| HS Code | 483658 |
| Polymertype | Acrylonitrile styrene acrylate (ASA) |
| Density | 1.07 g/cm³ |
| Tensilestrength | 45 MPa |
| Flexuralmodulus | 2200 MPa |
| Elongationatbreak | 20% |
| Izodimpactstrength | 100 J/m |
| Heatdeflectiontemperature | 85 °C |
| Vicatsofteningtemperature | 95 °C |
| Waterabsorption | 0.3% |
| Moldingshrinkage | 0.4–0.7% |
| Ul94flammability | HB |
| Dielectricconstant | 3.0 at 1 MHz |
As an accredited Hitachi Chemical ASA factory, we enforce strict quality protocols—every batch undergoes rigorous testing to ensure consistent efficacy and safety standards.
| Packing | Hitachi Chemical ASA is supplied in 25 kg moisture-proof paper bags with polyethylene liners, palletized for industrial handling. |
| Container Loading (20′ FCL) | Hitachi Chemical ASA is securely loaded into a 20-foot FCL container for safe, dry, and compliant chemical transport. |
| Shipping | Ship Hitachi Chemical ASA in sealed, labeled bags or drums, kept cool, dry, and ventilated, away from moisture, heat, and incompatible materials. Follow the SDS and all local/national transport regulations; use appropriate PPE during handling. Dangerous-goods classification depends on the specific grade/SDS. |
| Storage | Store Hitachi Chemical ASA in a cool, dry, well-ventilated area away from heat, sparks, flames, and direct sunlight. Keep containers tightly closed and protect from moisture, water, and contamination. Avoid contact with strong oxidizers, acids, and bases. Use secondary containment, label clearly, and follow the manufacturer’s SDS for specific temperature limits and shelf life. |
| Shelf Life | The shelf life of Hitachi Chemical ASA is typically 12 months from manufacture when stored unopened in original packaging under recommended conditions. |
Hitachi Chemical ASA is selected for unpainted mirror housings, radiator grilles, cowl vent panels, roof ditch mouldings, and exterior B-pillar covers because the saturated acrylate rubber phase eliminates the 1,3-butadiene double bonds that initiate photo-oxidative scission and gloss loss in ISO 4892-2 xenon-arc testing. The injection moulding window is narrower than for general-purpose ABS. Pre-drying in a desiccant-wheel dryer with dew point below -40°C at 80°C for 4 h is required to reduce moisture to 0.03% or less. Residual moisture above 0.08% produces silver streaking and splay on high-gloss black parts. Melt temperature at the nozzle is held at 240–260°C. Mould surface temperature is maintained at 70–90°C to reproduce low-gloss grains such as VDI 24 and VDI 27 without flow lines. On multi-cavity mirror-housing tools with valve-gated hot runners, clamp force ranges from 3.5 kN/cm² to 5.0 kN/cm² of projected area. Weld-line strength in grille frames falls 20–35% below that of the base material when melt fronts meet below 70°C mould temperature. Gates are therefore positioned away from clip bosses and screw bosses. Thin-wall sections below 1.2 mm require high-flow ASA with melt flow rate of 20 g/10 min under 220°C/10 kg load using ISO 1133-1. Gloss retention after 1000 h of ISO 4892-2 xenon-arc with daylight filters is reported at 80–90% for dark grey and black commercial ASA, whereas unstabilised ABS frequently falls below 50%. Notched Charpy impact under ISO 179-1/1eA at 23°C is typically 15–25 kJ/m²; at -30°C the value drops to 5–8 kJ/m², which is relevant for winter impact validation. Because unpainted ASA parts rely on surface integrity, post-mould flame or plasma treatment must raise surface energy to 48–56 mN/m before polyurethane adhesive bonding. The linear coefficient of thermal expansion is typically 80–100×10⁻⁶ K⁻¹, and an expansion difference of 0.2–0.4 mm/m occurs over a 40°C service temperature swing when ASA trim is attached to steel or aluminium carriers. Continuous service above 105°C is not recommended. Exposure to aromatic hydrocarbons or ketone-based solvents requires stress-cracking validation, not a simple immersion check.
ASA capstock over rigid PVC for window profiles, fascia panels, and soffit boards is processed as a coextruded layer, not as a monolithic extrusion. The functional capstock thickness is 0.10–0.20 mm. Below 0.08 mm, UV absorber concentration per unit surface area is insufficient to protect the PVC substrate, and migration of titanium dioxide from the substrate produces haze. Above 0.25 mm, differential melt viscosity between the ASA layer and PVC core produces layer-thickness variation, surface waves, and gloss non-uniformity at line speeds above 2.5 m/min. The PVC core is extruded on a counter-rotating conical twin-screw machine with screw diameter 55–65 mm, while the ASA top layer is fed by a single-screw extruder with L/D 24:1–30:1. ASA capstock melt temperature at the feedblock is held at 190–210°C. Die exit temperature is controlled between 195°C and 215°C. Processing above 230°C causes yellowing and generates gel particles in ASA due to acrylic-ester thermal degradation. Calibration vacuum is set at 0.06–0.08 MPa to prevent capstock delamination. The linear thermal expansion mismatch between ASA with coefficient 80–100×10⁻⁶ K⁻¹ and rigid PVC with coefficient 60–80×10⁻⁶ K⁻¹ creates bowing risk for dark profiles exposed to direct sun. A profile surface temperature of 70°C on a 2 m dark-coloured profile can produce a differential length change of 0.2–0.4 mm. Tropical solar qualification for capstock typically uses ISO 4892-2 xenon-arc at 0.51 W/m² at 340 nm and black-panel temperature 65°C for 6000 h. Acceptance criteria include grey scale rating not less than 4 under ISO 105-A02 and ΔE not more than 5 under ISO 7724. Published data for the specific Hitachi Chemical ASA capstock grade in high-line-speed PVC coextrusion is limited; the above ranges are process-control targets derived from commercial ASA capstock datasheets and profile qualification practice.
| Qualification | Standard | Condition | Requirement or observed range | Process failure mode |
|---|---|---|---|---|
| Xenon-arc weathering | ISO 4892-2 | Daylight filter, 0.51 W/m² at 340 nm, black panel 65°C, 6000 h | ΔE ≤ 5; grey scale ≥ 4 under ISO 105-A02 | Capstock below 0.08 mm depletes UV absorber |
| Gloss retention | ISO 2813 | 60° specular geometry | 70–90 GU initial; loss less than 15 GU after 3000 h | Die temperature above 230°C causes gel specks |
| Vicat softening | ISO 306/B50 | 50 N load, heating rate 50°C/h | ASA capstock 92–105°C | PVC core overheating while ASA remains below its melt temperature |
| Tensile modulus | ISO 527-2/1A | Test speed 1 mm/min, 23°C | 2300–2800 MPa | Moisture above 0.03% lowers modulus and raises splay |
Outdoor telecom cabinets, electric-vehicle charging posts, and solar inverter enclosures use Hitachi Chemical ASA when the housing must pass UL 746C F1 outdoor suitability without the heavy UV cap layer needed for PVC. Sheet stock at 3–6 mm is extruded and then vacuum-formed or pressure-formed. Top heater banks are set at 250–280°C, and bottom banks at 210–240°C. The broader bottom-to-top offset reflects the higher melt strength of ASA relative to ABS and its tendency to overheat at the bottom sheet surface. Formed halves are joined by hot-plate welding at 220–240°C under 0.3–0.6 MPa joint pressure or by ultrasonic welding at 20 kHz with amplitude 40–60 µm. Carbon black content above 2% reduces ultrasonic joint strength and causes variable power draw at the transducer. UL 746C F1 evaluation combines long-term UV or xenon exposure, flammability after exposure, and impact retention. ASA grades without flame retardants are typically UL 94 HB; flame-retarded compounds achieve V-0 at 1.5–3.0 mm but sacrifice some outdoor gloss stability because halogen or phosphorus additives can migrate. After 1000 h of ISO 4892-2, general-purpose ASA retains more than 70% of tensile impact strength, while general-purpose ABS drops below 40%. Post-mould machining is a concern because the outer surface contains the highest concentration of UV absorber, and drilling or routing through the skin exposes a core with lower stabilizer content. Exposed core surfaces chalk earlier and deliver lower electrical insulation resistance under IEC 60112 comparative tracking index conditions after weathering. Surface resistivity after weathering should remain above 1×10¹³ Ω under IEC 60093 for electrical enclosure applications. For sealing, compression-set-resistant EPDM or silicone gaskets are preferred; polyurethane foam gaskets should be avoided because they absorb water and hold it against the ASA surface during freeze-thaw cycles.
ASA is used for injection-moulded deck hatches, instrument bezels, non-structural trim plates, and ventilation cowls in marine applications where painted ABS fails by paint delamination and substrate chalking. Single-test xenon-arc or salt-spray qualification underestimates field degradation because salt crystals deposited during ISO 9227 neutral salt spray alter the UV attenuation pattern in subsequent ISO 4892-2 exposure. A sequenced test programme of 500 h salt fog followed by 1000 h xenon-arc, with an intermediate rinse in deionised water, is used before gloss and colour measurements. Injection moulding uses melt temperatures of 230–250°C and mould temperatures of 60–80°C. Mould shrinkage is 0.4–0.6%. Tools sized for ABS often produce acceptable first-off geometry if the gate is not positioned on a visible surface. Packing pressure is maintained at 50–70 MPa to avoid sink marks around ribs and bosses. Snap-fit and screw-boss sections are more sensitive to moulded-in stress than ABS, so annealing at 80°C for 2 h is applied after moulding when parts are exposed to alkaline cleaners above pH 10 or methanol-based deicers. Continuous below-waterline immersion is outside the intended service envelope, especially in ester-based hydraulic fluids. Bonding of acrylic or polyurethane sealants to ASA requires surface energy raised to 48–56 mN/m by plasma or flame. The component should not be post-painted; if colour matching to gelcoat is required, a pre-coloured ASA or an in-mould decorated acrylic film offers better chip resistance than liquid coating. Published data for Hitachi Chemical ASA in marine deck hardware is limited to general weathering and mechanical property retention. Project-specific validation against ISO 12215 is not satisfied by ASA alone for load-bearing hull structures, but deck hatches and non-structural trim fall outside the high-load laminate schedule and can be qualified by the sequenced salt-fog and xenon protocol.
String-trimmer motor housings, hedge-trimmer handle clamshells, and backpack-blower fan shrouds use ASA where sunlight exposure and petroleum splash coexist. The processing constraint is not temperature alone but rib fill. Injection moulding should use melt temperature 235–255°C and mould temperature 65–85°C. The cooling circuit must maintain a cavity-to-cavity temperature variation below 15°C; larger differences produce differential shrinkage and bowing in long clamshells. Flow length to wall thickness ratio for ASA is limited to approximately 120:1 at 250°C. Rib-to-wall ratio is kept between 0.5 and 0.6. Boss outer diameter is 2.0–2.5 times the screw major diameter to prevent sink marks and boss cracking. Hydraulic injection speed is set at 50–80 mm/s for thick-walled bosses and lower for thin cosmetic surfaces. Impact-modified ASA grades with notched Charpy impact not less than 25 kJ/m² under ISO 179-1/1eA at 23°C are specified for drop resistance. ASA withstands occasional fuel splash from gasoline-ethanol blends, but continuous immersion in fuel or aromatic solvents is outside the boundary; the fuel tank remains HDPE or nylon. Vibration welding of two moulded halves is performed at 200–240 Hz with amplitude 1.0–1.8 mm. Weld depth is controlled to 0.8–1.2 mm because over-welding ejects degraded material and weakens the joint. After welding, flash traps must be located away from fuel-vapour migration paths. Where the tool housing attaches to vibration mount elastomers, adhesion of TPE or EPDM gaskets must be revalidated after 72 h of ISO 1817 reference-fuel immersion because plasticizer migration changes surface energy. For battery-electric tools, the enclosure is usually required to meet EN 62841-1 mechanical shock, but ASA does not by itself provide the impact or flame performance of blends used for power tool end caps; verification is done on the final tool assembly. Published creep test data for ASA in power-tool housing shapes is limited, so structural bosses should be validated under thermal cycling from -20°C to 70°C rather than by short-term tensile data alone.
ASA filament for fused deposition modelling is used to print outdoor fixture brackets, agricultural sensor supports, irrigation valve covers, and short-run replacement grilles. Pellet-to-filament conversion uses a single-screw extruder with L/D 24:1–30:1 and a melt pump to hold diameter at 1.75 mm ± 0.05 mm or 2.85 mm ± 0.05 mm. The resin must be dried to 0.02% moisture or less before extrusion; elevated moisture causes filament microbubbles and diameter oscillation. Printing parameters on enclosed machines include nozzle temperature 240–260°C, build plate 90–110°C, chamber temperature above 50°C, and part-cooling fan speed limited to 30–50%. Layer height is set at 0.15–0.25 mm with printing speed 40–70 mm/s for a 0.4 mm nozzle. Interlayer fusion is the limiting mechanical property. Tensile strength in the build direction is often 40–60% lower than in the XY plane, and published data for the specific Hitachi Chemical ASA grade is limited. Printed holes under compression split along layer interfaces unless steel heat-set inserts M3–M5 are used after printing. Annealing at 80–90°C for 2 h reduces residual stress and improves interlayer crack resistance but produces anisotropic shrinkage of 0.2–0.5% in the build direction. UV resistance of the printed surface depends on layer fusion rather than bulk chemistry; exposed stair-stepped sidewalls have higher surface area and retain moisture longer than smooth injection-moulded surfaces. Outdoor printed parts should be tested under ISO 4892-2 after coating or vapour smoothing if dimensional stability is critical. ASA filament is not recommended for continuous service above 85°C under load, and contact with undiluted acetone or ester solvents causes stress cracking at interlayer boundaries.
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