| HS Code | 422037 |
| Material Type | Acrylonitrile Butadiene Styrene (ABS) thermoplastic |
| Tensile Strength | 37 MPa |
| Tensile Modulus | 2300 MPa |
| Elongation At Break | 6% |
| Flexural Strength | 61 MPa |
| Flexural Modulus | 2100 MPa |
| Izod Impact Strength Notched | 100 J/m |
| Heat Deflection Temperature At 0 45 Mpa | 88 °C |
| Heat Deflection Temperature At 1 82 Mpa | 82 °C |
| Glass Transition Temperature | 104 °C |
| Density | 1.08 g/cm³ |
| Rockwell Hardness | R108 |
| Dielectric Strength | 15 kV/mm |
| Volume Resistivity | 1.0E+15 ohm-cm |
| Coefficient Of Thermal Expansion | 8.5E-5 mm/mm/°C |
| Thermal Conductivity | 0.17 W/m·K |
| Water Absorption | 0.2% |
| Flame Rating | UL 94 HB |
| Chemical Resistance | Good against acids, alkalis, oils, and greases |
| Uv Resistance | Poor |
As an accredited Proto3000 ABSi Fused Deposition Modeling Polymer factory, we enforce strict quality protocols—every batch undergoes rigorous testing to ensure consistent efficacy and safety standards.
| Packing | One 1 kg spool of Proto3000 ABSi Fused Deposition Modeling Polymer, sealed in moisture-barrier foil bag with desiccant and label. |
| Container Loading (20′ FCL) | Container Loading (20′ FCL): Proto3000 ABSi FDM polymer supplied in palletized spools/cartons, stretch-wrapped, braced, moisture-protected, labeled, and shipped per transport regulations. |
| Shipping | Proto3000 ABSi Fused Deposition Modeling Polymer is a nonhazardous solid. Ship in original sealed packaging at ambient temperature. Protect from moisture, heat, and UV. Not regulated by DOT, IATA, IMDG, or ADR; no UN number, hazard class, or packing group. Ensure packaging remains closed and secure during transport. |
| Storage | Store Proto3000 ABSi Fused Deposition Modeling Polymer in a cool, dry, well-ventilated area away from direct sunlight, heat, sparks, and incompatible chemicals. Keep filament sealed in its original packaging or an airtight container with desiccant to prevent moisture absorption. Maintain moderate room temperature, avoid excessive humidity, and rotate stock. Do not store near oxidizers or ignition sources. |
| Shelf Life | Shelf life is 2 years when stored sealed in a cool, dry, well-ventilated area, away from direct sunlight and moisture. |
At a chamber temperature of 68 °C ± 2 °C and a build-sheet setpoint of 105 °C, automotive cabin air-management prototypes are produced from 1.75 mm Proto3000 ABSi filament pre-dried in a forced-air desiccant dryer at 80 °C for 4 h to a moisture content below 0.20 wt%. The feedstock addition ratio is fixed at 100% virgin ABSi; where an internal closed-loop recycling stream is used, regrind from failed prototype duct runs is capped at 10 wt% because diameter variation above ±0.05 mm produces inconsistent drive-wheel engagement and increases the probability of retraction-induced filament buckling in the extrusion head. Flammability documentation references FMVSS 302 and ISO 3795:1989, while thermal dimensional stability is evaluated under ISO 75-2:2013 Method B at 0.45 MPa using edgewise specimens machined to 80 mm × 10 mm × 4 mm. The downstream process uses a 0.4 mm brass nozzle at 250 °C, 0.20 mm layer thickness, 45% rectilinear infill, and three perimeter contours. Large duct sections are printed in 200 mm segments because flat span curl above 0.8 mm beyond 300 mm length is otherwise detected during unclamped cooling. Complex S-shaped duct cores are chilled to 5 °C before mechanical support break-off to avoid seam fracture. Terminal part types include dashboard defrost plenum mockups, B-pillar air outlet housings, rear cabin USB ventilation grille bezels, and under-seat battery-cooling duct prototypes subjected to 8 h airflow tests at 23 °C and 50% RH.
For medical device enclosure prototypes, Proto3000 ABSi is processed at 100% virgin feedstock addition with 0 wt% recycled content because ISO 13485:2016 clause 7.3 design and development records require material lot traceability for each physical configuration subjected to design verification. The only additive permitted at the filament conversion stage is a 1.0 wt% high-purity heat-stabiliser masterbatch; no carrier resin is added at the FDM nozzle, and the deposited part therefore remains 100% ABSi. Biocompatibility evaluation for limited-contact housing prototypes follows ISO 10993-5:2009 with 24 h extract preparation in supplemented cell culture medium, while prototypes entering an electromedical assembly are assessed against IEC 60601-1:2005 + A1:2012 + A2:2020 for marking legibility and mechanical housing integrity. Incoming resin lots are screened by melt volume-flow rate under ISO 1133-1:2022 at 230 °C/3.8 kg; if lot-to-lot variation exceeds ±10%, the extrusion multiplier is re-calibrated on a 50 mm × 50 mm wall coupon before release. The downstream build uses a 0.4 mm hardened steel nozzle at 255 °C, a build sheet at 110 °C, a chamber at 70 °C, 0.10 mm layer height for snap-fit engagement surfaces, and 60% triangular infill with four outer shells. Support material in blind snap grooves is removed with a 3.0 mm flat-ground chisel after 24 h cooling at 21 °C. Terminal products include handheld surgical stapler housing mockups, diagnostic monitor bezel prototypes, ultrasonic probe handle bodies, and bed-rail control pendant covers used in 72 h hand-piece ergonomic trials.
In robotic end-of-arm tool production, Proto3000 ABSi is specified at 0 wt% filler addition and 0 wt% plasticiser addition because dimensional compensation is controlled by process scaling rather than formulation adjustment. The feedstock remains 100% ABSi; when higher stiffness is required for a fixture body, the modification is made by increasing infill to 85% or 100% solid rather than by glass-fibre masterbatch dilution, for which published data for this specific configuration is limited. Dimensional control references ISO 294-3:2020 for shrinkage evaluation and ISO 1101:2017 for geometrical product specifications. Printed CMM fixtures are measured on a bridge CMM with a scanning probe repeatability of ±0.002 mm, and serial numbers are laser-engraved only after measurement. The deposition process uses a 0.8 mm nozzle, 260 °C setpoint, 110 °C build sheet, 75 °C chamber, 0.30 mm layer height, and 75% hexagonal infill. Printed dowel holes are reamed from 6.0 mm to 6.0 H7 with a carbide reamer at 800 rpm to avoid melting-induced hole taper. Post-print annealing is performed at 85 °C for 2 h, after which Shore D hardness is 78. Terminal part types include robot gripper fingers for 20 kg payload handling, drill guide blocks for carbon-fibre panel drilling, car-aid fixture nesting blocks, and CMM holding fixtures for cast aluminium housings.
| Downstream scenario | Primary compliance standard | Feedstock addition ratio | Critical process boundary | Terminal product type |
|---|---|---|---|---|
| Automotive HVAC duct prototypes | FMVSS 302; ISO 3795:1989; ISO 75-2:2013 Method B | 100% virgin ABSi; ≤10 wt% regrind | 68 °C ± 2 °C chamber; 0.20 mm layer | Dashboard plenums, B-pillar outlets, USB grille bezels |
| Medical device enclosure prototypes | ISO 10993-5:2009; ISO 13485:2016; IEC 60601-1 | 100% ABSi; 0 wt% recycled; 1.0 wt% stabiliser at extrusion | 0.10 mm layer; 70 °C chamber | Surgical stapler housings, monitor bezels, probe handle bodies |
| Industrial end-of-arm tooling and fixtures | ISO 294-3:2020; ISO 1101:2017 | 100% ABSi; 0 wt% filler/plasticiser | 0.30 mm layer; 85% hexagonal infill; 85 °C anneal for 2 h | Robot gripper fingers, drill guides, CMM fixtures |
| Consumer electronics enclosure prototypes | RoHS 2011/65/EU; REACH 1907/2006; ASTM D638-14 | 100% ABSi; 0 wt% flame-retardant masterbatch | 0.15 mm layer; 65 °C chamber; 0° snap raster | Phone cases, wearable housings, laptop bezels |
| UAS airframe test articles | AS9100D; ASTM D648-18; ASTM D790-17 | 100% ABSi; 0.5 wt% UV stabiliser at extrusion only | 0.25 mm layer; 75 °C chamber; 0.5 °C/min cooling anneal | Wing root fairings, radome mockups, camera plates |
| Mechanical test coupon production | ASTM D638-14; ASTM D790-17; ISO 527-2:2012 | 100% ABSi; 0 wt% fibre or particulate filler | 0.2 mm layer; raster angle 0°/45°/90° | Tensile bars, flexure bars, DOE specimens |
When a handheld consumer electronic enclosure prototype must survive 1.0 m drops onto concrete, Proto3000 ABSi is deposited at 100% feedstock addition with 0 wt% flame-retardant masterbatch unless the prototype is required to simulate the UL 94 V-0 grade of an eventual production polycarbonate-ABS resin; in that case the ABSi part is coated externally with a 0.1 mm intumescent clear coating after machining, while published data for direct V-0 ABSi filament is limited. Substance restrictions are documented under RoHS 2011/65/EU Annex II and REACH 1907/2006 candidate list screening for each incoming filament lot. Mechanical validation follows ASTM D638-14 tensile testing of 3.2 mm machined coupons and ASTM D256-10e1 Izod impact on notched samples cut from 6.4 mm plaques. The downstream process uses a 0.4 mm nozzle at 245 °C, a 105 °C build plate, a 65 °C chamber, 0.15 mm layer height, and 38% rectilinear infill. Snap-fit features are printed at 0° raster angle relative to the clip axis, while hinge pins are printed at 90° to avoid transverse layer shear. Terminal products include phone case drop-test mockups, wearable strap housings exposed to 5% salt spray for 48 h under ISO 9227:2022, and laptop bezel snap assemblies cycled 500 times at 23 °C.
Before UAS airframe test articles are printed, the feedstock addition ratio is locked at 100% ABSi with no regrind stream because traceability requirements in AS9100D clause 8.5.2 require full raw-material lot linkage. The only formulation modification allowed is a 0.5 wt% UV stabiliser masterbatch at the filament extrusion stage for outdoor ground-test articles, but published data for this specific configuration is limited. Without post-print thermal conditioning, dimensional flatness degrades when the part is uniformly exposed to 60 °C; flatness deviation over a 300 mm span reaches 1.9 mm to 2.3 mm on unannealed test plaques. Mechanical verification references ASTM D638-14 for X-Y oriented tensile specimens, ASTM D790-17 for flexural modulus, and ASTM D648-18 for heat deflection temperature at 1.82 MPa. Printed radome mockups are inspected for voids using a 2.0 MHz ultrasonic A-scan before environmental testing. The downstream build uses a large-format FDM platform with a 914 mm × 610 mm × 914 mm build envelope, a 0.5 mm nozzle at 265 °C, a 110 °C build sheet, a 75 °C chamber, 0.25 mm layer height, and 50% hexagonal infill with six perimeter shells. Annealing is performed in a convection oven at 85 °C for 2 h followed by a forced cooling ramp of 0.5 °C/min to 35 °C. Terminal part types include UAS wing root fairing test articles, nose radome mockups for antenna tuning, camera gimbal isolation plates, and fuselage access panel prototypes used in ground vibration tests.
In university mechanical testing laboratories, test coupon production from Proto3000 ABSi uses a fixed 100% virgin addition ratio and 0 wt% fibre or particulate filler so that process parameter effects can be isolated from formulation variables. Specimen geometry follows ASTM D638-14 Type I tensile bars at 3.2 mm thickness, ASTM D790-17 flexure bars at 3.2 mm × 12.7 mm × 127 mm, and ISO 527-2:2012 Type 1BA specimens for cross-standard comparison. Calibration prints are run at 240 °C, 110 °C bed, 65 °C chamber, 0.2 mm layer height, and 45% rectilinear infill. Each DOE cell records actual extruder heater temperature via a 0.5 mm grounded-tip thermocouple inserted into the nozzle block. The downstream process intentionally varies raster angle across 0°, 45°, and 90° to quantify anisotropic tensile strength; Z-axis layering is assessed on 50 mm × 50 mm × 12.7 mm blocks milled flat to 6.0 mm before Izod notching per ASTM D256-10e1. Conditioning before destructive testing follows ASTM D618-21 at 23 °C and 50% RH for 48 h. Terminal outputs include large-format instructional demonstration parts, interlaboratory round-robin tensile coupons, and parameter study specimens for polymer-print benchmarking.
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Proto3000 ABSi is an unfilled, impact-modified acrylonitrile butadiene styrene-type fused deposition modeling polymer supplied as filament feedstock for heated-chamber additive manufacturing systems. The product sits within the ABSi platform and uses a dispersed elastomeric phase to increase notched impact absorption at the expense of tensile and flexural modulus. Representative dry-condition mechanical values from coupons printed in the horizontal XY plane include tensile yield strength of 32 MPa tested to ASTM D638-14, tensile modulus of 1,920 MPa, flexural strength of 48 MPa tested to ASTM D790-17, and notched Izod impact of 347 J/m tested to ASTM D256-10. Specific gravity is reported near 1.04 g/cm³ under ASTM D792-20. Heat deflection temperature at 0.455 MPa is 86 °C under ASTM D648-16 for as-printed test specimens. These values are orientation-dependent; Fused Deposition Modeling generates an orthotropic body with lower through-thickness properties than in-plane properties, so load-bearing applications require printed verification coupons in the production toolpath orientation.
Proto3000 ABSi is commonly specified for functional prototype iterations, assembly fixtures, housing components, and short-run production parts that do not require sterilizability or sustained service above the published heat distortion limit. Soluble support compatibility is printer-specific and should be evaluated for adhesion at the ABSi-to-support interface, especially when stacked features reduce access for support removal. Batch-to-batch consistency in pigment-free material is generally controlled by the supplier, but colorant masterbatch or recycled content can shift melt rheology and impact resistance; lot-specific certificates remain the only valid source for formulation-sensitive claims.
The observed difference between ABSi and ABS-M30 is not a simple molecular-weight shift. Impact modification disperses a low-modulus rubbery domain within the glassy styrene-acrylonitrile matrix. Under tensile load, the dispersed phase reduces apparent stiffness because the soft domains lower the effective cross-sectional modulus. Under impact, the same domains initiate multiple crazes and shear bands ahead of the notch tip, increasing energy absorption to 347 J/m in notched Izod versus 139 J/m for ABS-M30. The same morphology lowers heat deflection temperature to 86 °C at 0.455 MPa compared with 96 °C for ABS-M30 because the elastomer phase softens at elevated temperature.
In Fused Deposition Modeling, the weld interface between layers remains the limiting structural feature. Morphology-driven improvements in bulk impact resistance are observed in XY coupons, but through-thickness impact and tensile strength are governed by neck formation at the interlayer boundary. A lower chamber temperature suppresses polymer diffusion across the weld line, and the resulting boundary can act as a notch-like discontinuity. Therefore ABSi should not be specified for high-load Z-direction impact without testing coupons printed at the production layer height and raster configuration. The impact-modifier dispersion also influences melt rheology: the higher elastomer content in ABSi can increase viscosity at a given nozzle shear rate, requiring slightly lower extrusion speed or higher nozzle pressure to maintain consistent road width. On systems with fixed volumetric flow control, operators may observe greater nozzle ooze during non-extrusion moves unless retraction and wipe settings are adjusted. These are processing consequences of the same phase morphology that creates the mechanical property difference.
| Property | ABSi | ABS-M30 | Test Method |
|---|---|---|---|
| Tensile yield strength | 32 MPa | 36 MPa | ASTM D638-14 |
| Tensile modulus | 1,920 MPa | 2,413 MPa | ASTM D638-14 |
| Flexural strength | 48 MPa | 61 MPa | ASTM D790-17 |
| Flexural modulus | 1,720 MPa | 2,650 MPa | ASTM D790-17 |
| Notched Izod impact | 347 J/m | 139 J/m | ASTM D256-10 |
| Heat deflection temperature at 0.455 MPa | 86 °C | 96 °C | ASTM D648-16 |
On production-scale FDM equipment with all-metal hot ends and a heated build enclosure, the extrusion barrel for ABSi is normally maintained between 230 °C and 250 °C and the chamber between 70 °C and 90 °C. A moisture mass fraction above approximately 0.2 wt% can create extrudate surface defects, die swell, popping, and reduced interlayer fusion because steam bubbles disrupt the melt path. Spools stored outside sealed desiccant at relative humidity above 60% RH require drying at 80 °C for 4 h to 8 h depending on spool mass and initial moisture load. The melt processing window is narrower than that of unmodified ABS: residence time above 260 °C or high local shear heating in the nozzle can degrade the impact-modifier phase and cause yellowing or brown streaking. Open-architecture printers without a heated chamber cannot reliably reproduce the ABSi property envelope because rapid free-convection cooling reduces interlayer weld strength.
Layering and raster angle convert the bulk polymer data into part-scale orthotropy. Unidirectional 0° raster with a 0.254 mm layer height typically maximizes tensile stiffness along the print axis but produces weak transverse resistance between adjacent roads. A +45°/−45° raster improves shear resistance and gives more uniform in-plane properties at a small loss in axial tensile modulus. Positive air gap settings above the supplier default reduce material overlap and introduce controlled porosity that lowers density below solid ABSi; this practice should only be used when the application tolerates reduced sealing and mechanical strength. Edge contour paths with insufficient overlap to the raster can create notch-like separation at the part perimeter and should be verified by cross-sectional inspection.
Several parameters interact to define the practical processing window for Proto3000 ABSi. If the chamber heater setpoint cannot maintain at least 75 °C at the height where the part is being built, the part will develop thermal gradients across tall geometries; the upper layers may contract at a different rate than the lower layers, producing interlaminar shear stress and delamination at the Z seam. In such cases, build volume temperature mapping is as important as nozzle temperature. The recommended nozzle temperature is typically selected within ±5 °C of the mid-range for the particular hot-end geometry; deviation beyond this band can trigger stringing, channel plugging, or reduced interlayer toughness without obvious changes in surface appearance.
Enclosure humidity should remain below 30% RH during operation when spool covers are removed. Humidified or moisture-contaminated filament often presents delayed failures rather than immediate process interruption: a part may show acceptable top surface finish but reduced local tensile strength at the weld lines. For critical parts, a hot-wire or thermogravimetric moisture check is preferred over relying solely on process appearance. Published data for the specific change in interlayer tensile strength as a function of filament moisture for Proto3000 ABSi is limited; general ABS-class FDM data indicate that moisture above 0.2 wt% can reduce weld strength substantially, mandating controlled re-drying rather than simple surface purging.
In service, Proto3000 ABSi is used for assembly tools, housing components, snap-fit brackets, and low-pressure functional prototypes where impact resistance during insertion or drop loading is the controlling failure mode. It is not specified for continuous load-bearing structures, high-cycle fatigue, or sustained exposure above 80 °C because published creep and fatigue data are limited and the heat deflection temperature under ASTM D648-16 does not provide long-term design allowables. Chemical compatibility follows the ABS-class profile: short-term contact under 24 h with dilute aqueous acids, many detergents, and some alcohols causes minor surface wetting, while ketones, esters, aromatic solvents, and aggressive plasticizers can dissolve or stress-crack the polymer. Compatibility with service fluids should be examined using ASTM D543-14 on as-printed samples rather than molded plaques because interlayer boundaries increase solvent ingress.
Surface post-processing with solvent-based smoothing can reduce surface roughness but may preferentially attack the impact-modifier phase, causing a loss in notched impact resistance. Machining operations such as drilling, reaming, and tapping should follow low-speed, low-feed parameters to avoid frictional heating above the heat distortion threshold. Heat-stake or threaded inserts provide better joint retention than self-tapping screws because the screw thread can split the interlayer boundary when loading is perpendicular to the build plane. Dimensional tolerances on FDM parts remain machine-specific; designers should not transfer injection-molding tolerances to Proto3000 ABSi without verifying multiple build iterations.
Replacement of machined ABS or polyurethane-cast ABS parts with Proto3000 ABSi shifts the design problem from solid isotropic material to layered orthotropic material. Machined ABS has isotropic tensile properties and no layer boundaries, but complex internal channels and snap features often require secondary assembly. Proto3000 ABSi can consolidate these features into one build, provided the finite element analysis accounts for orthotropic stiffness and interlayer tensile strength values. Published Z-axis tensile strength data for this specific configuration is limited; general FDM ABS studies report through-thickness tensile strength from 40% to 70% of the in-plane value depending on chamber temperature, raster angle, and air gap. For a load-bearing wall, this is the controlling value, not the XY coupon tensile strength of 32 MPa.
When replacing low-pressure molded ABS parts, the ABSi FDM part will often show larger surface roughness, lower bulk density, and lower Z-axis modulus unless the toolpath is densified with extra contours or positive raster overlap. Field experience with fixture components indicates that snap arms oriented in the XY plane exhibit fracture less often than vertical arms; this is consistent with the lower through-thickness tensile values discussed above. For this reason, critical snap geometries should be oriented so that deflection occurs within the build plane. Inserts and fastening points should be printed with additional solid layers around the hole perimeter and reamed to size after build to avoid sharp weld-line notches.
Compliance documentation is lot-specific and should be audited against the intended end-user jurisdiction. Verification of tensile properties follows ASTM D638-14 or ISO 527-2:2022; flexural properties follow ASTM D790-17 or ISO 178:2019; impact resistance follows ASTM D256-10 or ISO 180:2019. Heat deflection temperature is often reported under ASTM D648-16 or ISO 75-2:2013 at 0.455 MPa. Moisture content verification can use ISO 15512:2019 or a supplier-specific desiccation method. RoHS and REACH declarations apply to the material as supplied, not to the final assembled device, and additional requirements such as UL flame ratings, FDA food-contact status, or medical device cleanability cannot be inherited automatically from the filament certificate.