| HS Code | 421255 |
| Material | ALM PA 850 Black Nylon 11 SLS Prototyping Polymer |
| Color | Black |
| Polymer Base | Nylon 11 |
| Tensile Strength | 51.7 MPa |
| Tensile Modulus | 1.64 GPa |
| Elongation At Break | 60% |
| Flexural Strength | 68.9 MPa |
| Flexural Modulus | 1.45 GPa |
| Izod Impact Notched | 53.4 J/m |
| Heat Deflection Temperature 0 45 Mpa | 155°C |
| Heat Deflection Temperature 1 82 Mpa | 75°C |
| Melting Point | 190°C |
| Density | 1.02 g/cm³ |
As an accredited ALM PA 850 Black Nylon 11 SLS Prototyping Polymer factory, we enforce strict quality protocols—every batch undergoes rigorous testing to ensure consistent efficacy and safety standards.
| Packing | Supplied as 20 kg net in a sealed foil-lined fibre drum with tamper-evident closure, ensuring moisture protection during transport. |
| Container Loading (20′ FCL) | ALM PA 850 Black Nylon 11 powder in 20′ FCL: palletized, sealed moisture-proof bags, braced to prevent shifting. |
| Shipping | ALM PA 850 Black Nylon 11 SLS Prototyping Polymer ships as a non-hazardous, dry powder in sealed moisture-barrier containers. Protect from water, humidity, and excessive heat. Standard ground or air freight is acceptable; no special hazmat endorsement required. Keep upright and dry during transit to preserve powder flowability and print performance. |
| Storage | Store ALM PA 850 Black Nylon 11 SLS Prototyping Polymer in a cool, dry, well-ventilated area in its original, tightly sealed container. Protect from moisture, humidity, and direct sunlight, as damp powder can affect print quality. Keep away from heat, sparks, open flames, and incompatible materials. Avoid prolonged skin contact and dust accumulation. |
| Shelf Life | Shelf life is typically 12 months from manufacture when stored unopened in a cool, dry place. |
ALM PA 850 Black Nylon 11 SLS Prototyping Polymer is introduced into automotive air intake and fluid routing programs where closed-section ducting must be built without tooling and tested on vehicle for thermal soak and vibration. The relevant compliance screen for such under-hood prototypes is ASTM D648-18 at a flexural load of 0.45 MPa, combined with tensile testing to ISO 527-2:2012 at 23 °C and 80 °C. In this application the material is not melt-compounded; recovered powder is blended with virgin PA 850 Black at a fresh powder addition ratio of 35–50 wt%, depending on target tensile elongation and acceptable surface porosity. The blended feedstock is sieved through a 150 µm mesh, dried to a moisture content below 0.1 wt%, and loaded into a CO₂ laser sintering system operating at 10.6 µm wavelength with layer thickness of 0.10–0.12 mm. Bed temperature is held between 168 °C and 178 °C, and parts remain in the powder cake for not less than 24 h after the build to reduce residual stress and curl before extraction. Terminal part types from this workflow include air cleaner outlet snorkels, charge air cooler end tank mock-ups, and HVAC blend door linkage prototypes. A process boundary for this scenario is that continuous under-hood exposure above 130 °C under mechanical load should be qualified for specific oil mist and seal contact conditions, because polyamide 11 oxidation kinetics accelerate in hot hydrocarbon environments and published data for this specific black PA11 configuration under such combined exposure is limited.
Cabin air distribution plenum mock-ups and wire harness routing clips built from ALM PA 850 Black are typically produced without hard tooling to verify interface geometry against metallic attachment points and to locate conflict points prior to metal bracket procurement. In non-flight engineering mock-ups, the relevant quality compliance frame is ISO 9001:2015 configuration control rather than production aeronautical certification; any substitution into flight hardware requires OEM qualification under 14 CFR 25.853(a) for vertical burn and ASTM E662 for smoke density, and the supplier has not published a production aerospace qualification for this grade at time of writing. The powder feedstock for such builds is commonly maintained at a 50 wt% virgin addition ratio to reduce lot-to-lot variation in XY and Z tensile elongation, with recovered powder screened through 125 µm mesh and homogenised in a tumble mixer for 30 min. Build preparation places long unsupported walls at 15–20° rotation relative to the recoater travel to avoid layer-shift and curl. Laser sintering is carried out under an inert nitrogen atmosphere with oxygen concentration held below 1.5 vol%, and the parts remain in the powder bed for at least 24 h before extraction. Terminal part types include cabin air plenum mock-ups, avionics cooling duct prototypes, and harness clip iterations used in seat-frame and sidewall assembly reviews. The Z-axis elongation of PA 850 Black is typically lower than the XY-axis value, so snap arms and clip features are repositioned to the XY plane where possible; published data for specific build orientation effects on this grade is limited, but the anisotropy is consistent with other black PA11 SLS powders.
When consumer wearable and handheld device teams replace CNC-machined acetal prototype housings with laser-sintered black PA11, the primary acceptance criterion is snap-fit insertion force retention after repeated cycling at 23 °C and 85 % RH. Compliance for these non-saleable prototype enclosures is normally limited to RoHS Directive 2011/65/EU recast and REACH Regulation (EC) No 1907/2006 Article 33 documentation obtained from the powder supplier; no food-contact or medical enclosure claim is applicable. The feedstock blend is prepared with a fresh powder addition ratio of 40–50 wt%, and the recovered fraction is sieved at 125 µm to remove agglomerates and debris from previous builds. For living hinge test parts, the hinge line is placed in the XY build plane because Z-oriented PA11 SLS specimens show reduced elongation and lower notched Izod impact strength under ISO 180:2019; a build bed temperature between 170 °C and 175 °C is held stable because deviations of more than ±3 °C can generate visible surface striations and non-uniform hinge thickness. After extraction, glass bead blasting with 0.2–0.4 mm media and dry-air cleaning removes residual powder from hinge recesses. Terminal components include earbud charging case clamshell prototypes, wearable camera frame sections, and handheld device enclosure snap-fit iterations. A stated operational boundary is that snap-in forces shift after moisture equilibration; parts conditioned to equilibrium at 50 % RH should be used when measuring assembly force, while parts tested dry immediately after sintering can exhibit lower failure deflection.
| Validation domain | Standard or regulation | Application context | Observed condition or criterion |
|---|---|---|---|
| Heat deflection | ASTM D648-18 | Under-hood air intake prototypes | 0.45 MPa flexural load; distortion assessed after vehicle soak |
| Tensile anisotropy | ISO 527-2:2012 | Aerospace cabin mock-ups and consumer enclosures | XY and Z coupons from same powder batch |
| Notched impact | ISO 180:2019 | Snap-fit enclosures and motorsport ducts | 23 °C dry and conditioned states |
| Chemical immersion | ISO 175:2010 / ASTM D543-20 | Fluid handling jigs | 7 d immersion at 23 °C; flexural retention per ISO 178:2019 |
| Biological evaluation | ISO 10993-1:2018 | External rehabilitation device prototypes | Short-term external contact; risk-based test selection |
| Flammability and smoke | 14 CFR 25.853(a) / ASTM E662 | Aerospace cabin mock-ups | OEM qualification required prior to flight hardware use |
Scanning-derived extremity geometry converted directly into a shell file for laser sintering places PA 850 Black in short-run external rehabilitation device prototypes without the cutting waste associated with polypropylene sheet thermoforming; however, the material is not treated as a validated skin-contacting clinical product. The relevant assessment path is ISO 10993-1:2018; chemical characterisation and cytotoxicity testing are the responsibility of the device developer, and published data for this specific black PA11 SLS grade under repeated patient contact is limited. A fresh powder addition ratio of 30–40 wt% is commonly sufficient for shape-capture prototypes where surface cosmetics are less important than overall fit, but for weight-bearing check sockets the fresh fraction is raised to 50 wt% to maintain ductility in the posterior trimline region. The production process begins with autogenerated lattice venting for large enclosed volumes, followed by laser sintering at 0.10 mm layer thickness under nitrogen, post-build cooling in the powder bed for 24 h, and then ceramic tumbling to reduce surface roughness without closing vacuum holes. Terminal product types include trans-tibial check socket prototypes, ankle-foot orthosis shell trials, and finger splint capture devices. A practice-level limitation is that PA 850 Black parts should not be exposed to autoclave steam sterilisation because shape distortion occurs near the glass transition region; low-temperature hydrogen peroxide gas plasma or cold disinfection methods are the only options for short-term external fitting trials, and must be qualified by the device developer.
In fluid handling assembly lines, black PA11 SLS fixtures are used where hydrocarbon exposure is moderate and where the softer failure mode of polyamide 11 reduces the risk of brittle clamp fracture during operator handling. Compliance for chemical immersion testing follows ISO 175:2010 or ASTM D543-20, with flexural strength retention measured after 7 d immersion at 23 °C according to ISO 178:2019. The feedstock blend for chemical-exposed fixtures uses a fresh powder addition ratio of 50 wt%, because lower fresh fractions can increase open porosity at thin wall sections and accelerate reagent uptake. Parts are built with 0.10–0.12 mm layer thickness, packed to reduce unsupported overhang, and post-processed by bead blasting and dry-air treatment; critical sealing faces are machined flat after sintering to create a chip-free mating surface. Terminal components include diesel fuel filter housing assembly nests, oil separator test fixtures, and low-pressure hydraulic hose routing jigs. A known boundary is that PA 850 Black is not selected for continuous immersion in hot aqueous acid solutions above 10 % concentration; nylon 11 exhibits acid-catalysed chain scission that reduces molecular weight and tensile strength. If the fixture contacts such media, a direct substitution of Nylon 12 or a chemical-grade semi-crystalline polymer should be evaluated with comparative ISO 527-2:2012 tensile coupons.
Wind tunnel development programs where brake cooling duct geometry changes between runs require PA 850 Black parts produced overnight to test brake cooling flow paths at cornering yaw angles and to verify clearance between rotating wheel packages and suspension links. This scenario does not use production homologation standards for road vehicles; general part geometry is documented against ISO 2768-1 medium tolerance class for non-aerodynamic interfaces, while aerodynamic surfaces are verified by structured-light scanner with volumetric accuracy of ±0.05 mm, and mechanical properties are monitored with ISO 527-2:2012 tensile bars built in the same build chamber. The fresh powder addition ratio is held at 50 wt% to keep notched impact behaviour consistent for trackside component handling, and recovered powder is screened through 125 µm mesh to remove coarse charred particles from previous high-temperature builds. The sintering process uses 0.10 mm layer thickness and a bed temperature at the lower end of the PA11 window, around 168 °C, to reduce black surface discoloration caused by prolonged exposure to the hot powder bed. Parts are cooled in situ for 18–24 h, then extracted and fitted with sacrificial drain holes opened by low-speed drilling to release trapped powder from internal duct volumes. Terminal components include brake duct inlet rings, radiator exit louvres, and cockpit air hose adapters used during track and thermal validation. A practical limitation is that thin walls below 1.2 mm in the Z direction can develop pinholing under aerodynamic load; such sections are thickened locally or reoriented to the XY plane.
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ALM PA 850 Black Nylon 11 SLS Prototyping Polymer is a black-pigmented polyamide 11 powder formulated for selective laser sintering in CO₂-laser powder-bed fusion systems. The grade is specified for 100 µm and 120 µm layer thicknesses and is processed at a powder-bed temperature of 175°C to 185°C. The powder is supplied as a free-flowing material with a particle size distribution compatible with counter-rotating roller and blade recoating systems on EOS P396, Farsoon HT403P, and 3D Systems ProX SLS 6100 equipment. The polyamide 11 backbone differentiates PA 850 Black from PA 12 powders by lower water uptake, higher elongation at break, and improved resistance to flexural fatigue in thin-wall sections. The black pigment is dispersed within the polymer matrix rather than applied as a surface coating, reducing the need for post-process dyeing and eliminating surface color variation caused by secondary finishing. Published data for long-term UV weathering of this specific grade is limited, and outdoor deployment requires end-user validation under ISO 4892-2 or equivalent.
In industrial practice, PA 850 Black is selected for snap-fit enclosures, flexible air-handling ducts, living hinges, clip-in wiring harness retainers, and prototype prosthetic sockets. The material is specified when design requirements prioritize elongation at break and repeated flexural cycling rather than maximum stiffness. The black color allows light-obscuring enclosures and optical fixtures without carbon-black-filled formulations that would compromise impact performance. All application-specific load values are to be verified from machined specimens prepared according to ASTM D638 Type IV or ISO 527-2:2012. Published data for this specific configuration under combined thermal cycling and mechanical load is limited.
The mechanical response of PA 850 Black is most often compared against unfilled PA 12 and glass-filled PA 12 powders. Unfilled PA 12 grades commonly display tensile elongation values in the range of 15% to 25% when tested under ASTM D638 Type IV conditions, whereas PA 850 Black is typically reported at 45% elongation at break. The higher elongation is accompanied by a lower flexural modulus, typically near 1,300 MPa, compared with glass-filled PA 12 systems that may exceed 2,500 MPa. This combination shifts PA 850 Black toward snap-fit closures, integral hinges, and air-duct bellows where cyclic deformation must occur without brittle fracture. The black pigmentation does not significantly alter the electrical insulation properties; surface resistivity remains in the 10^13 ohm range under IEC 62631-3-2 conditions.
| Property | Test method | PA 850 Black | Unfilled PA 12 SLS | Glass-filled PA 12 SLS |
|---|---|---|---|---|
| Tensile strength at break | ASTM D638 Type IV | 48 MPa | 45 MPa | 50 MPa |
| Elongation at break | ASTM D638 Type IV | 45% | 18% | 8% |
| Flexural modulus | ASTM D790 | 1,300 MPa | 1,500 MPa | 2,800 MPa |
| Notched Izod impact | ASTM D256 Method A | 50 J/m | 35 J/m | 30 J/m |
| Heat deflection temperature at 0.45 MPa | ASTM D648 | 175°C | 170°C | 180°C |
At the powder-bed level, the build chamber must be held within a narrow thermal band because nylon 11 crystallization kinetics are slower than those of PA 12 and the supercooling window between melting and crystallization is wider. On an EOS P396 operating with a 340 mm × 340 mm × 600 mm build volume, edge-to-center bed temperature variation of ±2°C has been observed during long-duration builds; the resulting cold-edge conditions produce upward curl at part corners and occasional recoater impact. Operators compensate by raising the chamber setpoint from 178°C to 182°C and reducing recoater speed from 250 mm/s to 180 mm/s. These values are process-class adjustments, not material absolute limits, and require machine-specific infrared pyrometer calibration before implementation. The black pigment increases laser absorption at the powder surface, which may allow a 5% to 10% reduction in applied laser energy compared with natural nylon 11; this adjustment is confirmed by density measurements according to ISO 1183-1.
Chemical resistance of polyamide 11 is broadly similar to PA 12 for aliphatic hydrocarbons, dilute alkali, and many automotive fluids. However, PA 850 Black is not specified for continuous immersion in concentrated mineral acids, strong oxidizing agents, phenolic solutions, or zinc chloride solutions above 50°C. Chemical compatibility for a new application should be tested according to ISO 175 with service-equivalent fluids, temperature, and stress state. For humid environments, nylon 11 absorbs less water than PA 6 and typically exhibits lower equilibrium moisture uptake than PA 12 at 50% RH and 23°C, but dimensional stability claims require conditioning per ISO 291 and measurement of mass and linear dimensional change before final tolerance allocation.
Selective laser sintering produces anisotropic mechanical properties because interlayer coalescence is not equivalent to intralayer molecular diffusion. In PA 850 Black, the XY-axis elongation at break under ASTM D638 Type IV is generally reported near 45%, while the Z-axis elongation may be 30% to 50% lower depending on scan spacing, beam offset, and cooling rate. Flexural modulus shows less orientation sensitivity, but notched Izod impact on Z-normal specimens can fall below 30 J/m when layer thickness is increased from 100 µm to 120 µm. Components such as snap-fit closures, living hinges, and air-duct bellows should be oriented so that cyclic bending occurs in the XY plane. If application loads must cross the build axis, testing under ISO 527-1/2 should be performed on specimens machined from the actual build orientation. Published data for this specific configuration is limited, particularly for fatigue loading below 10^5 cycles.
Contour scan strategy also influences Z-bond strength. Slowing the contour scan by 20% relative to the fill scan can improve edge definition but may increase local thermal input at thin-wall transitions. On PA 850 Black, excessive contour overlap in walls below 1.0 mm thickness has been associated with local over-melting, edge bead formation, and dimensional error exceeding 0.4 mm over a 50 mm span. Process engineers typically set beam offset between 0.10 mm and 0.15 mm and validate with a test coupon containing wall thicknesses of 0.8 mm, 1.0 mm, and 1.5 mm under ISO 527-2 tensile loading. The absence of glass filler reduces abrasive wear on recoater blades compared with glass-filled PA 12, but the black pigment can require more frequent window cleaning because of increased radiative absorption and vapor deposition on the laser window.
Moisture control is critical for nylon 11 powder before and during processing. Nylon 11 absorbs less water at equilibrium than PA 6, but the powder surface area accelerates moisture uptake under relative humidity above 40% RH. Process guides for polyamide 11 SLS materials specify powder moisture content below 0.10% by mass, determined by ISO 15512 Method B, before first use. Powder stored in open hoppers at 50% RH can exceed this limit within 24 hours, producing steam-induced porosity and low surface gloss. A pre-drying step at 80°C for 4 hours in a circulating-air oven is typically used for reclaimed powder that has been exposed to ambient conditions; desiccant dryers are preferred because oxidative degradation is slower at low dew point. Build rooms should be maintained at 20°C to 25°C and 30% to 40% RH, with laminar airflow across the powder handling area.
PA 850 Black powder experiences thermal oxidative degradation when repeatedly exposed to build chamber temperatures above 170°C. Chain scission and crosslinking shift the melt flow index and increase the population of fused agglomerates larger than 250 µm. On production lines, reclaimed powder is sieved through a 150 µm screen and blended with virgin material at a refresh rate of 30% to 50%, depending on part packing density and cumulative bed residence time. A refresh rate below 30% raises melt viscosity and reduces elongation at break; a rate above 50% increases dimensional variability because of differing powder particle morphology. Machine operators monitor melt flow index according to ISO 1133-1 and reject recovered powder when the MFR shifts by more than 20% from its original value. Long-run builds on Farsoon HT403P systems have shown thermal drift of ±3°C over 24 hours when the chamber heater duty cycle exceeds 70%; this is corrected with infrared pyrometer feedback and chamber-side insulation. The material should not be blended with polyamide 6 or polyamide 66 SLS powders due to incompatible melting points and crystallization rates; contamination with those powders produces delamination at layer interfaces.
When reclaimed powder is blended, the mix must be homogenized in a mechanical tumbler or ribbon blender for a minimum of 20 minutes before loading into the feed hopper. Inadequate mixing produces spatial variation in part density and mechanical response across the build platform. On EOS P396 equipment, operators track the age of recovered powder by recording cumulative build time, sieving throughput, and melt flow index drift. If the recovered powder contains more than 5% by mass of agglomerates retained on a 250 µm sieve after gentle mechanical disaggregation, the batch is rejected for production parts. These controls are applied because nylon 11 is more susceptible to oxidation-induced embrittlement than many PA 12 grades when processed at equivalent bed temperatures for extended residence times.
Published data for PA 850 Black under continuous service above 120°C is limited. Short-term heat deflection data under ASTM D648 do not predict long-term oxidative stability. For applications involving hot air flow or under-hood exposure, validation should include oven aging at the expected service temperature for 500 hours and 1,000 hours followed by tensile testing under ASTM D638 Type IV. Failure is typically indicated by a loss of elongation at break greater than 50% relative to the unaged baseline. The material is not supplied as a food-contact grade; regulatory compliance under FDA 21 CFR 177.1500 or EU 10/2011 is the responsibility of the end-user and requires migration testing on the finished sintered article.