| HS Code | 628709 |
| Product Name | Mitsubishi PEI ULTEM™ 9085 3D Printing Filament |
| Material | Polyetherimide (PEI) blend |
| Polymer Family | Polyetherimide |
| Filament Diameter | 1.75 mm |
| Density | 1.34 g/cm³ |
| Tensile Strength | 71 MPa |
| Tensile Modulus | 2,900 MPa |
| Elongation At Break | 5.8% |
| Flexural Strength | 110 MPa |
| Flexural Modulus | 2,900 MPa |
| Glass Transition Temperature | 186 °C |
| Heat Deflection Temperature | 153 °C at 264 psi |
| Continuous Service Temperature | 160 °C |
| Flammability Rating | UL94 V-0 |
| Dielectric Strength | 630 V/mil |
| Dielectric Constant | 3.0 at 1 MHz |
| Water Absorption | 0.25% |
| Print Nozzle Temperature | 350–380 °C |
| Print Bed Temperature | 160 °C |
| Print Chamber Temperature | 190 °C |
| Print Speed | 30–50 mm/s |
| Layer Height | 0.2–0.3 mm |
| Nozzle Diameter | 0.4 mm |
| Spool Weight | 500 g |
| Color | Natural or Black |
As an accredited Mitsubishi PEI ULTEM™ 9085 3D Printing Filament factory, we enforce strict quality protocols—every batch undergoes rigorous testing to ensure consistent efficacy and safety standards.
| Packing | Vacuum-sealed foil bag with desiccant inside a cardboard box, containing one 1 kg spool of Mitsubishi PEI ULTEM™ 9085 3D printing filament. |
| Container Loading (20′ FCL) | 20′ FCL container loaded with palletized Mitsubishi PEI ULTEM™ 9085 3D Printing Filament, moisture-protected and secured for safe ocean transport. |
| Shipping | Mitsubishi PEI ULTEM™ 9085 3D Printing Filament ships as a non-hazardous solid, spooled in sealed moisture-barrier bags with desiccant and boxed. Store and transport at ambient temperature, away from moisture, heat, UV, and contamination. Handle carefully to prevent spool damage. No special DOT/IATA hazard class required under normal conditions. |
| Storage | Store Mitsubishi PEI ULTEM™ 9085 3D printing filament in a sealed, moisture-barrier bag or airtight container with fresh desiccant. Keep in a cool, dry, dark location, ideally 15–25°C and below 10–20% relative humidity. Avoid heat, sunlight, moisture, and prolonged air exposure. Use a dry cabinet if available, and re-dry before printing if moisture uptake is suspected. |
| Shelf Life | Mitsubishi PEI ULTEM™ 9085 filament has an approximately two-year shelf life when sealed with desiccant and stored cool and dry. |
Mitsubishi PEI ULTEM 9085 filament is introduced into aircraft cabin interior replacement-part production cells where the printed assembly must pass FAR 25.853(a) vertical burn and FAR 25.853(d) heat release limits. Supplier datasheets list the PEI-PC blend tensile strength at 68 MPa under ASTM D638-14 and heat deflection temperature at 153°C under ISO 75-2:2013 at 1.82 MPa. The compliance boundary for a printed air register housing or seat signage bracket is peak heat release below 65 kW/m², total heat release below 65 kW·min/m² in the first 2 min, and smoke density below 200 Ds after 4 min under ASTM E662-18. Slicing for this part class uses 100% infill, 0.20 mm layer height, 1.0 extrusion multiplier, and 7 to 9 perimeter shells; no secondary resin, regrind, or filler is introduced downstream. The built-part weight is therefore a direct function of the CAD envelope and filament density near 1.36 g/cm³. Drying is fixed at 120°C for 4 h to below 0.02% residual moisture before the sealed-filament bay is indexed to the machine. The production platform is a Fortus 900mc-class enclosed high-temperature FDM system operated at 350°C nozzle temperature, 140°C platen temperature, and 90°C chamber setpoint. After support removal, parts are annealed at 180°C for 2 h and cooled at ≤2 K/min to reduce layer-direction residual stress. Terminal finished products include cabin air register housings, lamp bracket retainers, oxygen mask panel frames, and replaceable seat signage brackets.
Process failures in this application cluster around chamber-to-ambient differentials above 60 K and moisture excursion above 0.04%. When the chamber falls below 80°C on a high-aspect-ratio bracket, each deposited road quenches before the next layer, producing interlaminate voids that operate as additional pyrolysis sites under ASTM E662 smoke testing; the same void population reduces z-axis tensile retention to 60–70% of X-Y plane strength, a value that must be confirmed by per-batch flat coupon testing rather than assumed from homogeneous resin datasheets. If moisture exceeds the 0.02% threshold during filament residence time, hydrolysis at 350°C creates visible surface blisters and lowers interlayer weld strength below the airworthiness substantiation envelope. Published data for fatigue-loaded cabin fittings at 0.25 mm layer height is limited compared with 0.18 mm coupon data, so fatigue qualification programs require baseline S-N curves generated on the same machine model, chamber geometry, and build orientation as production.
| Standard | Application scope | Printed condition to be tested |
|---|---|---|
| FAR 25.853(a) | Cabin interior vertical burn | 100% infill, as-built surface |
| FAR 25.853(d) | OSU heat release and smoke | 2.0 mm panel with production infill |
| ASTM E662-18 | Specific optical density of smoke | 2.5 mm panel, thermally conditioned |
| EN 45545-2:2020 | Rail vehicle interior fire performance | mounted final assembly |
| NFPA 130:2020 | Fixed guideway transit fire safety | installed configuration |
| UL 94 | Flammability of plastic materials | 1.5 mm bar, printed and machined |
Rail interior component design under EN 45545-2:2020 moves qualification from feedstock data to the installed assembly, because the regulation classifies the final part by its function, location, and occupied area. ULTEM 9085 filament is used for passenger rolling stock seat-back frames, armrest supports, and HVAC grilles when the part must meet Hazard Level HL2 or HL3 in the R1 category. The test chain is EN ISO 5660-1 for cone calorimeter heat-release rate, EN ISO 5659-2 for smoke density, and EN 45545-2:2020 Annex A for classification; the U.S. transit market may additionally require NFPA 130:2020 and ASTM E162-17 surface flammability. In this application class, a seat-back support printed at 2.5 mm nominal wall thickness, 85% infill, and 6 outer perimeters is submitted for HL3 evaluation; a smaller HL2 bracket may be qualified at 2.0 mm wall thickness and 62% infill. The filament is used without downstream diluents, flame-retardant coats, or post-print impregnation because any surface modification alters the fire test response. Drying at 120°C for 4 h and a sealed-filament path are mandatory; ambient shop floor exposure in humid coastal depots has led to moisture pickup above 0.04%, which is outside the processing control window.
The downstream production sequence is high-temperature FDM at 350°C nozzle, 140°C bed, and 90°C chamber, followed by CNC machining of mounting faces to ±0.2 mm and mechanical fastening into the final vehicle assembly. No solvent smoothing is permitted without repeating the full fire-test matrix, because surface finish has a measurable influence on ignition time and smoke release. Terminal finished products include armrest supports, information screen bezels, air distribution grilles, and electrical cabinet brackets in passenger rail vehicles. A field failure observed on line-side replacement stock is premature interlayer separation when the dried filament is held in non-dry-air storage and reprinted without re-drying; the corrective line practice is storage at −20°C dew point after initial drying and re-drying verification before each build batch.
Because under-hood connector shell and sensor mounting block production with ULTEM 9085 filament operates below the thermal ceiling where the polycarbonate phase loses rigidity, the process window is stable so long as continuous air temperature remains near 120°C and transient peaks stay below 150°C. The applicable compliance framework is SAE J1455 for thermal shock, chemical splash, and random vibration, with material restrictions addressed under EU RoHS 2011/65/EU plus Delegated Directive (EU) 2015/863 and REACH Regulation (EC) No 1907/2006 Annex XVII. No downstream additive masterbatch is introduced at the printing stage; the ratio is 100% ULTEM 9085 filament. Slicer settings for these components use 0.15 mm layer height, 85% infill, 4 perimeter shells, and 1.0 extrusion multiplier; flat coupons at this density record tensile strength near 60–68 MPa in the X-Y plane under ASTM D638-14. The production sequence begins with 120°C forced-air drying for 4 h to below 0.02% moisture, continues on a high-temperature FDM platform set to 350°C nozzle, 140°C bed, and 80°C chamber, and concludes with support removal followed by 160°C annealing for 2 h under unrestrained placement.
Terminal product types include transmission sensor connector shells, engine test-cell wiring clamps, and ECU mounting plates. The primary qualification risk is not heat distortion but chemical stress cracking from hot automatic transmission fluid, so batch immersion testing at 80°C in the specific fluid is required; published data for 9085 retention against aggressive modern transmission additive packages is limited and cannot be substituted by generic chemical resistance tables. Under-hood parts with long cantilever loads at or above 120°C have shown creep-induced fit loss at bolted mounting faces, which is addressed by increasing the printed shell thickness to 6 perimeters and moving the joint clamping plane into the same X-Y build plane rather than across layer interfaces.
The electrical switchgear application set for ULTEM 9085 filament depends on UL 94 V-0 flammability at 1.5 mm thickness and on interlayer fusion consistency that determines dielectric strength in a finished printed part. Printed arc barriers are produced at 100% rectilinear infill, 10 perimeter walls, 0.20 mm layer height, and 350°C nozzle temperature; the 140°C build plate and 90°C chamber maintain interlayer temperature long enough to reduce void channels that can initiate partial discharge. Because ASTM D149 dielectric strength is measured on homogeneous compression-molded coupons, the printed-part qualification must include a per-batch 100% infill flat coupon test at 1 mm thickness; supplier resin data can be used only as an upper bound. The downstream process includes CNC machining of bus bar slots to ±0.1 mm flatness, 60°C dry-air cleaning to remove cutting debris, and torque-limited assembly to avoid compression creep around inserts. Terminal finished products include arc barriers in low-voltage switchgear, terminal board insulators, and contactor base plates.
Operational boundaries for this application set are continuous surface temperature above 140°C and installation in uncontrolled high-humidity environments where conductive dust and moisture condense on microvoids at cut edges. At 140°C or above, creep deformation under screw torque is observable in flatwise compression tests; design reviews therefore derate the clamped joint allowable stress or shift the part to solid thermoset polyamide-imide alternatives only after an inability to meet the thermal requirement is confirmed. Published data for long-term comparative tracking index of 9085 filament in polluted indoor environments is limited, so electrical spacing must be verified on printed plaques under the buyer's specific contamination class rather than extrapolated from resin molding data.
Composite layup tool production with ULTEM 9085 uses sparse infill to reduce thermal mass while maintaining enough shell stiffness to resist vacuum bag compaction at −0.8 bar to −0.9 bar. Geometric compliance is set by ISO 2768-1 class m for machined edges and by the buyer's vacuum bag integrity specification; no global fire-performance standard applies to this non-passenger part class. The standard build style is 65% infill, 4–5 mm wall thickness, 5 top layers, and 0.254 mm layer height, printed at 350°C nozzle and 140°C bed with a 90°C chamber. After printing, the tool face is machined with vacuum grooves and sealed with a two-part epoxy coating to close the inherently microporous FDM surface; the acceptance criterion is vacuum decay leakage below 20 mbar over 10 min on a localized bladder test. The tool is conditioned at 120°C for 4 h before first use to stabilize creep and drive residual stress release. Terminal finished products include out-of-autoclave prepreg layup mandrels, vacuum channel drilling fixtures, and trim-route locating jigs.
The operational ceiling is 120°C continuous and 140°C short excursion; autoclave cycles above 150°C exceed the heat deflection temperature of the PEI-PC blend and produce measurable surface indentation under caul plate pressure. Another failure route specific to tooling is vacuum channel leakage after repeated thermal cycling, caused by microcrack propagation through the epoxy sealing layer into the FDM shell when the tool is heated at a rate above 2 K/min. Production controls therefore require a 20°C start temperature and a maximum heating ramp of 2 K/min to 120°C for first-cycle conditioning and post-machining inspection of groove corners at 10× magnification.
For Class I medical equipment enclosures and non-implantable anatomical models, ULTEM 9085 filament is processed only after the enclosure geometry has been evaluated against IEC 60601-1:2005 + A1:2012 + A2:2020 mechanical housing and leakage current provisions. The filament is used at 100% infill, 0.15 mm layer height, 6 perimeters, and 1.0 extrusion multiplier to prevent internal void networks that could retain cleaning agents. Printing follows 120°C drying for 4 h, 350°C nozzle, 140°C bed, and 90°C chamber; after support removal, surfaces are cleaned with neutral pH detergent and dried with 0.2 µm filtered air. Solvent wiping with isopropyl alcohol is excluded from the line because the polycarbonate phase in 9085 can undergo environmental stress cracking around mounting bosses. Published data for ULTEM 9085 under ISO 10993-5 cytotoxicity is limited; therefore the material is not assigned to direct tissue-contact or long-duration skin-contact applications without supplier-specific validation. Terminal finished product types include diagnostic device housings, cart-mounted system brackets, and patient-monitor pedestal covers.
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Mitsubishi PEI ULTEM™ 9085 3D printing filament is an amorphous thermoplastic feedstock converted by Mitsubishi Chemical Advanced Materials from SABIC ULTEM 9085 polyetherimide-based resin. ULTEM is a trademark of SABIC Global Technologies B.V. The filament is supplied in 1.75 mm ± 0.05 mm diameter with ovality below 0.03 mm, in sealed spool configurations of 500 g and 1 kg. The resin is a polyetherimide-polycarbonate blend that carries a UL 94 V-0 rating at 1.5 mm. Compared with unfilled polyetherimide grades such as ULTEM 1010, the 9085 blend exhibits higher melt mass-flow rate per ISO 1133-1:2022 and lower heat deflection temperature. This processability offset is intended for fused filament fabrication: it lowers the extrusion setpoint and improves layer-to-layer wetting while retaining flame and smoke performance. Filament conversion is performed on twin-screw extruders with closed-loop melt pumps, triple-zone cooling, and continuous three-axis laser micrometry. Melt temperature at the die is held within ± 2°C, and spooling tension is reduced because polyetherimide blends are stiff and wound-in curvature can create dogleg feed paths.
The primary distinction between ULTEM 9085 and unfilled polyetherimide is thermal-capability offset against processability. Injection-molded ULTEM 9085 resin reports a tensile stress at yield of 69 MPa when tested according to ASTM D638-14 and a flexural modulus of 3,100 MPa when tested according to ASTM D790-17. Unfilled polyetherimide grades may exceed 80 MPa in tensile stress at yield, but their higher glass transition and higher melt viscosity force build-chamber requirements above 150°C. Heat deflection temperature of ULTEM 9085 under 1.82 MPa is approximately 153°C per ASTM D648-18. The polycarbonate modification lowers that value relative to unfilled polyetherimide but provides longer flow length in thin-wall geometries. Compared with PC-ABS, ULTEM 9085 retains an oxygen index of 44% per ISO 4589-2:2017 and a UL 94 V-0 classification at 1.5 mm. PC-ABS systems typically operate in a heat deflection temperature band of 110°C to 125°C and require flame-retardant packages to approach equivalent vertical-burn ratings.
Pre-drying is mandatory before extrusion because the resin absorbs atmospheric moisture rapidly. Undried filament produces voids, hydrolysis-induced viscosity shift, surface roughness, and reduced interlayer strength. Industrial practice is to dry sealed spools at 120°C for at least 4 hours in forced-air or vacuum ovens with a dew point below -40°C. Target moisture content is below 0.05% by weight. At relative humidity above 60%, spools are loaded into heated dry-feed enclosures or returned to dry storage. Moisture content is verified by Karl Fischer titration according to ISO 15512 or ASTM D7191. Open-frame desiccant systems are not adequate for this polymer during sustained high-humidity production months. If a vacuum-sealed bag is punctured or the desiccant indicator shows saturation, the spool is pre-dried even when no surface haze is visible.
The values below are resin supplier data for injection-molded ULTEM 9085, not direct FFF part warranties. Printed-part values shift with raster angle, air gap, chamber temperature, and build orientation.
| Property | Standard | Published value |
|---|---|---|
| Specific gravity | ISO 1183-1:2012 | 1.34 |
| Tensile stress at yield | ASTM D638-14 | 69 MPa |
| Tensile modulus | ASTM D638-14 | 3,000 MPa |
| Flexural modulus | ASTM D790-17 | 3,100 MPa |
| Heat deflection temperature at 1.82 MPa | ASTM D648-18 | 153°C |
| Vicat softening temperature B/120 | ISO 306:2022 | 186°C |
| Oxygen index | ISO 4589-2:2017 | 44% |
| UL 94 vertical burn at 1.5 mm | UL 94 | V-0 |
In fused filament fabrication, the printed article is built by repeated fusion of a moving polymer melt stream onto a cooling road. ULTEM 9085 is amorphous; therefore, interlayer bonding is governed by chain diffusion across the interface rather than crystallite bridging. Industrial FFF systems processing ULTEM 9085 operate a heated build chamber at 120°C to 150°C, with a build sheet temperature of 140°C to 160°C and an extrusion setpoint between 350°C and 390°C. When chamber temperature falls below 120°C, the surface of the previously deposited road cools too quickly and chain interdiffusion is incomplete. The failure mode is brittle delamination between layers rather than ductile rupture within a road. The magnitude of the loss is machine- and toolpath-specific; published data for this exact filament under all raster conditions is limited, but resin supplier guidance imposes a chamber floor of 120°C for full-density aerospace-grade parts.
Hot-end design must be all-metal, not PTFE-lined, because PTFE degradation begins above 260°C. Nozzle diameters of 0.4 mm to 0.6 mm are typical; diameters below 0.25 mm are not recommended because melt fracture and pressure accumulation exceed typical hot-end force limits. Layer height is kept between 0.15 mm and 0.25 mm for load-bearing sections. Larger layer heights reduce interlayer contact time and lower Z-direction strength. The extrusion multiplier is set between 0.98 and 1.02 after drying, with solid infill extracted after three perimeter roads to reduce void density. Prolonged molten residence at 390°C above 5 minutes produces oxidative branching, yellowing, and viscosity increase; purging after thermal interruption is required before part production.
In fused filament fabrication, printed-part mechanical behavior differs sharply from injection-molded coupons. Flat tensile specimens built with alternating 45° raster orientations and solid infill exhibit anisotropy: XY-plane tensile strength is typically higher than Z-direction tensile strength by a factor of two to three. Users should qualify printed coupons according to ASTM D638-14 or ISO 527-2:2012 and record build orientation, raster angle, air gap, and chamber temperature on the test report. Dimensional accuracy is affected by residual stress; large planar sections distort if chamber temperature gradients exceed 5°C across the build volume. Heated polyimide tape, high-temperature build plates, sacrificial rafts, and closed-loop thermal control are standard. First-layer adhesion is achieved at 140°C to 160°C. Published data for Mitsubishi-branded ULTEM 9085 filament in all raster configurations is limited; the table above is not a printed-part warranty.
The resin is selected for aircraft interiors because it supports compliance with FAR 25.853(a) Appendix F Part I vertical burn and FAR 25.853(d) Appendix F Part IV heat release testing at relevant thicknesses. UL 94 V-0 performance at 1.5 mm is accompanied by an oxygen index of 44% per ISO 4589-2:2017. Smoke density testing under ASTM E662 and toxicity testing under BSS 7239 are commonly referenced by qualified fabricators; however, each finished printed article must be revalidated because raster voids, colored additives, and surface sealants alter combustion response relative to injection-molded coupons. The polyetherimide-polycarbonate blend lowers smoke opacity and toxic gas yield compared with many PC-ABS systems, but it is not a non-combustible material and should not be substituted without component-level certification.
Chemical compatibility boundaries are defined by the polyetherimide and polycarbonate phases. Resistance is acceptable for aliphatic hydrocarbons, alcohols, and dilute aqueous detergent solutions at ambient temperature. Continuous immersion in hot water above 80°C, steam, strong mineral acids, ketones, esters, chlorinated solvents, and N-methyl-2-pyrrolidone is not recommended. Environmental stress cracking may occur under tensile load in methylene chloride, toluene, or strong aromatic hydrocarbon exposure. Solvent-welded assemblies require compatibility trials, and residual solvent must be evaporated before thermal post-treatment. Isopropyl alcohol wiping is acceptable only if the surface is fully dry before chamber heating; retained solvent causes surface crazing and interlayer softening.
After printing, support removal is performed mechanically or with high-temperature soluble supports where the FFF platform permits. Sanding, drilling, and insert installation generate fine amorphous particulate; local exhaust ventilation and HEPA filtration are required. Machined edges are deburred under dry conditions. Annealing may be applied at 150°C to 180°C for 2 hours to 4 hours to reduce residual stress, but dimensional change and flatness loss are mapped on a first-article basis. Non-destructive inspection includes visual transillumination for gross voids, ultrasonic pulse-echo scanning for delamination, and structured-light dimensional audit against CAD. Acceptance criteria are part-specific; no universal NDT threshold applies.