| HS Code | 933034 |
| Material | Nylon 11 (PA11) |
| Tensile Strength | 50 MPa |
| Tensile Modulus | 1.7 GPa |
| Elongation At Break | 45% |
| Flexural Strength | 48 MPa |
| Flexural Modulus | 1.5 GPa |
| Izod Notched Impact | 53 J/m |
| Heat Deflection Temperature 0 45 Mpa | 47°C |
| Melting Point | 201°C |
| Density | 1.02 g/cm³ |
| Water Absorption 24h | 0.4% |
As an accredited 3D Systems DuraForm ProX EX NAT Nylon 11 based plastic factory, we enforce strict quality protocols—every batch undergoes rigorous testing to ensure consistent efficacy and safety standards.
| Packing | Sealed moisture-proof bag inside sturdy cardboard box, containing 10 kg of DuraForm ProX EX NAT Nylon 11 based plastic powder. |
| Container Loading (20′ FCL) | 20’ FCL loaded with palletized DuraForm ProX EX NAT Nylon 11 powder, secured for transport, non-hazardous, stable container loading. |
| Shipping | Ship as dry, sealed, non-hazardous powder in approved containers. Protect from moisture, humidity, and direct sunlight. Avoid extreme heat and open flames. Use sturdy packaging to prevent spills or dust dispersion. Label as nylon-based plastic powder and follow standard freight or courier regulations for non-hazardous materials. |
| Storage | Store DuraForm ProX EX NAT Nylon 11 in its original, tightly sealed container in a cool, dry, well-ventilated area away from direct sunlight, heat sources, and open flames. Keep away from oxidizing agents. Ensure the container is resealed immediately after use to prevent moisture absorption, which can affect print performance. |
| Shelf Life | Shelf life is 2 years when stored in original sealed packaging, in a cool, dry place, away from direct sunlight and moisture. |
Unmanned aerial system intake duct sections and avionics mounting brackets are produced from DuraForm ProX EX NAT on selective laser sintering hardware equipped with 100 W CO₂ lasers and 0.100 mm layer thickness. The nylon 11 powder is conditioned at 80 °C for 12 h to reduce moisture below 0.15% before loading, because residual moisture creates interlayer porosity and surface pitting when beam energy exceeds 60 W. Manufacturer datasheets list tensile strength near 48 MPa under ASTM D638-14 and tensile elongation at break in the range of 45–50%. Notched Izod impact values for unfilled PA11 SLS commonly fall between 60 J/m and 90 J/m under ASTM D256-10, supporting snap-fit bracket retention under UAV vibration spectra of 10–500 Hz. In build orientation comparisons, Z-direction elongation is typically 20–35% lower than XY-direction elongation, so duct sections with wall thickness below 1.2 mm are nested with the primary airflow axis parallel to the build plane. Unconsolidated powder from overflow bins is blended with virgin PA11 at ratios from 30:70 to 50:50 by mass; higher recycled content shifts zero-shear viscosity and produces edge delamination in sections thinner than 0.8 mm. Dimensional checks after 48 h at 23 °C and 50% RH show water uptake of 0.25–0.30% per ISO 62:2008, which preserves hole-to-hole positional tolerance of ±0.15 mm in production runs. Continuous exposure to aircraft de-icing fluid or strong acids is an operational boundary because both plasticize the surface and reduce fastener retention.
In custom foot orthoses and dynamic AFO shells, the controlling process variable is powder moisture at layering rather than the polymer’s equilibrium water uptake. Shells are printed with wall thickness from 2.0 mm to 3.5 mm, using scanned patient geometry with calcaneal and metatarsal pads added as seamless surface offsets. Flexural modulus measured under ASTM D790-17 is approximately 1400–1500 MPa, allowing the shell to resist fatigue cracking at AFO hinge radii above 6 mm. Perforation patterns for ventilation are placed no closer than 4 mm from the trim line because interlayer cleavage initiation concentrates where notch radius falls below 0.5 mm. Unsealed SLS nylon 11 parts are porous, so skin-contact devices are coated with a medical-grade polyurethane sealant and then evaluated under ISO 10993-5:2009 and ISO 10993-10:2013; uncoated shells are restricted to short-term external contact only. The material cannot be autoclaved above 121 °C without dimensional distortion, and repeated steam sterilization at 121 °C for 30 min cycles should not be specified because critical arch height may shift by 0.5–1.0%. Aging under 50 °C and 90% RH for 168 h increases mass by less than 0.4%, which preserves orthotic fit far better than PA6-based SLS alternatives. Patient-specific cyclic validation on a servo-hydraulic frame is typically run at 2 Hz with peak plantar pressure near 350 kPa for 250,000 cycles, although published fatigue data for this specific powder configuration is limited.
For low-pressure diesel return lines, connector housings and fuel vapor filter shells are printed in PA11 because aliphatic hydrocarbon exposure does not drive the same swelling gradient observed in shorter-chain nylons. Immersion in diesel fuel at 80 °C for 168 h under ISO 1817:2015 typically produces diametral swell in the range of 0.4–0.6%, which is compensated by clearance allowances of 0.2 mm on printed bore diameters. Sintered parts are porous and require vacuum impregnation or chemical vapor sealing before contact with fuel; otherwise, leak paths form at interlayer boundaries. Continuous-use temperature is held below the heat deflection temperature measured at 0.45 MPa under ASTM D648-18, and service above 90 °C in underhood environments has produced creep relaxation and should be avoided. Ethanol-blended fuels and biodiesel blends above the fuel grade used in validation are not automatically compatible, because polar oxygenated species can increase PA11 solvency; published data for this specific feedstock in high-ester biodiesel is limited. The pressure rating is limited to low-pressure return and vapor lines, not pressurized hydraulic or brake circuits, because anisotropic tensile strength and layer-boundary porosity reduce burst margin compared with extruded PA11 tubing.
Snap-fit housings for wearable electronics and handheld enclosures are produced from DuraForm ProX EX NAT when the design requires impact ductility above the capability of glass-filled SLS grades. Latch arms are designed with undercut depths of 0.3–0.7 mm and beam length-to-thickness ratios above 5:1, with the beam neutral axis printed parallel to the build plane to avoid interlayer failure in Z-oriented tensile stress. Tensile strain at break under ASTM D638-14 exceeds 40% for XY-printed specimens, but creep tests under ASTM D2990-17 show that retention force relaxes after 500 h at 50 °C; preload is therefore set 15–20% above nominal to maintain electrical contact pressure. Mating surfaces are printed with 0.15 mm offsets to account for powder granule surface roughness after glass bead blasting with 60–80 mesh media. Under repeated assembly of 50 cycles, latch arms show no visible stress whitening if the hinge fillet radius is above 1.0 mm; below this radius, stress concentration at the notch root initiates microcracks in the interlayer region. The material is not specified for live hinges because cyclic bending at strain amplitudes above 5% accelerates creep; separate PA11 snap features are bonded or fastened into rigid enclosures instead.
Guide pads and yarn tensioner bodies in high-cycle textile machinery are sintered from PA11 where cyclic impact from rapier and projectile motions dominates steady sliding wear. Under unlubricated sliding, the pressure-velocity ceiling of this unfilled SLS formulation is lower than PTFE-filled grades; published PV data for this specific unfilled grade is limited. The application is therefore restricted to pads that experience intermittent contact with low sliding velocity and high impact frequency. Notched Izod impact under ASTM D256-10 and dry tensile elongation above 45% provide ductile response under repeated impact, while the PA11 backbone limits moisture-induced dimensional growth to 0.25–0.30% in humid weaving sheds per ISO 62:2008. Pad thickness is maintained above 3 mm to prevent interlayer delamination from point-load contact with steel yarn guides, and mounting holes are reinforced with 6 mm boss diameters to distribute bolt preload. Wear debris generated during break-in is removed by air purge; abrasive nylon fines can accumulate on adjacent machine surfaces and must not enter bearing raceways. For continuous sliding contact at speeds above 0.5 m/s or pressures above 0.3 MPa, a filled lubricated grade should be substituted because unfilled PA11 wear rate becomes unacceptable under sustained PV load.
Industrial helmet comfort liners and face-shield bracket bases are printed as lattice structures with strut thickness from 0.8 mm to 1.5 mm. Impact screening is performed with notched Izod under ASTM D256-10 and instrumented puncture under ASTM D3763-18; however, device-level certification to EN 1078, ANSI Z87.1, or equivalent standards remains the responsibility of the helmet manufacturer and is not inherent to the powder. Lattice nodes are filleted to 0.6 mm radius to prevent brittle node failure when the liner is compressed at 20 m/s impact velocity in laboratory drop tests. Post-build glass bead blasting removes unsintered powder from open-cell lattice voids; closed-cell regions must include drainage apertures of at least 2.0 mm to permit powder removal and reduce trapped mass. Environmental conditioning at 40 °C and 90% RH for 168 h produces a mass increase of less than 0.4%, preserving liner dimensions. The operational boundary is solvent exposure from adhesive primers used in shell lamination; ketone-based primers should be replaced with aqueous primers because acetone and methyl ethyl ketone attack the surface and reduce interlayer bond strength.
| Standard designation | Measured property | Application screen |
|---|---|---|
| ASTM D638-14 | Tensile strength and elongation at break | Snap-fit and ducting |
| ASTM D790-17 | Flexural modulus | Orthotic shell bending stiffness |
| ASTM D256-10 | Notched Izod impact | Bracket and crash drop resistance |
| ASTM D648-18 | Heat deflection temperature | Diesel connector service limit |
| ASTM D2990-17 | Tensile creep and stress relaxation | Snap-fit retention force |
| ASTM D3763-18 | Instrumented puncture | Helmet liner impact screen |
| ISO 62:2008 | Water absorption | Humidity dimensional stability |
| ISO 1817:2015 | Liquid resistance | Diesel and biodiesel swell |
| ISO 10993-5:2009 | In vitro cytotoxicity | Skin-contact orthoses |
| ISO 10993-10:2013 | Skin sensitization | External patient-contact devices |
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3D Systems DuraForm ProX EX NAT is a polyamide 11 (PA11) powder supplied for selective laser sintering on production-scale powder bed fusion systems, most commonly the ProX SLS 500. The product designation NAT identifies the natural unpigmented feedstock. Manufacturer-published typical values for sintered parts include a density of 1.03 g/cm³ under ASTM D792, ultimate tensile strength of 48 MPa under ASTM D638, elongation at break of 50% under ASTM D638, tensile modulus of 1,400 MPa under ASTM D638, flexural modulus of 1,250 MPa under ASTM D790, notched Izod impact of 70 J/m under ASTM D256, and Shore D hardness of 72 under ASTM D2240. The melting point is reported as 186 °C under ASTM D3418, with heat deflection temperatures of 180 °C at 0.45 MPa and 50 °C at 1.82 MPa under ASTM D648. The product is used in functional prototypes and short-run end-use parts where the higher ductility and impact toughness of PA11 are required.
On the ProX SLS 500 platform, the build envelope is 381 mm × 330 mm × 457 mm and the material is typically processed at a layer thickness of 0.100 mm. The feedstock is a semicrystalline polyamide 11 powder; its behavior in laser sintering differs from unfilled PA12 and glass-filled nylon powders because of the PA11 melt-crystallization profile and longer aliphatic segment between amide linkages. The practical consequence is a shift in the energy density, powder bed temperature, and cool-down time required to maintain dimensional accuracy across the build.
Handling behavior is governed by particle size distribution and moisture uptake. Unconditioned PA11 powder exposed to relative humidity above 60% can absorb surface moisture, leading to powder clumping on the recoater blade and non-uniform layer density. Drying in a desiccant dryer to a moisture content below 0.1% by mass is used in SLS production for polyamide powders before introduction to the build chamber. The manufacturer’s datasheet should be consulted for lot-specific moisture limits. Melt flow rate is measured under ISO 1133-1:2022 or ASTM D1238 for incoming powder qualification, but melt flow index alone does not capture the effects of thermal history on crystallization.
Thermal stability in the build chamber is the main process control variable. The PA11 melt point of 186 °C under ASTM D3418 is higher than many PA12 feedstocks, so the powder bed is maintained within a narrow temperature band below that point. Production SLS systems typically control build-chamber air temperature to ±3 °C; deviations above the target band promote melt pool broadening and edge growth, while deviations below the target band reduce interlayer coalescence and produce brittle Z-direction tensile behavior. Recoater blade strikes caused by super-elevated part edges are a documented failure mode in SLS production when the bed temperature is too high or when insufficient cool-down time is allowed for large cross-sections. Parts with solid cross-sections greater than approximately 50 mm in the Z axis require longer cool-down cycles to avoid residual stress.
Recycled powder management is important because PA11 exposed to repeated sintering temperatures can undergo molecular weight redistribution and a shift in crystallization onset. In production, the used powder is blended with virgin powder at a refresh ratio established by the facility; common SLS polyamide practice uses 30–50% virgin powder depending on part class and mechanical requirements, but published data for DuraForm ProX EX NAT specific refresh limits is limited. Operators track apparent density, melt flow rate, and dry part density across builds. If part density falls below 1.00 g/cm³ while using the same energy density, the recycled fraction is usually increased or the powder is removed from service because of reduced particle fusion.
The nitrogen atmosphere in the ProX SLS 500 prevents oxidative degradation of the PA11 melt pool. Oxygen levels above 1% by volume during laser exposure can cause discoloration, reduced tensile strength, and powder yellowing. Facilities monitor oxygen in the chamber and maintain a positive-pressure nitrogen purge. For PA11, the required laser energy density is determined by melt pool stability and layer adhesion. Operators tune fill power, scan count, and scan spacing to achieve a part density above 1.00 g/cm³. A documented failure mode at low energy density is surface porosity and weak interlayer boundaries; at high energy density, part edges grow and cool-down warpage increases.
| Property | Test method | Published typical value |
|---|---|---|
| Density | ASTM D792 | 1.03 g/cm³ |
| Tensile strength at break | ASTM D638 | 48 MPa |
| Tensile modulus | ASTM D638 | 1,400 MPa |
| Elongation at break | ASTM D638 | 50% |
| Flexural strength | ASTM D790 | 43 MPa |
| Flexural modulus | ASTM D790 | 1,250 MPa |
| Notched Izod impact | ASTM D256 | 70 J/m |
| Shore D hardness | ASTM D2240 | 72 |
| Heat deflection temperature at 0.45 MPa | ASTM D648 | 180 °C |
| Heat deflection temperature at 1.82 MPa | ASTM D648 | 50 °C |
| Melting point | ASTM D3418 | 186 °C |
| Flammability | UL 94 | HB |
Unfilled PA12 SLS materials often list elongation at break near 15–20% and notched Izod impact below 50 J/m, while DuraForm ProX EX NAT lists 50% elongation at break and 70 J/m notched Izod impact under the same test methods. The difference arises from the PA11 crystalline structure and chain mobility, which contribute to higher elongation during tensile deformation. Relative to unfilled PA12 SLS materials, this grade provides higher ductility and impact toughness at the cost of a modest reduction in tensile stiffness. Unfilled PA12 SLS materials may have tensile modulus near 1,600 MPa, whereas the PA11 grade is listed at 1,400 MPa. For snap-fit installations, the lower modulus reduces insertion force but also reduces retention force when geometry is unchanged; design compensation through thicker sections or larger undercuts is necessary.
Glass-filled SLS nylon powders typically offer flexural modulus above 3,000 MPa and elongation at break below 5%. The PA11 material is therefore selected when a part must survive repeated deformation, impact at low temperature, or living hinge cycling. Dimensional stability under moisture is another differentiator: PA11 absorbs less moisture than PA6 or PA66, but direct comparison with PA12 requires part-specific conditioning data because both low-absorbing nylons are often within a few tenths of a percent moisture uptake after 24 h immersion.
Chemical resistance follows polyamide behavior: the material resists many aliphatic hydrocarbons, greases, and salt solutions, but hydrolytic degradation occurs in strong acids, strong bases, and prolonged hot-water exposure above approximately 70 °C. For fluid-contact applications, compatibility tests should follow ISO 175 or ASTM D543. The natural color allows post-build dyeing and painting. Dye uptake and surface sealing should follow post-processing recommendations of the SLS service provider; adhesion tests for coatings on polyamide parts are run under ASTM D3359 or ISO 2409.
Automotive air-intake ducts and climate-control components represent one application class for DuraForm ProX EX NAT. The material has been selected for thin-walled duct sections that require impact resistance after conditioning at -30 °C; low-temperature drop tests are typically performed according to ISO 6603-2 or customer-specific specifications. The published 70 J/m notched Izod value under ASTM D256 does not by itself validate a duct at subzero temperatures, so production facilities use instrumented puncture on sintered plaques to compare crack formation energy. Published data for the specific formulation under those impact conditions is limited.
Living hinges manufactured from the material benefit from the 50% elongation at break under ASTM D638. A living hinge with thickness near 0.6–0.8 mm can be flexed through a 180° closure without fracture when the hinge line is oriented perpendicular to the Z axis; Z-axis hinges often show reduced fatigue life because interlayer fusion boundaries act as crack initiation sites. Cyclic hinge testing under ASTM D7774 provides quantitative durability data. Published process-specific fatigue curves for this PA11 material are limited; each build orientation requires validation.
Snap-fit brackets and protective covers in consumer products use the material where repeated assembly and removal require high strain without stress whitening. Because the material is a polyamide, dimensional inspection should occur after conditioning at equilibrium moisture, not immediately after sintering. A common conditioning protocol is 24 h at 23 °C / 50% RH before final metrology.
For snap-fit features, the maximum surface strain in a cantilever snap arm of rectangular cross-section can be estimated as ε = (3 h δ)/(2 L²), where h is thickness, δ is deflection, and L is beam length. With a reported elongation at break of 50% under ASTM D638, design strain during installation should be kept below 10–15% to avoid stress whitening and permanent set. The low tensile modulus of 1,400 MPa reduces assembly force but also lowers retention; larger undercut depths or thicker beams are required when retention stiffness is critical.
For living hinges, the flexural modulus of 1,250 MPa under ASTM D790 permits hinge closure without excessive manual force. The hinge thickness should be limited to approximately 0.8 mm; thicker hinges raise surface bending strain beyond the material’s yield elongation. Post-build annealing at 150 °C increases crystallinity and reduces residual stress but can reduce impact toughness; published data for DuraForm ProX EX NAT under exact production annealing cycles is limited. Facilities should validate tensile and impact properties after any thermal post-treatment.
On the ProX SLS 500, a documented production bottleneck occurs when tall, thin-wall parts are packed too densely. The part mass retains heat, and the surrounding powder bed cools unevenly. This produces Z-direction warpage at the free ends of ducts and long snap arms. Operators mitigate this by orienting parts parallel to the recoater travel, adding perforated drain holes, and extending the cool-down phase inside the nitrogen-filled build chamber. The build envelope of 381 mm × 330 mm × 457 mm allows high nesting density, but thermal uniformity limits the maximum packing density for parts with solid cross-sections. Humidity exposure above 60% RH before processing and continuous service above the 50 °C HDT under load define the main operational boundaries.