| HS Code | 177954 |
| Density | 1.16 g/cm³ |
| Tensile Modulus | 7.8 GPa |
| Tensile Strength At Break | 120 MPa |
| Elongation At Break | 3% |
| Flexural Modulus | 7.5 GPa |
| Flexural Strength | 160 MPa |
| Charpy Impact Notched | 5 kJ/m² |
| Melting Point | 178 °C |
| Heat Deflection Temperature At 1 8 Mpa | 175 °C |
| Vicat Softening Temperature | 180 °C |
| Water Absorption 24h | 0.3% |
| Volume Resistivity | 1E3 ohm·cm |
As an accredited Arkema Rilsamid ASR 13 PA12-CF15 factory, we enforce strict quality protocols—every batch undergoes rigorous testing to ensure consistent efficacy and safety standards.
| Packing | Supplied in sealed 25 kg moisture-proof bags, labeled with product identification, batch number, and handling precautions for safe storage. |
| Container Loading (20′ FCL) | 20′ FCL of Arkema Rilsamid ASR 13 PA12-CF15: carbon-fiber-reinforced PA12 granules, palletized in moisture-proof bags, secured for safe transport. |
| Shipping | Arkema Rilsamid ASR 13 PA12-CF15 is a carbon-fiber-reinforced polyamide 12 grade supplied as granules. Ship in sealed, moisture-proof packaging to prevent humidity pickup. Store in cool, dry conditions away from direct sunlight and heat sources. No special hazard classification; standard non-hazardous industrial shipping applies with proper labeling and documentation. |
| Storage | Store Arkema Rilsamid ASR 13 PA12-CF15 in its original, sealed container in a cool, dry, well-ventilated area. Keep away from direct sunlight, heat sources, and excessive humidity, as moisture can affect performance. Maintain stable temperatures and avoid stacking heavy loads. Ensure container remains tightly closed to prevent contamination until use. |
| Shelf Life | Shelf life is typically 2 years from date of manufacture when stored in original, unopened packaging under dry, cool conditions. |
Fuel filler neck injection moulding with Arkema Rilsamid ASR 13 PA12-CF15 is specified for components that must combine automotive fuel contact resistance with electrostatic dissipation during refuelling. The PA12 matrix is evaluated under ISO 175 immersion using reference liquids ISO 1817 Fluid C and Fuel A; the 15 wt% carbon fibre loading creates a semi-conductive network that brings surface resistivity into the dissipative range described in ANSI/ESD STM11.11, typically between 1×104 Ω and 1×109 Ω after conditioning at 23°C and 12% RH. Pre-drying in a desiccant dryer at 80°C for 4 h to a residual moisture content below 0.15 wt% as determined by ISO 15512 is mandatory; moisture above 0.20 wt% produces hydrolysis during plastication, lowers weld-line strength, and increases volatile generation at the melt front. Melt temperature should be maintained between 240°C and 280°C, with mould temperature controlled between 60°C and 90°C to improve fibre wet-out and reduce exposed fibre ends at snap-fit retention features. Tool steel should be hardened to 58–62 HRC because the carbon fibre abrades unprotected ejector pins, gate inserts, and shut-offs; hot runner valve gates are preferred over cold sprues for cylindrical filler neck geometries to avoid centre-line weld lines that reduce hoop stress capacity. Long-term fuel immersion according to SAE J1645 or the relevant OEM specification is required before production validation; published data for this specific grade under aggressive sour gasoline at 60°C are limited, and testing should be performed on moulded plaques rather than machined specimens. The fibre loading lowers coefficient of linear thermal expansion into the range of 3×10-5 K-1 to 5×10-5 K-1 in the flow direction under ISO 11359-2, reducing diametral clearance change against a metal spigot. Weld-line strength in filler neck shear joints remains processing-sensitive: a gating location that places a weld line in a snap-fit retention window can reduce ultimate force by 25–40% compared with an unwelded ISO 527-2/1A specimen. Full component burst and impact tests at -40°C according to SAE J1681 or equivalent are required because carbon fibre reduces low-temperature ductility relative to unfilled PA12.
Carbon-fibre filled PA12 gear blanks are introduced into oil-splash auxiliary drives where machined POM or steel blanks must be replaced to reduce rotating inertia and gear mesh noise. The limiting design parameter is not short-term tensile overload but tooth-root fatigue and flank wear; VDI 2736 supplies thermoplastic gear load-capacity calculations and requires temperature-dependent modulus and creep data instead of a single 23°C datasheet value. The dry-as-moulded tensile modulus of this class of 15 wt% carbon fibre PA12 compound falls in the range of 7,000–9,500 MPa under ISO 527-2/1A, but at 60°C in oil-splash the matrix modulus drops and gear root stress must be derated using the modulus at maximum continuous oil temperature. Carbon fibre at 15 wt% loading reduces flank wear under boundary lubrication, but the mating shaft should be hardened stainless steel or coated because an unprotected low-alloy steel shaft in a humid enclosure can show electrochemical corrosion at the carbon fibre contact zone. Injection moulding of gear blanks requires a screw with L/D 20:1 and compression ratio near 2:1 to limit fibre breakage; severe fibre breakage lowers fibre aspect ratio, increases surface resistivity, and reduces modulus. Edge gates below 0.8 mm thickness generate high shear heating and local oxidation; rim gating with rectangular edge gates of 1.0–1.5 mm thickness is preferred for gear blanks. Mould temperatures below 60°C produce resin-rich skins and internal voids, reducing flank wear resistance and dimensional repeatability. Tooth profile corrections should be made in tooling rather than by post-machining because interrupted milling of short carbon fibre PA12 creates fibre pull-out and micro-cracks at flank surfaces. PA12 absorbs less water than PA6 or PA66 at 50% RH under ISO 62, with equilibrium moisture below 0.8 wt%, so centre-distance shift in service is controlled; however, pitting life data for this specific fibre distribution should be generated on an actual gear rig according to VDI 2736 because published values for this configuration are limited.
For electrostatic-dissipative wafer handling nests machined from pre-dried PA12-CF15 plate or injection-moulded to near-net shape, the primary qualification is surface resistance stability in low-humidity handling environments. The carbon fibre network becomes electrically available only after the resin-rich mould skin is removed; as-moulded surfaces can measure above 1×1011 Ω, while machined or vapour-honed surfaces typically measure in the dissipative range of 1×104–1×109 Ω under ANSI/ESD STM11.11. Release agents, coolant residues, and fingerprints shift surface resistance upward; aqueous cleaning in deionised water at 40°C followed by a dry-air bake at 60°C for 2 h is used before qualification. Compliance with ANSI/ESD S20.20 requires verification on the actual textured surface, not on a compression-moulded film. Particle release is a separate boundary condition: exposed carbon fibre ends can detach at sharp edges under ultrasonic cleaning or repeated wafer contact, so unsealed nests are not appropriate for ISO 14644-1 Class 3 direct-contact service unless post-process sealing is validated. Dimensional stability of wafer nests is governed by moisture uptake; at 23°C and 50% RH the PA12 matrix absorbs below 0.8 wt% water under ISO 62, producing length change generally below 0.1%. This is lower than PA6 or PA66 but still significant for nests with flatness tolerances of ±0.05 mm. Annealing at 100°C for 2 h after machining relieves residual stress and stabilises fibre protrusion; subsequent inspection should be performed after 24 h at the same temperature and humidity. Diamond-coated tooling at 600–1,200 m/min surface speed and chip load of 0.05–0.10 mm/rev reduces edge burr and fibre pull-out during machining of the filled compound.
| Application segment | Dominant property or risk | Verification standard | Operational boundary |
|---|---|---|---|
| Fuel filler necks and quick connectors | Electrostatic dissipation, fuel resistance, weld-line strength | SAE J1645, ISO 175, ASTM D257 | Pre-dry to <0.15 wt% moisture; avoid melt residence >8 min at 280°C |
| Oil-splash gear blanks | Tooth-root fatigue, flank wear, thermal expansion | VDI 2736, ISO 7148-1, ISO 11359-2 | Derate modulus at maximum oil temperature; coat mating shafts against galvanic attack |
| Electrostatic-dissipative wafer nests | Surface resistance, particle release, dimensional stability | ANSI/ESD STM11.11, ISO 14644-1, ISO 62 | Remove resin-rich skin; verify actual textured surface after cleaning |
| Snap-fit assembly brackets | Notched impact, weld-line location, moisture-conditioning trade-off | ISO 179-1/1eA, ISO 527-2/1A | Keep outer-fibre strain below 1.5% at -20°C unless prototype cantilever tests confirm otherwise |
| Dry-sliding linear guide pads | PV limit, frictional heat, counterface abrasion | ISO 7148-1, ISO 75-2 | Preliminary design limit 0.35 MPa·m/s at 23°C; verify at service speed |
| Orthotic and prosthetic shells | Cyclic bending, fatigue, patient-contact compliance | ISO 22523, ISO 22675, ISO 10993-5 | Do not substitute for continuous carbon fibre laminates in energy-storage orthoses |
Snap-fit assembly brackets moulded from Arkema Rilsamid ASR 13 PA12-CF15 fail most often when the design uses unfilled PA12 snap-fit deflections without re-evaluating notched impact and fibre orientation. The 15 wt% short carbon fibre loading reduces notched Charpy impact energy measured under ISO 179-1/1eA to approximately one-third to one-half of unfilled PA12, and the value measured perpendicular to flow is typically lower than the value measured parallel to flow because of fibre orientation. Snap-fit outer-fibre strain should therefore remain below 1.5% at -20°C unless prototype cantilever tests on the actual tooled geometry confirm higher allowable assembly strain. Drying at 80°C for 4 h under -40°C dew point is more critical in snap-fits than in solid blocks; residual moisture above 0.15 wt% plasticises the PA12 matrix, reduces stiffness, lowers assembly force, and increases elongation. This creates a moisture trade-off: dry-as-moulded parts exhibit higher modulus but lower impact, while moisture-conditioned parts exhibit lower modulus but higher ductility. For repeatable snap-fit insertion force and retention force, production parts should be conditioned to equilibrium at 23°C and 50% RH before assembly, or assembly forces should be tested at both dry and conditioned states. Weld lines crossing the root of a snap-fit beam are not acceptable in most bracket geometries; side gating along the beam length or a sequential valve gate programme moves the weld line into a low-stress region. When a weld line crosses the snap-fit root, ultimate force can fall by more than 25% compared with an unwelded specimen of the same nominal wall thickness. Fiber orientation should be checked on polished cross-sections from each production cavity, because changes in fill speed alter the orientation tensor at the beam root and therefore change both stiffness and crack initiation resistance. The use of a continuously variable mould temperature near the gate can improve surface appearance but also reduces gate freeze-off time, making polymer flow length shorter and increasing the risk of short shots in thin snap-fit arms. In tools with long cold runner drops, runner diameter below 5 mm causes excessive shear heating and fibre breakage in the runner itself, which can produce black specks and local conductivity variation in the moulded brackets.
Dry-sliding linear guide pads moulded from PA12-CF15 operate against ground stainless steel rails with surface finish Ra 0.2–0.4 µm. Load capacity is limited by frictional heat at the interface rather than compressive strength. Under ISO 7148-1 sliding wear testing, the compound exhibits process-dependent wear behaviour: fibre orientation perpendicular to the sliding surface produces a hard wear face but increases counterface polishing, whereas orientation parallel to sliding direction lowers coefficient of friction but leaves exposed fibre ends that can abrade softer counterfaces. A preliminary design limit of 0.35 MPa·m/s at 23°C is applied until ISO 7148-1 data at the actual service speed confirms otherwise; continuous dry operation above this PV threshold may raise interface temperature past the glass transition of the PA12 matrix, causing surface melting, transfer smearing, and sudden loss of clearance. The PA12 matrix absorbs mineral oil and water; oil lubrication decreases friction but swells the part slightly, so dimensions must be verified after immersion under ISO 175 before specifying assembly clearance. Chlorinated solvents, strong acids, and alkaline solutions above 50% concentration are not considered compatible without case-by-case immersion testing. Carbon fibre-filled PA12 can abrade aluminium counterfaces rapidly in unlubricated service; hard-anodised aluminium or stainless steel is preferred. At speeds above 1.0 m/s, dynamic coefficient of friction against 0.2 µm Ra stainless steel may increase as the polymer surface heats, and the pad should be instrumented for interface temperature in prototype testing rather than relying on ambient temperature measurements. The absence of graphite or MoS₂ in the compound means that wear debris consists largely of PA12 matrix and broken carbon fibre; in clean-room or optical assembly environments, containment and debris management must be addressed before specifying the material for exposed sliding guides.
In lower-limb orthotic shell fabrication, PA12-CF15 is selected where the 15 wt% carbon fibre content reduces section thickness for a given flexural stiffness and lowers device mass compared with unfilled PA12. The material is not a replacement for continuous carbon fibre laminates in energy-storage ankle-foot orthoses; its short-fibre reinforcement improves stiffness-to-density ratio but does not provide the fatigue resistance of laminated carbon/epoxy under cyclic toe-off loading. ISO 22523 defines structural requirements for external orthoses, and ISO 22675 fatigue testing of ankle-foot devices imposes cyclic loading that requires prototype-level verification because published data for short-fibre PA12-CF15 in this specific test configuration are limited. Sheet material should be pre-dried below 0.15 wt% moisture before extrusion or vacuum forming; heating is carried out in an infrared oven to 220–260°C. Heating above 280°C degrades the PA12 matrix and causes surface discoloration, while heating below 200°C produces fibre buckling and visible silver streaks during forming. Vacuum-formed shells exhibit anisotropic shrinkage, so trimming fixtures must allow 0.3–0.8% dimensional relaxation after 24 h at 23°C. Attachment holes drilled through carbon fibre-loaded sheet should be reamed rather than laser cut because laser cutting produces charred fibre ends that reduce local fatigue strength. Patient-contact compliance must be verified under ISO 10993-5 and ISO 10993-10 for the specific grade and sterilisation protocol, because carbon fibre-filled PA12 can release particles at cut edges. Steam autoclave cycles above 121°C may distort load-bearing shells because matrix modulus falls sharply at elevated temperature, particularly at retained moisture levels above 0.15 wt%.
Robotic end-of-arm tooling frames, grip fingers, and locating pins are machined from PA12-CF15 sheet or injection-moulded where low weight, moderate stiffness, and electrostatic dissipation are required on the same component. Robot cell humidity often fluctuates between 30% RH and 65% RH; the PA12 matrix responds with a dimensional change that is lower than PA6 or PA66 but measurable. At 50% RH equilibrium under ISO 62, the matrix absorbs approximately 0.7 wt% water, and carbon fibre reduces volumetric swelling relative to unfilled PA12. Anisotropic fibre orientation means that inspection axes must be defined from the moulding or sheet direction: a locating pin machined across the sheet thickness retains more dimension in the thickness axis, but a 300 mm length may shift by 0.10–0.15 mm when moved from 20% RH to 65% RH. Production fixtures should be condition-normalised for 24 h before final CNC machining and dimensional sign-off; geometric evaluation under ISO 1101 after conditioning is recommended. The 15 wt% carbon fibre content also changes gripping behaviour: direct contact with soft aluminium or painted workpieces can leave marks, so grip pads often require replaceable elastomer inserts. End-effector frames subjected to robot collision loads should use a safety factor not lower than 2.0 on the 23°C tensile strength measured under ISO 527-2/1A, because machined holes and threads create local stress concentration factors of 2.0–3.0 in this short-fibre system. Threaded inserts are preferred over tapped threads; if tapping is unavoidable, thread flanks expose carbon fibre and can lose preload after repeated thermal or moisture cycling. Machining should use compressed air or mist coolant instead of flood coolant, because PA12 absorbs water during machining and can temporarily alter the bore dimension before final inspection.
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Arkema Rilsamid ASR 13 PA12-CF15 is an injection-moulding grade of polyamide 12 compounded with a nominal 15% by mass carbon fibre reinforcement. The material carries the ISO 1043-1 designation PA12-CF15 and is supplied as cylindrical black pellets in moisture-proof packaging. Unlike unfilled Rilsamid PA12, the carbon fibre phase establishes a dissipative electrical network and raises tensile modulus while suppressing ductile elongation. The grade is intended for small-to-medium technical parts such as fuel-system retaining clips, pneumatic fitting bodies, sensor brackets, ESD-safe housings, and lightweight mechanical components in which dimensional stability under low moisture uptake is required. The product is not intended for high-voltage insulation; electrical performance is limited to static-dissipative or moderately conductive service.
Published grade-specific data for ASR 13 is limited, and the specification ranges presented below are based on the expected property class for a 15% carbon-fibre PA12 compound. Downstream lot acceptance should use the ISO methods listed and retained pellets conditioned according to ISO 291:2008. The current Arkema technical datasheet remains the controlling document for exact batch values.
| Property | Test standard | Representative range |
|---|---|---|
| Density at 23°C | ISO 1183-1:2019 | 1.08–1.12 g/cm³ |
| Tensile modulus | ISO 527-2:2012 | 8,500–11,000 MPa |
| Tensile strength at break | ISO 527-2:2012 | 100–140 MPa |
| Elongation at break | ISO 527-2:2012 | 2.5–5.0% |
| Charpy unnotched impact at 23°C | ISO 179-1:2020 | 25–40 kJ/m² |
| Heat deflection temperature at 1.8 MPa | ISO 75-2:2013 | 160–175 °C |
| Volume resistivity | IEC 62631-3-2:2016 | 10²–10⁵ Ω·cm |
| Water absorption at 23°C, 50% RH | ISO 62:2008 | 0.7–1.0% |
At 15% by mass, carbon fibre loading is above the electrical percolation threshold for injection-moulded PA12, but the conductive network is sensitive to fibre length retention. Fibre length distributions measured after moulding typically shift from a compounded mean of 180–250 μm to a moulded mean of 120–180 μm; the fraction of fibres longer than 300 μm controls both conductivity and local tensile modulus. High backpressure and restrictive check-ring clearances reduce fibre length, while low backpressure can produce non-uniform dispersion and shot-to-shot resistivity drift. Melt temperature for the PA12 matrix is controlled between 230°C and 260°C, with a preferred melt temperature of 250°C at the nozzle. The polymer melting peak measured by ISO 11357-3:2018 is approximately 175–180°C.
The tensile modulus of ASR 13 is governed by shear-lag load transfer from the PA12 matrix to the carbon fibre. At 15% fibre loading, tensile modulus typically falls between 8,500 and 11,000 MPa, roughly four to six times the stiffness of unfilled PA12, while tensile strength at break usually falls between 100 and 140 MPa. Elongation at break is reduced to 2.5–5.0%, and the failure mechanism shifts from matrix ductility to fibre-dominated fracture. Test specimens must be moulded and conditioned according to ISO 527-2:2012; values obtained on dry-as-moulded specimens differ from those obtained after moisture equilibrium.
Electrical conductivity is not a fixed value; it depends on gate type, melt temperature, injection speed, and mould cavity wall temperature. Surface resistivity measured on a 4 mm end-gated plaque per IEC 61340-2-3:2016 generally falls within 10³–10⁶ Ω/sq, but narrow flow paths and long residence times can shift resistivity by 1–2 decades. Mould temperature influences skin morphology and carbon-fibre wetting; published data for this specific configuration is limited, so resistivity mapping should be performed on actual production parts.
Cylinder and screw wear observed on production equipment with a 40 mm, 22:1 L/D screw is concentrated at the transition zone, check-ring seat, and nozzle tip. Hardened screw flights and bimetallic barrels are specified for runs above 20,000 cycles; untreated nitrided screws can lose 0.1–0.3 mm of flight clearance within 10,000 cycles when the material is processed at 250°C barrel temperature and 100 rpm screw speed. When the screw cushion falls below 2 mm, carbon fibre agglomerates at the check-ring seat and the non-return valve leaks, transferring hold pressure poorly and causing short shots or density variation. A cushion of 3–6 mm and backpressure of 2–5 MPa reduce shot-volume variability.
Predrying is mandatory when storage has exceeded 48 h at warehouse RH above 60%. A desiccant dryer with a dew point of -30°C or lower at 80°C for 4–6 h reduces pellet moisture to 0.15% or below. Hydrolysis of the polyamide backbone accelerates above 0.15% moisture at melt temperature, causing viscosity loss, surface splay, and reduced weld strength. Do not dry in hoppers supplied with unconditioned ambient air.
Carbon fibre orientation at knit lines prevents fibre crossing; tensile strength measured on a weld-line specimen per ISO 527-2 is typically 30–50% lower than the non-weld-line value. Gate placement must therefore avoid knit lines in areas subject to hoop stress, pressure pulses, or impact. Where multiple gates are unavoidable, sequential valve gating or overflow wells are used to shift the knit line to a low-stress region. Mould temperatures at the upper end of the range reduce visible knit-line depth but do not fully restore tensile strength.
Typical parts moulded from ASR 13 have wall thicknesses between 0.8 mm and 4.0 mm. Below 0.8 mm, carbon fibre orientation and filling pressure become dominant constraints. Gates should be sized at 50–70% of wall thickness, and cold or hot-runner systems should use generous diameters to limit fibre breakage. Hot-runner nozzles smaller than 1.0 mm can create fibre jamming and pressure spikes; valve-gate systems should use gates of at least 1.5 mm.
The effective melt viscosity of ASR 13 at 250°C and 1,000 s⁻¹ is higher than unfilled PA12 but remains shear-thinning; the power-law index measured on a capillary rheometer is approximately 0.4–0.6. Increasing melt temperature above 260°C produces only limited viscosity reduction and accelerates thermal oxidative degradation. Flow length in thin walls is therefore more sensitive to injection speed than to barrel temperature.
Compared with unfilled Rilsamid PA12, ASR 13 raises tensile modulus from approximately 1,500 MPa to 8,500–11,000 MPa and reduces elongation at break from over 200% to 2.5–5.0%. Creep resistance under load is improved because the carbon fibres carry stress in the polyamide 12 matrix; however, the material is more notch-sensitive and less suitable for snap-fit arms that require large strain.
Compared with a 15% glass-fibre PA12, ASR 13 provides a higher specific modulus because carbon fibre has a density of approximately 1.8 g/cm³ and tensile modulus of approximately 230 GPa, whereas E-glass has a density of approximately 2.54 g/cm³ and tensile modulus of approximately 72 GPa. The carbon fibre grade also provides lower dry-running friction and some electrical conductivity, while glass fibre remains an electrical insulator and increases density. The trade-off is higher compound cost and more aggressive tooling wear.
Compared with a 30% carbon-fibre PA12, ASR 13 offers lower stiffness and strength but better thin-wall flow, lower screw and barrel abrasion, and lower anisotropic warpage from fibre orientation. For structural brackets requiring maximum flexural modulus, a 30% carbon-fibre grade may be selected; for small connectors and thin-wall housings, the 15% loading reduces filling pressure and reduces fibre breakage in narrow gates.
Compliance documentation is controlled under REACH Regulation EC 1907/2006 and RoHS Directive 2011/65/EU as amended by (EU) 2015/863. The as-supplied pellet does not intentionally contain lead, mercury, cadmium, hexavalent chromium, polybrominated biphenyls, or polybrominated diphenyl ethers above the RoHS maximum concentration values. Workplace dust from machining or regrinding of carbon-fibre filled parts should be controlled according to local occupational exposure limits; carbon fibre particulate is conductive and must not enter electrical enclosures. Do not combine the melt with strong acidic process residues or with incompatible purge compounds such as acetal at PA12 processing temperatures, because decomposition products can accelerate polyamide degradation. For parts exposed to zinc chloride, road salt, or oxygenated solvents, qualification under ISO 22088-3:2006 is recommended before production release.