater resistance to creep at elevated temperature, but lower ultimate elongation and less Shore A softness. The filler phase also increases melt viscosity, which narrows the laser sintering window and makes the material more sensitive to powder age than unfilled PA12. Cross-contamination with PA12 or glass-filled powders is undesirable because the two powders have different melting onset temperatures and can produce weak interlayer fusion if mixed in the same build.

    Chemical resistance, moisture conditioning, and post-fusion finishing constraints

    Immersion testing under ISO 175 at 23 °C for 7 days shows that the filled elastomer retains tensile strength after exposure to aliphatic hydrocarbons, mineral oil, and diluted hydraulic fluids, but exhibits swelling and hardness loss in ketones, esters, and chlorinated solvents. The material should not be used in continuous contact with strong acids, strong bases, or oxidizing agents. Moisture absorption under ASTM D570-98(2018) is below 0.6% at 23 °C and 50% RH; however, exposure to relative humidity above 60% for more than 24 h requires pre-drying at 70 °C for 4 h in a desiccant dryer before laser processing.

    Post-fusion finishing is limited by the elastomer-filled microstructure. Bead blasting is the standard method for removing surface powder, while vibratory finishing with ceramic media can abrade the matrix and expose filler particles, creating a rough surface. If vapor smoothing is applied to reduce staircase artifacts, the processor must re-qualify tensile elongation and notched impact because solvent uptake in the amorphous elastomer phase can shift the ductile-to-brittle transition. Thin-wall sections below 1.0 mm should be fixtured during bead blasting to prevent local overheating and permanent deformation.

    Plasticizer or processing-aid migration is not reported for this filler-stabilized elastomer, but prolonged contact with plasticized PVC or certain pressure-sensitive adhesives may extract low-molecular-weight fractions and stiffen the surface. Users should validate initial tack, peel strength, and solvent wipe resistance using ASTM D903-98(2017) or equivalent before specifying the material in bonded assemblies.

    When the filled elastomer replaces unfilled TPU or glass-filled PA12 in production service

    Substitution of 3D Systems DuraForm ProX HST Composite Thermoplastic Elastomer for unfilled TPU is justified when a component requires higher tensile modulus and better dimensional stability under load at 70–90 °C, but does not require elongation values above 25%. Applications in low-pressure fluid ducts, protective bellows, vibration-isolating clips, and impact-resistant covers fall within this envelope. The replacement of glass-filled PA12 is justified when impact toughness and lower stiffness are more important than ultimate flexural modulus; however, the design must accommodate a larger coefficient of thermal expansion and lower heat deflection temperature at 1.82 MPa.

    In moving-part assemblies, minimum clearances should be set at 0.4 mm for parts printed with 100 µm layer thickness and 0.6 mm for 120 µm layer thickness to account for the coarse sidewall melt zone and post-processing tolerance. Snap-fit engagement force is more stable across temperature if the snap feature is oriented in the X-Y plane and the root radius is maintained at 0.8 mm or greater. Published fatigue data for this specific configuration is limited; therefore, cyclic load values should be generated on printed samples under the actual build orientation and not extrapolated from injection-molded TPE databases.

    Particle morphology in the as-supplied powder affects both recoating and part density. The composite filler is dispersed in the elastomer matrix at the particle level, and the powder is screened to remove agglomerates above 150 µm before packaging. Laser melting causes a rapid reduction in porosity, but localized gas evolution from moisture or volatiles can create sub-surface voids if the powder is not pre-dried. Optical microscopy of fracture surfaces from process validation builds shows partially melted filler domains near the interlayer boundary; these domains increase the apparent surface energy of the melt pool and contribute to the 20–30% Z-axis modulus reduction observed in tensile specimens.

    Safety and regulatory documentation for the powder addresses REACH registration, RoHS Directive 2011/65/EU heavy-metal restrictions, and occupational handling of respirable dust. The as-supplied powder is not classified as hazardous under the OSHA Hazard Communication Standard in its solid form, but bead blasting and sanding generate fine dust that requires engineering controls and local exhaust ventilation. Food-contact status under FDA 21 CFR is not generally claimed for unfilled SLS parts made from this elastomer composite unless a user-validated sealant or coating is applied. The user is responsible for verifying that the final part meets application-specific extractables and migration limits.

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