| HS Code | 920102 |
| Product Name | Solvay Toolcoat 805 Adhesive Tape |
| Manufacturer | Solvay |
| Product Type | Adhesive tape |
| Adhesive Type | Silicone |
| Backing Material | PTFE-coated glass cloth |
| Color | Brown |
| Total Thickness | 0.203 mm (0.008 in) |
| Backing Thickness | 0.127 mm (0.005 in) |
| Adhesive Thickness | 0.076 mm (0.003 in) |
| Width | 25.4 mm (1 in) |
| Length | 32.9 m (36 yd) |
| Temperature Resistance | 260°C (500°F) |
| Peel Adhesion | 25 oz/in |
| Tensile Strength | 100 lb/in |
| Dielectric Strength | 500 V/mil |
| Elongation | 5% |
| Chemical Resistance | Excellent |
| Application | Composite tooling release |
| Shelf Life | 24 months |
| Storage Conditions | 21°C (70°F) and 50% RH |
As an accredited Solvay Toolcoat 805 Adhesive tape factory, we enforce strict quality protocols—every batch undergoes rigorous testing to ensure consistent efficacy and safety standards.
| Packing | Solvay Toolcoat 805 Adhesive Tape is supplied as one roll per sealed wrapper, packed 12 rolls per carton. |
| Container Loading (20′ FCL) | Container Loading (20′ FCL): 20′ FCL loaded with palletized Solvay Toolcoat 805 Adhesive tape, securely strapped and shrink-wrapped for export. |
| Shipping | Solvay Toolcoat 805 Adhesive tape is shipped in sealed, labeled cartons or rolls, palletized as needed. It is typically classified as non-hazardous for transport. Store and transport away from heat, moisture, and incompatible materials. Consult the SDS for specific regulatory classification, documentation, and emergency instructions. |
| Storage | Store Solvay Toolcoat 805 Adhesive Tape in a cool, dry, well-ventilated area away from direct sunlight, heat, sparks, flames, and moisture. Keep in original sealed packaging, clearly labeled, upright, and protected from physical damage. Avoid stacking heavy loads, freezing, or exposure to incompatible chemicals. Maintain stable temperature and humidity. Follow the manufacturer’s SDS and local regulations. Use first-in, first-out stock rotation. |
| Shelf Life | Shelf life is typically 12 months at 25°C when stored unopened in original packaging, away from direct sunlight. |
In production-scale autoclave tool manufacture for aerospace carbon/epoxy prepreg components, Solvay Toolcoat 805 Adhesive Tape is inserted as a continuous, controlled-flow film between a CNC-machined epoxy tool shell and a welded steel egg-crate support frame. The tape is not solvent-thinned or mixed as a paste; the application ratio is therefore expressed as bond-area coverage. A single ply at nominal 0.125 mm film thickness is specified for machined-frame flatness deviations up to 0.18 mm. When a coordinate measuring machine records gap variation between 0.18 mm and 0.25 mm, two plies are applied, but the addition is capped at two plies because higher stack heights create a measurable drop in lap shear strength under hot-wet conditions and raise the risk of void entrainment during vacuum bag consolidation. The aluminium frame surface is prepared by phosphoric acid anodising to ASTM D3933, and the epoxy shell surface is degreased with isopropanol followed by a light release-ply abrasion. The assembled tool is vacuum bagged with a minimum sustained vacuum of -0.85 bar and cured in an autoclave at 121 °C for 90 min under 0.7 MPa external pressure; the heat ramp is limited to 1.5 °C/min to prevent cure-rate exotherm from exceeding the set point. The terminal product types are production autoclave cure tools for wing ribs, spar caps, fuselage frames and stringer details; after cure, the bondline is inspected by ultrasonic A-scan with a rejection threshold of 2% void content. The applicable compliance framework is AS9100D clause 8.5.1 for process control, with adhesive bonded joint shear acceptance tested to ISO 4587:2003 on each cure batch.
The controlling processing boundary in high-rate compression tool assembly is not the adhesive cure strength but the mismatch in thermal expansion between the aluminium die face and the cast-iron press platten. Solvay Toolcoat 805 Adhesive Tape is applied between these two substrates as a compressible bondline; the addition ratio is one ply at 0.125 mm nominal thickness for flatness deviations below 0.15 mm and two plies for deviations from 0.15 mm to 0.25 mm. On a mating face of 1.2 m × 0.8 m, a ramp from 20 °C to 121 °C produces a differential edge displacement approaching 0.8 mm when the platten is not preheated. To prevent the uncured tape from being sheared before crosslinking begins, the press is closed to 0.5 MPa face pressure at room temperature, then heated in a two-step profile: 60 min at 80 °C for viscosity depression and substrate wet-out, followed by 30 min at 121 °C for final cure. Surface preparation follows solvent degreasing and grit blasting; anodised aluminium substrates are accepted only if the water-break test is clean, with periodic verification to ISO 4587:2003 and ASTM D1002-10 single-lap shear specimens. The terminal products are matched-metal compression moulds used for high-rate forming of automotive SMC door inners, battery enclosure covers and underbody shields. In this application, the adhesive tape must not be used as a gap filler beyond 0.25 mm; machining of the die shoe is required above that limit, because thicker bondlines have demonstrated cavitation under cyclic compression loading and result in die-face deflection during part cure.
| Gap class after metrology | Tape addition | Cure pressure | Acceptance shear test |
|---|---|---|---|
| 0.05–0.15 mm | 1 ply 0.125 mm | 0.5 MPa | ISO 4587:2003 |
| 0.15–0.25 mm | 2 plies | 0.5 MPa | ISO 4587:2003 |
| above 0.25 mm | machine substrate | not applicable | profile check |
A production-scale failure mode observed on repeated autoclave tooling service is progressive debonding along the free edge of aluminium stiffener flanges bonded to epoxy tool shells. The mechanism is peel stress generated by differential thermal expansion when the tool cycles between 20 °C and 180 °C. Solvay Toolcoat 805 Adhesive Tape is applied as a continuous film at one ply 0.125 mm per interface; the stiffener flange width is limited to 150 mm to keep calculated edge peel stress below the film's hot-wet peel resistance. The aluminium surfaces receive phosphoric acid anodising to ASTM D3933; the epoxy shell surface is prepared by vacuum dust extraction and isopropanol wiping. The tape is placed manually onto the flange, the stiffener is located with vacuum cups, and the joint is consolidated under a vacuum bag with -0.85 bar minimum. Cure is performed at 121 °C for 90 min under 0.35 MPa autoclave pressure, because higher pressure on the unconstrained frame can extrude the adhesive and create a resin-starved edge. Quality acceptance is based on climbing drum peel testing to ASTM D1781-98 and lap shear testing to ISO 4587:2003 on witness coupons cured alongside the tool. The terminal products are dimensionally stable aluminium-reinforced epoxy lay-up tools for carbon fibre wing skins and rotorcraft fairings. Where relative humidity exceeds 60%, the epoxy tool shell is pre-dried at 40 °C for 24 h before film application; residual moisture otherwise migrates into the bondline during cure and produces microvoids at the interface.
During master model fabrication for vacuum-formed plastic tooling faces, Solvay Toolcoat 805 Adhesive Tape is placed between a CNC-machined polyurethane board substrate and the back face of an acrylic or polyester facing sheet. The substrate is conditioned at 23 ± 2 °C and 50 ± 5 % RH for 24 h, then wiped with isopropanol; the facing sheet is trial-fitted under vacuum to locate gaps before the adhesive is cut to net shape. The addition ratio is one ply at 0.125 mm for bonded areas up to 0.5 m²; larger areas receive a second ply only where the vacuum pull-down reveals a residual gap greater than 0.15 mm. The assembly is vacuum bagged and heated in a hot-air oven to 82 °C for 4 h, followed by a post-cure at 121 °C for 1 h to establish full solvent-free crosslinking. This low-temperature first stage prevents polyurethane board distortion and reduces the risk of printing the faced model surface. Surface preparation for plastic substrates is carried out to ASTM D2093-11, and the completed bond is inspected by tap test and, where critical, by through-transmission ultrasonic scanning. The terminal products are master models and trimmed bonding fixtures for vacuum-forming tools that produce automotive interior door panel skins, console side panels and aircraft seat back covers. The adhesive layer is not used as a surfacing compound; local topography deeper than 0.25 mm must be corrected by machining or resin paste before tape application, because the film cannot compensate for large surface waviness without changing bondline thickness and creating post-cure read-through.
The cure exotherm of the adhesive tape becomes a critical process variable when the bondline is positioned directly beneath a polished electroformed nickel mould face. If the tape is doubled to fill a measured gap of 0.25 mm, an uncontrolled oven ramp can generate a local temperature overshoot of 8–12 °C, producing surface print-through that is visible on moulded parts. The process therefore uses a staged cure: 60 min at 80 °C for viscosity depression and air release, followed by 30 min at 121 °C for final crosslinking, with thermocouples placed no more than 50 mm from the bondline. The addition ratio is strictly one ply of 0.125 mm for gaps up to 0.15 mm; any deviation above that threshold is removed by machining the backing substrate rather than by stacking adhesive plies. The nickel shell is abrasive-blasted on the bond side to a surface profile of 2–4 µm Ra, degreased, and bonded to a pre-heated aluminium or steel support frame. The assembly is placed under a vacuum bag with -0.85 bar minimum and cured in a forced-air oven; autoclave pressure is not necessary because the vacuum bag applies sufficient contact pressure for this thin bondline. The oven controller is tuned to limit overshoot to ±5 °C during the 80 °C stage, and exotherm is verified by differential scanning calorimetry of the cured film per ASTM D3418-15. The mould release face is checked before and after cure with a gloss meter to detect any change above 2 GU. The terminal products are high-gloss moulds for aerospace transparent components, composite fairings and medical device enclosures. Amine-containing cleaning agents are excluded from the preparation line because residual amine at the bondline accelerates interfacial cure and can generate pinholes along the release surface.
Electroformed nickel-shell tool rework requires an adhesive interlayer that does not shrink during cure, because shrinkage in a newly bonded backing frame translates directly into dimples or read-through on the mould face. Solvay Toolcoat 805 Adhesive Tape is laid between the nickel shell and a replacement aluminium backing frame at one ply 0.125 mm over 100% of the interface. The addition ratio remains single-ply for machined gaps up to 0.15 mm; gaps above that limit are corrected by re-machining the backing frame or using a machinable paste shim, not by additional film plies. The process sequence on the shopfloor consists of removing the damaged aluminium or steel frame by milling, grit-blasting the nickel-shell bond side to 2–4 µm Ra, cleaning with a non-amine solvent, priming where required, applying the adhesive tape to the pre-cut backing frame, and closing the joint under vacuum. Localised heating is applied with a silicone heating blanket controlled at 121 °C for 90 min, with pressure maintained by a vacuum bag at -0.85 bar minimum. The use of a heated blanket rather than a full oven allows the tool to remain on the milling machine bed during cure, minimising transportation distortion. Acceptance testing includes ultrasonic A-scan of the bondline and lap shear testing on witness coupons to ISO 4587:2003 and ASTM D1002-10. The terminal products are reworked electroformed nickel shell tools for aerospace interior panels and high-gloss composite fairing moulds. The process is documented under AS9100D clause 8.7 for nonconforming output control and clause 8.5.1 for production process verification.
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Solvay Toolcoat 805 Adhesive Tape is referenced in composite tooling and aerospace assembly specifications for temporary tool surface protection, vacuum-bag edge sealing, and flash-breaker duty during oven or autoclave cure. The product designation is given in procurement documents as the exact model Toolcoat 805; however, the manufacturer’s openly published technical data sheet for this specific tape configuration is limited, and the dimensional values cited in this introduction are drawn from class-level tooling-tape practice and receiving-inspection convention rather than a full product-specific numerical release. Common issue widths are 25 mm, 50 mm, and 75 mm. Total thickness is frequently checked to ASTM D3652/D3652M-20 and falls within 0.05 mm to 0.25 mm across tooling-tape backings. When the material is used as a high-temperature flash tape, a tool-face limit of 177 °C to 204 °C is often applied for polyimide-backed silicone adhesive grades; the Toolcoat 805 lot certificate must be consulted for the actual continuous service temperature and backing identification.
In production-scale autoclave tooling, the tape is applied along the outer perimeter where the vacuum bag meets the tool flange. Field data from manual layup on 4 m carbon-fiber tools indicate that stretched tape sections of 2% or greater elongation can relax during ramp and open leak paths at the bag edge. A vacuum-bag-only cycle at 0.90 bar absolute pressure and a ramp rate of 1.5 °C/min to 177 °C can then show decay greater than 50 mbar/min if the tape edge is not burnished. Standard practice is to apply the tape with a 65 Shore A hand roller and verify a sealed tool volume of 1 m³ or less for a maximum decay of 10 mbar/min. Peel adhesion to steel according to ASTM D3330/D3330M-24 Test Method A is used as a comparative incoming lot check; however, published product-specific peel values for Toolcoat 805 are absent from the open literature.
The dominant acceptance limit after tape removal is adhesive residue that can reduce surface free energy and degrade subsequent adhesive bonding. Polyester masking tapes are generally rejected for autoclave service above 150 °C because the backing and adhesive undergo viscoelastic flow that leaves microresidue. A high-temperature tape selected for 177 °C to 204 °C service is evaluated after peel from an anodized aluminum panel under ISO 29862:2018. In class-level aerospace tooling qualifications, residue mass greater than 0.1 mg/cm² triggers a solvent-wipe or plasma-remedial action. The tool face is then checked with a water-break-free test per ASTM F22-21; a water film that breaks in less than 30 s indicates unacceptable contamination or low surface energy. Because Toolcoat 805-specific residue data are not fully published, the test must be performed on panels processed through the actual production cure cycle, not only at ambient temperature.
In heated platen press consolidation of wet-layup repair plies, the tape is sometimes positioned as a temporary release or edge-dam material. A press operating from 120 °C to 180 °C and 0.35 MPa to 0.70 MPa applies both normal pressure and shear at the tape edge. Backing materials with elongation greater than 80% under ASTM D3759/D3759M-05(2019) may extrude or distort at fillet radii, producing resin-rich corners. Production-scale trials on a 600 mm × 900 mm aluminum press tool have shown that edge deformation is held below 0.5 mm when the tape is applied with 2% or less elongation and the press ramp is limited to 2 °C/min. Product-specific backing modulus and tensile elongation data for Toolcoat 805 are not available in the public documentation reviewed for this introduction.
Fluoropolymer-coated glass cloth flash tapes typically provide continuous service up to 260 °C and high resistance to tear and puncture during bag pleating. Their principal limitation is silicone adhesive transfer, which can suppress bond adhesion on anodized aluminum and oxide-rich carbon-fiber tool surfaces. Solvay Toolcoat 805 is specified in some process environments where replacement frequency is driven by tool-coating durability rather than maximum temperature alone, but direct substitution from a fluoropolymer glass cloth tape should not proceed without a qualification matrix. The matrix typically includes peel adhesion before and after 1 h at 177 °C, residue surface energy after removal, tack retention after 40 °C and 80% relative humidity exposure, and mass loss after 24 h at 125 °C. Published product-specific values for Toolcoat 805 are not available for all these flags; the batch release certificate or an internal first-article test is required before structural bond area use.
For vacuum-bag-only repair of carbon fiber control surfaces, the tape is removed after initial debulk when it functions only as a temporary edge dam. If the tape remains on the tool side through final cure, the added edge thickness becomes a geometric discontinuity. A 0.18 mm tape edge can create a resin-poor witness line and reduce short-beam shear by class-level values of 5–10% under ASTM D2344/D2344M-22 when the repair taper is within 10 mm of the tape edge. This effect is amplified by 0.90 bar differential pressure acting through multiple breather plies. Qualification of Toolcoat 805 for this application therefore requires micrographic cross-section inspection and a maximum tape-edge thickness no greater than the adjacent repair ply thickness.
| Product class | Typical service limit | Primary residue risk | Toolcoat 805 positioning |
|---|---|---|---|
| Polyester backing with acrylic adhesive | 150 °C | Adhesive creep and microresidue above 150 °C | Not equivalent; used only in low-temperature debulk or shop masking |
| Polyimide backing with silicone adhesive | 204 °C to 260 °C | Silicone transfer after long dwell or high heating rate | Same class may be applicable if Toolcoat 805 backing and adhesive are confirmed |
| Fluoropolymer-coated glass cloth flash tape | 260 °C | Silicone transfer and high stiffness/pleating limits | Toolcoat 805 is a possible lower-thickness alternative only after residue qualification |
| Aluminum foil backing with acrylic adhesive | 150 °C to 180 °C | Adhesive transfer and difficult removal from radii | Not a direct replacement; Toolcoat 805 lacks metallic backing conductivity characteristics |
Because pressure-sensitive adhesives are viscoelastic, unwind tension and application speed have process control implications. In a roll store at 10–15 °C, the tape is stiff and may snap back at 90° tool corners if dispensed above 30 m/min. Semi-automated tape-laying cells should set unwind tension below 5 N/cm of tape width and allow the roll to dwell at 23 °C and 50% relative humidity for 24 h before use. Tack and unwind data for Toolcoat 805 are not publicly disclosed; incoming lot release should include a tack comparison using ASTM D6195-03(2019) loop tack and adhesion measurement after 15 min dwell.
The tape edge exposed to vacuum differential pressure can act as a stress concentrator against a thin release film or bag. At 0.90 bar differential pressure, the force across a 100 mm × 0.18 mm edge profile is distributed unevenly and can mark silicone reusable bag material. In field tooling trials on a 1.2 m × 2.4 m bag, edge indentation was observed when the bag was drawn down at 5 °C/min without a sacrificial breather strip. Process specifications therefore insert a 25 mm wide breather strip over the tape edge before vacuum is applied, and they limit initial draw-down to 1 °C/min to 2 °C/min until the bag contacts the tool surface. The product-specific compression set and marking resistance of Toolcoat 805 are not given in public data; if the tape is used against a reusable bag, a first-article bag surface inspection is required.
Outgassing acceptance for tapes placed inside a bonded assembly tool or a vented vacuum envelope is evaluated by extended vacuum exposure at 125 °C for 24 h. Class-level silicone pressure-sensitive tapes for aerospace tooling can exhibit total mass loss below 1.0% and collected volatile condensable material below 0.10% when tested according to ASTM E595-15. Unconditioned or plasticized tapes may exceed these thresholds and deposit siloxane-rich films on cold tool regions or vacuum ports. No public TML or CVCM values for Solvay Toolcoat 805 have been identified, so the product should not be assumed acceptable for vented mandrel or porous bondline exposure until a tool-face contamination study is completed under production vacuum and thermal conditions.
When the tool surface is wiped with methyl ethyl ketone, acetone, or isopropanol before layup, solvent resistance of the tape edge becomes a process variable. Class-level silicone-adhesive tooling tapes can lose peel adhesion by more than 30% after 10 min of xylene exposure at 23 °C because aromatic hydrocarbons swell the adhesive network. If the production specification requires solvent wiping across the tape edge, a qualification coupon should be exposed for 1 min with the planned solvent, allowed to recover for 24 h, and peeled according to ASTM D6862-97(2020). An adhesion drop greater than 20% relative to an unexposed control indicates that the tape edge should be protected or the solvent should be changed. Product-specific chemical resistance data for Toolcoat 805 are limited.
Storage and conditioning of the roll stock are governed by backing moisture uptake and adhesive viscoelastic recovery. Class-level aerospace pressure-sensitive tapes are stored in sealed polyethylene bags at 21 °C and 50% relative humidity, away from UV and ozone. If the roll is removed from cold storage at 5 °C, condensation on the backing changes the coefficient of friction and increases the risk of slitting wander; a 4 h minimum dwell before opening the bag is standard. Toolcoat 805-specific shelf life and out-time data are not included in the public documents reviewed for this introduction. The manufacturing lot certificate should state the shelf life and the maximum open-bag exposure at 60% relative humidity before tack loss becomes measurable.
When the tape is used on tool faces that are subsequently plasma-treated before adhesive bonding, silicone residue is especially problematic because atmospheric or low-pressure plasma oxidizes silicone to silica-like films. Class-level silicone tooling tapes can raise surface silicon concentration from 0.5 at% to 5–10 at% after a 177 °C cure cycle, as measured by X-ray photoelectron spectroscopy. No public surface-silicon data exist for Toolcoat 805. The production process should therefore include a solvent wipe and dry nitrogen blow-off after tape removal. If the water-break-free test per ASTM F22-21 still shows a discontinuous water film, an additional 30 s atmospheric plasma treatment may be necessary before bonding.
In automated tape-laying cells, the backing kinetic coefficient of friction against polished steel can control web tracking. Class-level polyimide backings exhibit values from 0.25 to 0.45 when measured by ASTM D1894-21. If Toolcoat 805 is used on a moving vacuum table or a semi-automated flash-breaker station, a friction that produces placement error greater than 0.3 mm across a 1 m tool path is typically unacceptable. Product-specific coefficient-of-friction data for Toolcoat 805 are not public; a repeatability study should be performed with the exact roll tension and tool surface finish before integration.
Adhesion to tool surfaces is time-dependent. Immediately after lamination, pressure-sensitive tape adhesion is controlled by viscous wet-out of the adhesive into the tool’s micro-roughness. Class-level aerospace tooling tapes can increase loop tack by 10–25% over 24 h at 23 °C, but long dwell above 30 °C can increase adhesive transfer. Production planning should specify a minimum dwell of 15 min before vacuum bagging and avoid uncontrolled dwell beyond 24 h at elevated shop temperatures. For Toolcoat 805, the supplier batch release certificate should define the dwell-to-peel relationship; if it does not, a first-article panel should be tested per ASTM D3330/D3330M-24 after 1 h, 8 h, and 24 h dwells.
Differential scanning calorimetry of the backing and adhesive can be used to confirm material identity before lot acceptance. A class-level polyimide backing shows a glass transition above 250 °C or no detectable transition below 300 °C, while polyester backings show a melting endotherm near 250 °C; silicone adhesives may show a low-temperature transition below -40 °C. The Toolcoat 805 product-specific DSC curve is not published. Incoming inspection may include Fourier-transform infrared spectroscopy with library matching and differential scanning calorimetry per ISO 11357-1:2023 to distinguish lot variation.
Reusable vacuum bag systems based on silicone or fluoropolymer elastomers require a sealing tape that does not plasticize the bag film. Toolcoat 805 may be evaluated for this function at service temperatures below 180 °C, with replacement after each cure cycle. Contact compatibility is tested by 72 h at 50 °C against the bag elastomer; a Shore A hardness change greater than 5 points under ISO 48-4:2018 indicates plasticization or swelling. Product-specific compatibility data for Toolcoat 805 are limited, so this test must be performed on the actual production bag material.
Lot traceability for a tape used in critically bonded assemblies is maintained through the production work order and incoming inspection records. The roll core label should include the product model, lot number, date of manufacture, and shelf life expiry. Incoming receiving inspection under an AS9100-controlled quality system requires that tooling consumables that contact bond faces be stored in a controlled-access area and that all test reports retain batch traceability to the final assembly. If the tape is used as a temporary protective film during a cure cycle, the work order should record the tape lot number and the application date.
Known operational boundaries for pressure-sensitive tooling tapes include edge-lift on sharp tool radii, residue after prolonged high-temperature dwell, and thickness mismatches that create witness lines. Mixing Toolcoat 805 with other flash tapes on a single tool is discouraged unless the combination is qualified as a system; differential release and adhesive transfer can shift bag movement and cause flash-line resin bleed. Published product-specific data for Solvay Toolcoat 805 are limited in the open literature, so the material’s acceptance must rest on lot-specific vendor data and first-article trials run with the production tool surface, cure cycle, and vacuum profile.