| HS Code | 314794 |
| Productname | BASF 3D Ultrafuse PEI 9085 Fused Filament |
| Material | Polyetherimide (PEI) |
| Density | 1.34 g/cm³ |
| Glasstransitiontemperature | 186 °C |
| Heatdeflectiontemperature 1 82mpa | 153 °C |
| Heatdeflectiontemperature 0 45mpa | 210 °C |
| Tensilestrength | 69 MPa |
| Tensilemodulus | 2600 MPa |
| Flexuralstrength | 110 MPa |
| Flexuralmodulus | 2700 MPa |
| Elongationatbreak | 3.5% |
| Charpyimpactstrength Notched | 5.5 kJ/m² |
| Printingtemperature | 350-380 °C |
| Bedtemperature | 140-160 °C |
| Chambertemperature | 150-180 °C |
| Filamentdiameter | 1.75 mm ± 0.05 mm / 2.85 mm ± 0.10 mm |
| Netweight | 500 g |
| Color | Amber / Black |
| Flamerating | UL94 V-0 |
| Waterabsorption | 0.25% |
| Chemicalresistance | Good against fuels, oils, acids, and bases |
| Dielectricstrength | 17 kV/mm |
| Dryingtemperature | 120 °C |
| Dryingtime | 4-6 hours |
As an accredited BASF 3D Ultrafuse PEI 9085 Fused Fillament factory, we enforce strict quality protocols—every batch undergoes rigorous testing to ensure consistent efficacy and safety standards.
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BASF 3D Ultrafuse PEI 9085 Fused Fillament is an amorphous polyetherimide-based feedstock for fused filament fabrication in high-temperature material extrusion systems. The product is supplied in 1.75 mm and 2.85 mm nominal diameters on 750 g spools, with a reported solid density of 1.34 g/cm³ under ISO 1183-1. The material is not a metal-polymer system and does not require catalytic debinding or sintering; after extrusion and support removal it remains a thermoplastic polyetherimide part. This separates it from the BASF Ultrafuse 316L and 17-4 PH grades, which are green-body feedstocks for furnace sintering. The resin is also distinct from filled high-temperature filaments because it is unfilled, yet it requires an actively heated build chamber, an all-metal hot end, and a hardened steel or ruby nozzle. Published processing guidance indicates a nozzle setpoint between 350 °C and 380 °C, a build plate from 120 °C to 140 °C, and a chamber setpoint from 150 °C to 180 °C. Open-frame or passively heated machines are therefore outside the documented process envelope.
The amorphous character of the polymer means that no melt crystallization exotherm is present, but layer-to-layer adhesion and residual stress remain strongly governed by chamber temperature, extrusion temperature, and prior moisture content. On production-scale direct-drive systems with active chamber heating and a liquid-cooled cold zone, the material processes with a narrow window: below 350 °C the melt exhibits insufficient diffusion for consistent interlayer strength, while above 380 °C prolonged melt residence can produce carbonized nozzle deposits and pressure drift. Bowden arrangements are generally unsuitable because the filament is high-modulus and the spring-back on retraction increases the risk of buckling at the extruder drive. A nozzle diameter of 0.4 mm or larger is typical for extrusion stability, and extrusion multipliers are commonly held between 0.95 and 1.00 after line-thickness calibration on the specific machine.
At the molecular level, polyetherimide absorbs atmospheric moisture. The resin is reported to exhibit water absorption of 0.25% after 24 h under ASTM D570. Absorbed water at 350 °C to 380 °C flashes into steam during extrusion, generating microvoids, nozzle spitting, and intermittent extrusion-line roughness. In addition, moisture at high melt temperature may contribute to chain scission in condensation polymer systems, causing localized viscosity loss and reduced melt strength. The manufacturer therefore specifies pre-drying at 120 °C for 4 h in a forced-air drying oven. Spools left in an uncontrolled ambient environment above 60% relative humidity for extended periods require re-drying. Visual dryness is not an adequate control because bulk moisture can remain even when the surface appears dry.
Moisture-related extrusion defects are frequently misdiagnosed as incorrect nozzle temperature or insufficient purge. In practice, a frothy or speckled extrusion line during the first few metres of purging is a stronger indicator of water in the filament than of thermal degradation. Closed-loop hot-end temperature control alone cannot compensate for this condition. High-temperature material extrusion machines equipped with idle-temperature reduction and automatic purge routines are preferable, because static residence in the melt zone at 380 °C accelerates thermal degradation. The safe procedure is to dry the spool thoroughly, verify the hot-end setpoint with a calibrated pyrometer, purge after any dwell longer than 10 min, and begin printing only after a solid bead with uniform diameter is produced.
Because printed properties are toolpath-dependent, the values in Table 1 are reported from supplier-published data and resin reference data. They are not automatically valid for every part orientation, infill geometry, or machine configuration. For structural applications, part-specific testing is required.
| Property | Test method | Reported value | Condition |
|---|---|---|---|
| Density | ISO 1183-1 | 1.34 g/cm³ | Solid resin/filament |
| Tensile strength | ISO 527-2 / ASTM D638 | 68 MPa | XY printed coupon |
| Tensile modulus | ISO 527-2 | 2150 MPa | XY printed coupon |
| Elongation at break | ISO 527-2 | 5.9% | XY printed coupon |
| Heat deflection temperature | ISO 75-2/B at 0.45 MPa | 153 °C | Annealed/resin reference |
| Heat deflection temperature | ISO 75-2/A at 1.82 MPa | 143 °C | Annealed/resin reference |
| Notched Izod impact | ASTM D256 | 106 J/m | Resin reference |
| Water absorption | ASTM D570 | 0.25% | 24 h |
| Flammability | UL 94 | V-0 at 1.5 mm | Resin reference |
Material extrusion anisotropy is not captured by resin values. The Z-direction tensile strength of printed PEI 9085 is typically lower than the XY tensile strength because the layer interface is the weak plane. Published Z-direction data for this specific filament is limited, and design allowables should be established by printing test bars with the intended build orientation, layer height, infill density, and chamber setpoint. The notched Izod value is also sensitive to raster direction, shell thickness, and welding temperature. A resin-reference impact value does not substitute for a notched Izod test on a printed specimen with the actual toolpath. For aerospace interior applications, the resin flammability rating is a starting point only; component-level vertical burn testing under FAR 25.853 is required because part thickness, honeycomb or foam interfaces, and post-processing affect burn behaviour.
To differentiate PEI 9085 from ULTEM 1010, PEEK, and flame-retardant PC/ABS, the service environment must be fixed first. PEI 9085 has a lower heat deflection temperature than unfilled ULTEM 1010: 143 °C versus approximately 213 °C at 1.82 MPa under ISO 75-2/A. That difference restricts PEI 9085 when a tool or fixture must survive continuous exposure above 140 °C under flexural or tensile load. In return, PEI 9085 is typically processed at lower chamber and nozzle temperatures than ULTEM 1010 and is less notch-sensitive in many impact-loaded geometries. Compared with unfilled semicrystalline PEEK, which has a published heat deflection temperature near 152 °C at 1.82 MPa under ISO 75-2/A and continuous-use capability near 250 °C, PEI 9085 offers a lower processing temperature and eliminates the crystallization-dependent dimensional control that PEEK requires. The tradeoff is lower chemical resistance, lower maximum service temperature, and reduced resistance to hot aqueous acid or alkaline hydrolysis.
Against flame-retardant PC/ABS blends, PEI 9085 generally provides higher heat deflection and the ability to achieve UL 94 V-0 at thinner sections, but it imposes a much higher chamber temperature and nozzle setpoint. Many flame-retardant PC/ABS systems process at nozzle temperatures from 260 °C to 280 °C and can be printed on lower-temperature enclosed machines, whereas PEI 9085 requires sustained chamber operation near 160 °C to 180 °C. The difference in machine capability is a more significant barrier than the difference in raw material price. For chemically corrosive service, PEI 9085 should not be used with continuous immersion in chlorinated solvents, ketones, aromatic hydrocarbons, or high-pH alkaline solutions. Cleaning agents should be screened by immersion testing under ASTM D543, because stress cracking may appear only after the part is installed under load. Steam autoclaving above 134 °C and repeated hot-water exposure can also exceed the practical envelope for amorphous polyetherimide unless part-specific validation demonstrates acceptable retention of tensile strength and impact.
In fire-resistant housings, ducting, brackets, and functional prototypes, PEI 9085 is used where flame, smoke, and low-toxicity requirements exclude standard polycarbonate or PC/ABS grades. The material is also applied in tooling and semiconductor-adjacent fixtures where dimensional stability at elevated temperature is required but full PEEK chemical resistance is unnecessary. Unlike BASF metal-polymer filaments, PEI 9085 does not produce a metallic final part and does not require solvent debinding or sintering shrinkage compensation. Process control is therefore simpler than for catalytically debound metal systems, but polymer creep-fatigue data for printed PEI 9085 remains limited. For dynamic structural parts, test coupons should follow ASTM D638 or ISO 527-2, and long-term creep testing should be performed according to ISO 899-2 or an equivalent design-code protocol.
Post-processing by drilling, tapping, sanding, and light machining is possible with carbide or diamond tooling, but heat generation during machining can soften the surface and should be controlled by low feed pressure and sharp tools. Adhesive bonding is generally more consistent than solvent welding, and adhesive selection should include lap-shear testing under ASTM D3163 at the intended service temperature. The supplier documentation should be reviewed for REACH and RoHS declarations; a neat resin classification does not automatically certify a post-processed assembly for a specific regulatory environment. For printed aerospace parts, flame and smoke certification must be performed on the final fabricated component because part geometry, coating, and bonding layers affect the test outcome.