| HS Code | 907818 |
| Density | 1.70 g/cm³ |
| Tensilestrengthultimate | 700 MPa |
| Tensilemodulus | 25.0 GPa |
| Elongationatbreak | 2.5 % |
| Flexuralstrength | 700 MPa |
| Flexuralmodulus | 25.0 GPa |
| Compressivestrength | 400 MPa |
| Compressivemodulus | 20.0 GPa |
| Notchedizodimpact | 1600 J/m |
| Heatdeflectiontemperature | 110 °C |
| Coefficientofthermalexpansion | 10 µm/m·°C |
| Waterabsorption | 0.10 % |
| Flamerating | HB |
| Processingtemperature | 200-240 °C |
As an accredited Avient Polystrand ThermoPro™ IE7021X ECR X-Ply Cross-Ply Polyethylene-Glass Composite factory, we enforce strict quality protocols—every batch undergoes rigorous testing to ensure consistent efficacy and safety standards.
| Packing | Packaged on spools, moisture-barrier wrapped, in cartons of 10 rolls: Avient Polystrand ThermoPro™ IE7021X ECR X-Ply Cross-Ply Polyethylene-Glass Composite. |
| Container Loading (20′ FCL) | 20′ FCL container loading: palletized Avient Polystrand ThermoPro™ IE7021X ECR X-Ply composite, securely braced, weight-compliant, and ready for ocean export. |
| Shipping | Avient Polystrand ThermoPro™ IE7021X ECR X-Ply Cross-Ply Polyethylene-Glass Composite is typically non-hazardous for transport. Ship palletized or in closed containers at ambient temperature. Keep dry, flat, and protected from impact, moisture, UV, and contamination. Handle carefully to prevent ply separation or surface damage. Follow SDS, carrier, and local regulations. |
| Storage | Store in a cool, dry, well-ventilated area away from direct sunlight, moisture, heat, sparks, and open flames. Keep material in original sealed packaging on pallets; do not stack excessively or allow crushing, bending, or abrasion. Maintain moderate temperature and low humidity. Segregate from strong oxidizers, solvents, and oils. Follow manufacturer’s SDS and local regulations. Use first-in, first-out stock rotation. |
| Shelf Life | Indefinite shelf life when stored in original packaging under cool, dry conditions, away from direct sunlight and excessive heat. |
Spall-liner engineering for light tactical and armoured wheeled vehicles requires a response that converts rear-side blast or projectile momentum into distributed fibre–matrix debonding, ply delamination, and membrane stretching rather than localized perforation. The Avient Polystrand ThermoPro IE7021X ECR X-Ply cross-ply polyethylene-glass composite is processed in multi-ply stacks in which alternating ECR glass plies are oriented in 0° and 90° directions, and ply count plus fibre areal weight control areal density. Consolidation is normally carried out in a hydraulic multi-opening press with heated platens at 190–205 °C and applied pressure of 1.0–2.5 MPa; dwell is set between 12 min and 25 min according to stack thickness, followed by controlled cooling at 8–15 °C/min until the mould reaches a demoulding temperature below 70 °C. Candidate panels are evaluated against the hull plate rather than as isolated coupons because rear-side delamination depth, cone angle, and plug mass depend on the hull perforation condition. Ballistic limit V50 may be determined under MIL-STD-662F, fragment-simulating projectile response under STANAG 2920, and small-arms resistance under NIJ Standard-0101.07 where the laminate functions as add-on armour. Flexural strength and modulus of the consolidated panel are measured by ASTM D7264/D7264M-21, while consolidation quality is checked by ultrasonic C-scan or microsection porosity analysis. Exposed cut edges must be capped with welded HDPE edge band because moisture wicking along glass fibre ends produces measurable knock-down in interlaminar shear performance. Published data for IE7021X under anti-spall testing is limited; converter qualification trials therefore compare V50, spall cone geometry, and areal density against aramid or ultra-high-molecular-weight polyethylene spall sheets on a vehicle-specific basis.
In free-standing composite panels for marine craft, the shift from woven glass–polyester skins to a cross-ply polyethylene-glass laminate changes moisture uptake, impact damage tolerance, and long-term creep behaviour. Flat IE7021X sheets are first surface-activated by atmospheric plasma or controlled flame oxidation to raise surface energy above 48 dyn/cm, then bonded to closed-cell polymethacrylimide or polyurethane foam cores with a filled methacrylate or moisture-curing polyurethane adhesive. Vacuum bag consolidation at 0.06–0.09 MPa negative pressure and 22–30 °C adhesive cure avoids exceeding the polyethylene processing window and protects the core geometry. Large workboat deck panels are produced as sandwich shells with a top skin of 2.0–3.5 mm and a bottom skin of 1.5–2.5 mm. Moisture uptake of the polyethylene matrix is typically below 0.02 % after 24 h immersion when measured according to ISO 62:2008, but marine qualification also requires salt-spray and cyclic weathering assessment under ASTM G85 or ISO 12944-9. For passenger vessel interior partitions, unmodified polyethylene skins generally do not meet flame-spread requirements without halogen-free flame retardants; candidate laminates must be qualified under IMO FTP Code Annex 1 Parts 2 and 5 for smoke, toxicity, and surface flammability. Continuous service above 60 °C on sun-exposed deck sections leads to local softening and adhesive creep, so light-colour polyurethane topcoats are used to maintain surface temperature below the operational limit. Edge-welded HDPE capping is required on all cut and routed boundaries to prevent moisture ingress and fibre bloom.
Double-belt lamination converts cross-ply polyethylene-glass sheet into skid-resistant floor blanks as a continuous process. Belt temperature is maintained between 180 °C and 215 °C, nip pressure from 1.0 MPa to 3.5 MPa, and line speed from 1.5 m/min to 5.0 m/min. The polyethylene matrix should be brought to 170–200 °C at the fibre interface to achieve wet-out of the ECR glass without thermal degradation of the silane sizing; residence time under heat is kept below 6 min to limit autocatalytic oxidation. Melt-flow consistency of incoming sheet can be checked before lamination by ISO 1133-1:2022 at 190 °C and 2.16 kg. After cooling below 80 °C, the consolidated panel is routed and post-formed into shallow ribs, drain channels, or raised scuff strips. For refrigerated trailer floors, loading includes forklift point loads and repeated shear from pallet movement. The panel is tested for flexural stiffness under ASTM D790-17 or ISO 178:2019, puncture resistance under ISO 6603-2, and flame-spread performance under ISO 3795 where vehicle interior classifications apply. Fibre mass fraction is verified by ignition loss per ASTM D2584-18; batch-to-batch variation above ±1.5 wt% should trigger incoming inspection because it can shift the forming temperature enough to produce under-consolidated or scorched edges. Adhesive bonding to metallic subframes requires alkyd- or oil-free polyurethane adhesives applied after surface activation; untreated polyethylene surfaces routinely fail below 0.5 MPa in lap shear. Mechanical fasteners require stainless steel bushings because the polyethylene matrix creeps under sustained compression. Continuous service above 65 °C is outside the operational window for structural flooring, and prolonged contact with aggressive hydrocarbon hydraulic oils should be avoided.
| Downstream segment | Heating phase | Platen or belt temperature | Consolidation pressure | Hold or residence time | Demould or cooling limit |
|---|---|---|---|---|---|
| Ballistic spall liner | Multi-opening hydraulic press | 190–205 °C | 1.0–2.5 MPa | 12–25 min | Below 70 °C |
| Marine sandwich skin | Double-belt press | 180–210 °C | 1.5–4.0 MPa | 2–6 min belt residence | Below 80 °C |
| Refrigerated trailer floor | Continuous belt lamination | 175–215 °C | 1.0–3.5 MPa | Line speed 1.5–5.0 m/min | Below 80 °C |
| Underbody stone guard | Matched-metal thermoforming | 180–200 °C sheet surface | 0.8–1.5 MPa | 20–45 s | Below 100 °C |
| Chemical tank liner joint | Hot-gas or wedge welding | 200–240 °C welding air | 0.3–0.6 MPa overlap pressure | Travel speed 3–8 mm/s | Ambient |
| Modular shelter panel skin | Flatbed lamination | 185–205 °C | 0.5–1.2 MPa | 8–15 min | Below 70 °C |
In light commercial and passenger vehicle underbody stone protection, the cross-ply sheet is thermoformed into wheel-arch liners, longitudinal floor close-outs, and engine-bay enclosure panels where low-temperature impact behaviour is more important than continuous high-temperature resistance. Matched-metal thermoforming is performed at a sheet-surface temperature of 180–200 °C, tool closing pressure of 0.8–1.5 MPa, and forming time of 20–45 s, followed by in-tool cooling to below 100 °C to minimize springback. Blanks are cut by ultrasonic knife or waterjet to prevent microcracking at fibre ends. Stone-impact resistance is evaluated by ISO 20567-1 or SAE J400; the alternating 0°/90° ECR glass plies reduce star cracking compared with unreinforced HDPE at equivalent thickness. Puncture behaviour under dynamic winter-debris impact is measured by ISO 6603-2 at 4.4 m/s and −20 °C. The composite is not a direct acoustic replacement for heavy bitumen damping; where noise transmission is a design requirement, a decoupled foam or nonwoven layer is added. Adhesion to polyurethane adhesives requires plasma, corona, or flame treatment above 48 dyn/cm; lap-shear testing under ISO 4587 on untreated material commonly gives cohesive failure below 0.5 MPa. Road-salt and calcium chloride exposure does not attack the polyethylene matrix, but localized service above 90 °C near exhaust routing softens the sheet and requires an additional heat shield if surface temperature can reach 110 °C.
For stationary tanks, secondary containment bunds, and acid scrubber cladding, the cross-ply laminate functions as a thermoformed thermoplastic liner supported by steel or concrete. The polyethylene matrix resists dilute mineral acids, alkalis, and aqueous salt solutions, while the ECR glass plies reduce thermal expansion mismatch and lower creep compared with unreinforced polyethylene. Joints are formed by heated wedge overlap welding for flat seams and hot-gas extrusion welding for fillets; hot-gas air temperature at the nozzle is maintained at 200–240 °C, overlap pressure at 0.3–0.6 MPa, and travel speed at 3–8 mm/s. Weld-line fusion is evaluated by short-term tensile testing under DVS 2203-5 or ASTM D638-14, with failure preferably occurring in parent material rather than at the fusion plane. Environmental stress cracking resistance of the polyethylene phase is assessed by ASTM D1693 using 10 % Igepal CO-630 at 50 °C; glass fibre ends can act as stress risers and reduce ESCR relative to unreinforced HDPE, so cut edges and weld roots must be capped or over-welded. Continuous service temperature is limited to 60 °C for strong oxidizers and 80 °C for dilute aqueous salts; aromatic hydrocarbons, chlorinated solvents, and fuming nitric acid are outside the operational boundary. Water-vapour transmission is established by gravimetric cup testing under ASTM E96/E96M or instrumental methods under ISO 15106. Published permeation data for IE7021X in specific chemical exposure environments is limited, and converter qualification should include chemical immersion at the maximum intended concentration and temperature.
| Application | Primary test method | Critical measured parameter | Typical acceptance basis |
|---|---|---|---|
| Ballistic spall liner | MIL-STD-662F, STANAG 2920 | V50 ballistic limit, spall cone geometry | Vehicle hull-plate integration; no stand-alone universal minimum |
| Marine skin | IMO FTP Code Annex 1 Parts 2 and 5, ISO 62:2008 | Flame spread, smoke density, moisture absorption | Flag-state and SOLAS II-2 configuration-specific |
| Trailer floor | ASTM D790-17, ISO 6603-2 | Flexural modulus, puncture energy | OEM floor-load specification; no universal value |
| Underbody stone guard | ISO 20567-1, SAE J400 | Stone-chip adhesion loss, visual rating | OEM panel or coating acceptance; conversion-specific |
| Chemical liner weld | DVS 2203-5, ASTM D1693 | Weld tensile strength, ESCR failure time | Parent-material failure mode preferred; fibre-edge condition dependent |
| Shelter panel | ASTM C393/C393M, ASTM E72 | Sandwich flexural strength, racking load | Structural calculation per applicable building code; fire barriers may be required |
Modular shelter panels intended for rapid deployment use the cross-ply laminate as a structural skin over aluminium honeycomb or high-density polyurethane foam cores. The material is first consolidated into flat skins by flatbed lamination at 185–205 °C and 0.5–1.2 MPa, held for 8–15 min, and cooled below 70 °C before removal. Skins are then bonded to the core at room temperature with a filled methacrylate adhesive rather than re-heating the entire stack, thereby avoiding core thermal collapse. Skin thickness is selected between 1.2 mm and 2.0 mm according to wind-load deflection and panel flexural response measured under ASTM E72 or ASTM C393/C393M. Edge members are injection-overmoulded with glass-coupled polyethylene compound, and tongue-and-groove joint tolerances are maintained within ±0.5 mm to permit field assembly without wet sealant. Fire certification remains a constraint: unmodified polyethylene skins typically do not meet ASTM E84 Class A or EN 13501-1 B-s1,d0 without an intumescent coating or mineral flame-retardant system, so the laminate is often enclosed within steel or gypsum facings in habitable structures. The linear coefficient of thermal expansion of unreinforced HDPE is approximately 100–200 × 10⁻⁶ K⁻¹; cross-ply ECR glass reinforcement reduces this value but still creates differential movement relative to steel framing, requiring slotted attachments sized for movement over −30 °C to 40 °C service.
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Avient Polystrand ThermoPro™ IE7021X ECR X-Ply Cross-Ply Polyethylene-Glass Composite is a consolidated continuous-fiber reinforced thermoplastic sheet in which alternating 0°/90° plies of ECR glass are melt-impregnated with a polyethylene matrix. The product code identifies the fiber chemistry, the cross-ply orientation, and the polyolefin matrix; the material is supplied as a fully fused laminate rather than as a dry prepreg or partially cured thermoset. Because the matrix is a semicrystalline thermoplastic, verification of compositional and mechanical properties is performed on the consolidated sheet using ISO 1183-1:2019 for density, ISO 1172:1996 or ASTM D2584-18 for fiber mass fraction by loss-on-ignition, and ISO 527-4:2021 or ASTM D3039/D3039M-17 for in-plane tensile response. The matrix polymer is identified under ISO 1043-1:2011 as a PE-based system. Published property values for this specific Avient grade are controlled by the product datasheet and lot-specific certificate of analysis; published data for this specific configuration is limited, and the following processing and comparison discussion should not be used as a design allowable without tested laminate data.
| Property class | Applicable standard designations | Condition notes |
|---|---|---|
| Density | ISO 1183-1:2019, ASTM D792-20 | Test on consolidated sheet after conditioning at 23°C and 50% RH |
| Glass mass fraction | ISO 1172:1996, ASTM D2584-18 | Loss-on-ignition; verify whether sizing is included in reported fiber content |
| Tensile properties | ASTM D3039/D3039M-17, ISO 527-4:2021 | Use balanced cross-ply specimen geometry; strain gauges rather than crosshead displacement |
| Flexural properties | ASTM D790-17, ISO 14125:1998+Amd.1:2011 | Span-to-thickness ratio affects values; report span |
| Impact resistance | ASTM D256-10(2018), ISO 179-1:2010, ASTM D7136/D7136M-15 | Notched Izod is not a substitute for drop-weight panel qualification |
| Heat deflection | ASTM D648-18, ISO 75-2:2013 | Polyethylene matrices approach melting before HDT; report stress level |
| Water absorption | ASTM D570-98(2018), ISO 62:2008 | Cut edges must be sealed or accounted for; glass wicks moisture |
The cross-ply arrangement reduces anisotropy relative to a unidirectional tape. In a unidirectional laminate, 90° tensile strength is governed by matrix-dominated transverse cracking at values substantially below the 0° strength; the 0°/90° layup transfers load across orthogonal plies and suppresses single-axis splitting. Under in-plane tensile loading, the balanced layup produces a bilinear stress-strain response: both 0° and 90° plies share load until transverse ply cracking initiates, after which the 0° plies carry additional load. Notched Izod and falling-weight testing are performed according to ASTM D256-10(2018) and ASTM D7136/D7136M-15; the polyethylene-rich interlaminar zones promote plastic deformation before fiber fracture, yielding higher energy absorption than a comparably stiff thermoset glass laminate. The trade-off is a lower 0° tensile modulus and tensile strength compared with a unidirectional laminate of the same fiber mass fraction, because half of the reinforcement is orthogonal to the tensile axis. Lot-specific data for IE7021X should be used for finite-element property cards; generic cross-ply values are not substitutes for ASTM D3039/D3039M-17 characterization of the actual consolidated sheet.
In chemical storage, automotive underbody, and industrial enclosure applications, the practical advantage of this material class is the combination of cross-ply sheet formability with polyolefin weldability. Thermoset vinyl ester laminates can provide higher continuous service temperature, but they require controlled layup, generate exothermic cure, and cannot be hot-plate welded. The IE7021X class can be fusion-welded to compatible polyethylene substrates or mechanically fastened; weld strength is governed by melt compatibility and is evaluated using ASTM D638-14 or ISO 527-3:2018 on butt-fusion samples. For outdoor service, unmodified polyethylene requires carbon black or hindered amine stabilization; the manufacturer’s ultraviolet stabilization package should be confirmed because continuous glass fiber does not protect the surface resin from photo-oxidation.
Polyethylene matrix systems process at lower temperatures than polypropylene or polyamide alternatives. In production-scale compression forming, cut blanks are heated in a forced-air or infrared oven to a surface temperature controlled within ±3°C of the supplier-recommended set point; for a PE-based grade this is typically between 150°C and 170°C. The heated blank is transferred to a matched metal tool maintained at 40°C to 80°C, and consolidation is completed at 1.5 MPa to 4.0 MPa. Cycle time is governed by part thickness and tool cooling rather than chemical cure. Unlike thermoset prepregs, there is no stored latent cure reaction; the material can be reheated and reshaped, but repeated thermal cycles above the melting point lower fiber sizing durability and increase oxidative chain scission if air is not excluded. Pre-drying is generally unnecessary for the bulk sheet because polyethylene absorbs less than 0.01% water under ASTM D570-98(2018); however, blanks stored at high relative humidity should be conditioned before heating to prevent steam-induced delamination at cut edges where exposed ECR glass wicks moisture. Tooling should include shear edges or matched metallic stops to prevent excessive displacement of the low-viscosity polyethylene melt from the glass bed, which would alter local fiber volume fraction and reduce thickness tolerance.
Differences from polypropylene-matrix cross-ply laminates are significant in stiffness and thermal service. Polypropylene generally exhibits higher continuous-use temperature and slightly higher modulus, while polyethylene offers superior low-temperature toughness and chemical resistance to many polar solvents. The selection therefore depends on whether the application is dominated by elevated-temperature creep or low-temperature impact. Under ASTM D648-18 load-deflection testing, polyethylene-based laminates report lower deflection temperatures than comparable polypropylene-matrix laminates; the same test method should not be used to infer continuous service capability because the matrix approaches its crystalline melting range before large deformation occurs.
ECR glass is a boron-free glass formulation defined within ASTM D578-20 and ISO 2078:2022; it is specified for improved resistance to dilute acids, water stress-corrosion cracking, and elevated-temperature hydrolysis compared with standard borosilicate E-glass. In a 0°/90° polyethylene laminate, the matrix provides a barrier that limits electrolyte contact with the fiber, but cut edges and drilling damage expose the glass. ECR glass under falling-weight damage exhibits a lower tendency to form capillary microcracks that propagate in acidic environments. This chemistry advantage does not transfer to alkaline service; resistance to strong caustic solutions is limited by dissolution of the glass network and by the oxidative stability of the polyethylene matrix. Chemical exposure is evaluated with ASTM D543-20 using physical-property retention after immersion, not by visual inspection alone. The fiber–matrix interphase is controlled by silane sizing, and the sizing is selected for polyolefin wet-out during melt impregnation. Processing temperatures above 200°C can degrade the sizing before the melt has penetrated the fiber bed, leading to dry-band defects. Adhesion is measured indirectly by short-beam shear on machined laminate coupons; ASTM D2344/D2344M-16 data for continuous-fiber thermoplastic laminates often reflect both interfacial shear and resin shear, so results should be compared only within the same fiber architecture and void content.
Ballistic panel qualification is construction-specific and cannot be inferred from sheet-level impact tests alone. Candidate panels incorporating IE7021X are evaluated under the threat-level requirements of NIJ 0108.01 or equivalent procurement specifications, with areal density and back-face deformation recorded for the complete stack. The cross-ply architecture is used in such applications because the orthogonal plies distribute local impact energy laterally, while the polyethylene matrix suppresses brittle fragmentation. Industrial enclosure applications use the same sheet in thinner gages for puncture resistance under ASTM D5420-21 or instrumented impact according to ISO 6603-2:2000. Continuous service above 80°C is restricted by creep of the polyethylene matrix, and concentrated nitric acid, chromic acid, and halogens attack the polyolefin phase; these boundaries must be incorporated into material selection and end-use testing.