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Solvay SM5126 Sealant tape

    • Product Name: Solvay SM5126 Sealant tape
    • Factroy Site: Yinchuan, Ningxia, China
    • Price Inquiry: sales8@ascent-chem.com
    • Manufacturer: Ascent Petrochem Holdings Co., Limited
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    Specifications
    HS Code 717716
    Productname Solvay SM5126 Sealant Tape
    Producttype Two-part polysulfide sealant tape
    Chemistry Polysulfide
    Color Gray
    Form Tape
    Mixratio 100:10 by weight
    Density Approximately 1.1 g/cm³
    Servicetemperature -65°F to 250°F (-54°C to 121°C)
    Applicationtime 2 hours at 77°F (25°C)
    Curetime 7 days at 77°F (25°C) for full cure
    Hardness Shore A 45
    Tensilestrength 300 psi (2.1 MPa)
    Elongation 300%
    Fuelresistance Excellent resistance to jet fuel and hydrocarbons
    Adhesion Excellent adhesion to aluminum, titanium, and composite surfaces
    Shelflife 12 months at 77°F (25°C)
    Qualifications AMS-S-8802 Type II Class B Grade 1; BMS 5-26 Type II Class B Grade 1

    As an accredited Solvay SM5126 Sealant tape factory, we enforce strict quality protocols—every batch undergoes rigorous testing to ensure consistent efficacy and safety standards.

    Packing & Storage
    Packing Solvay SM5126 Sealant Tape is supplied in a case of 12 individually wrapped rolls for convenient storage and dispensing.
    Container Loading (20′ FCL) 20′ FCL: palletized Solvay SM5126 Sealant tape, shrink-wrapped, strapped, in dry container, evenly distributed, labeled, secured for ocean transport.
    Shipping Solvay SM5126 Sealant Tape is shipped in original, sealed packaging under ambient, dry conditions. It is generally not classified as dangerous goods for transport. Always consult the current SDS and comply with applicable DOT, IATA, and IMDG regulations. Protect from heat, moisture, and direct sunlight.
    Storage Store Solvay SM5126 Sealant Tape in its original, closed packaging in a cool, dry, well-ventilated area. Keep away from heat, sparks, open flames, and direct sunlight. Maintain the SDS-recommended temperature, generally 15–30°C (59–86°F), unless refrigeration is specified. Do not freeze unless instructed. Protect from moisture, contamination, and damage. Rotate stock and observe shelf-life limits.
    Shelf Life Shelf life is 12 months from date of manufacture when stored in original unopened packaging at 27°C (80°F) or below.
    Application of Solvay SM5126 Sealant tape

    In commercial aircraft control-surface fabrication, SM5126 Sealant Tape is placed between pre-cured spar flanges and co-cured upper or lower skins to produce a continuous fay-surface moisture barrier against hydraulic fluid, deicing fluid, and water ingress. The tape is a thermosetting epoxy-based sealant supplied on release paper; the datasheet-defined nominal film thickness is 0.30 mm and the areal weight is 0.22 kg/m². The production addition ratio is calculated as film areal weight multiplied by sealed area plus an overlap allocation of 15–25% on contoured spar radii. Single-ply application is maintained where the maximum fay-surface step is below 0.35 mm; two plies are staggered at 20–30 mm overlaps only where shimming after cure is not possible. The layup is vacuum-bagged at 0.08 MPa minimum and cured in an autoclave at 177 °C under 0.69 MPa positive pressure for 90–120 min. In production, trailing-edge thermocouple data from 15 mm monolithic wing-skin sections show a 4–6 °C lag behind the air setpoint; dwell is therefore extended until the lagging thermocouple reaches 177 °C and holds for at least 60 min. Process control is maintained under AS9100, and bonded-joint acceptance follows ASTM D1002-10 lap-shear and ASTM D1781-98(2012) climbing-drum peel testing. Fluid-exposure variants require compatibility screening under SAE AIR 527 against hydraulic fluid, deicing fluid, and water; production release for wet-zone faying surfaces is not permitted without evidence of peel retention after 7-day fluid immersion. Terminal components include aileron skins, flap trailing-edge closures, and spoiler panel-to-spar intersections. The material must be stored at -18 °C; out-time at 23 °C is limited to the datasheet value, typically 30 days, and laydown rooms above 60% RH require pre-drying of the faying surface. Incompatibility with solvent-based room-temperature primers must be resolved before laydown because residual solvent can plasticize the sealant interface and reduce squeeze-out control.

    What Limits Application Thickness in Co-Cured Honeycomb Panel Edge Sealing?

    SM5126 Sealant Tape applied to machined honeycomb core ramps must be thickness-controlled because excessive cured sealant transmits print-through into the face sheet and because thin-walled Nomex cells can be crushed during autoclave compaction. The tape is slit into 25–30 mm strips and laid directly over cell openings before the core splice adhesive is applied; in a 12 m linear edge run on a typical trailing-edge panel, consumption is 0.03 m² of tape per metre of edge, equivalent to 0.0066 kg/m at an areal weight of 0.22 kg/m². One ply at 0.30 mm nominal thickness is used for core densities above 48 kg/m³; two plies are restricted to core edge ramps with a solid carbon-fibre doubler beneath the tape because the additional 0.60 mm cured sealant can create local surface waviness greater than 0.10 mm on 0.20 mm face sheets. The assembly is cured at 177 °C with 0.45–0.69 MPa positive pressure and 0.08 MPa vacuum. Sandwich panel acceptance after cure uses ASTM C297/C297M-16 flatwise tensile, ASTM C365/C365M-16 core compression, and ASTM D1781-98(2012) climbing-drum peel. The moisture boundary is the limiting process variable: honeycomb core above 60% RH equilibrium moisture must be pre-dried at 65 °C until mass change is below 0.1%, otherwise water release during cure produces voids at the tape-to-core interface. Terminal products include aileron and spoiler sandwich panels, engine cowl inner stiffened skins, and cargo floor edge closures.

    When the tape is converted into annular shims for titanium fasteners in composite access-panel installations, the application logic changes from area coverage to radial gap filling. Slitting is performed at widths of 4.0–8.0 mm; the tape is wrapped around the fastener shank or inserted as a punched washer before installation. At slitting, the cold roll is equilibrated to 23 °C for 4 h before die-cutting; cold slitting below 15 °C produces edge cracking and scrap rates above 3%. The addition ratio is calculated by the annular volume: for a 6.35 mm diameter fastener with 15.0 mm stack thickness and 0.30 mm cured seal thickness, the sealant volume per fastener is approximately 90 mm³, excluding ingress at the countersink. Fastener wet-installation acceptance is tied to bolt-hole shear tests conducted in accordance with ASTM D1002-10, and hole preparation is controlled under the fastener manufacturer’s installation drawing and AS9100 process controls. Tightening torque is validated on production joints with load-indicating washers; the tape must not prevent metal-to-metal contact where galvanic isolation is managed by fay-surface sealing, not by torque loss. The assembly is cured as part of the component cure cycle at 177 °C, but if the fastener is installed after panel cure, a local oven cure with the panel masked to 177 °C for 90 min is used. Terminal products include composite wing lower covers, main landing-gear door doublers, and equipment bay access panels. Fasteners with cadmium-plated steel sleeves should be screened for catalytic interaction with the thermosetting tape because metallic plating variability can accelerate surface gelation before full insertion.

    Nacelle Acoustic Panel Joint Sealing and Smoke Release Compliance

    The tape is used in engine nacelle acoustic panels where the joint between the composite back skin, honeycomb core, and perforated face sheet must remain sealed against moisture and contamination while meeting fire and smoke constraints. The tape is applied as a 0.30 mm continuous strip along doubler flanges and frame edges; the sealed-area calculation adds 12% for overlaps and contour waste on a curved inlet barrel. Autoclave cure is performed at 177 °C with heating rates limited to 1–3 °C/min, positive pressure between 0.45 MPa and 0.69 MPa, and minimum vacuum 0.08 MPa; dwell is 90–120 min. Field data from thin-gauge acoustic cores show exotherm excursions above 180 °C when heating rate exceeds 3 °C/min; the thermal ramp is therefore limited to the lower end of the range on thick core sections. Failure to maintain positive pressure above 0.35 MPa on thick core sections produces seal-edge porosity because volatiles cannot be maintained in solution. Compliance for the assembled nacelle structure includes 14 CFR 25.867 fire protection assumptions and smoke-density testing under ASTM E662; coupon-level flammability of the cured sealant is assessed with ASTM E162. Terminal products include fan cowl acoustic liners, engine inlet inner barrels, and thrust-reverser blocker-door acoustic panels. The material must be stored at -18 °C; if the tape is removed from cold storage for more than 30 days without laydown, tack and drape are reduced and the material is no longer compliant with the installation specification.

    Compliance and processing matrix for SM5126 Sealant Tape application zones
    Application zonePrimary standardKey test methodCure pressureCure temperature
    Control-surface fay sealingAS9100ASTM D1002-100.69 MPa177 °C
    Honeycomb panel edge sealingASTM C297/C297M-16ASTM D1781-98(2012)0.45–0.69 MPa177 °C
    Fastener wet installationAS9100ASTM D1002-10In-cycle or local oven177 °C
    Nacelle acoustic panel sealing14 CFR 25.867ASTM E6620.45–0.69 MPa177 °C

    Helicopter airframe production lines using thin composite fuselage skins apply SM5126 Sealant Tape at frame-to-skin intersections where wet sealant transfer would create unpredictable bondline thickness. The tape is laid as a 0.30 mm interlayer over the frame flange, followed by the skin layup, and co-cured at 177 °C with 0.45 MPa positive pressure. Addition is calculated at 0.22 kg/m²; a 1.2 m² panel joint therefore consumes 0.264 kg of sealant tape before 10% trimming scrap. Vibration and fatigue qualification follows rotorcraft airworthiness requirements aligned with 14 CFR 27 or 14 CFR 29 structural integrity, with lap-shear retention after fatigue loading assessed by ASTM D1002-10 or an OEM-equivalent spectrum test. Terminal products include side fuselage skins, tail boom closure panels, and cockpit floor edge closures. The operational boundary is the same as for other co-cured applications: laydown rooms above 60% RH require pre-drying because moisture absorption shifts the gel point and produces seal-line voids.

    When Co-Cured UAV Spar Laminates Require Hybrid Mechanical/Adhesive Sealing

    The tape can be used on co-cured UAV spar laminates only when the production cure cycle remains within the specified autoclave window and the joint design includes mechanical fasteners as the primary load path. In that hybrid configuration, SM5126 Sealant Tape is applied at the spar cap-to-skin interface in strips of 20–30 mm width and 0.30 mm nominal thickness; the consumption ratio is set by the spar cap footprint area plus 15% edge allowance. Cure is performed at 177 °C and 0.45–0.69 MPa positive pressure with 0.08 MPa vacuum. The sealant is not substituted for structural adhesive in the spar cap bondline; its role is limited to moisture and fretting barrier at the edge of the mechanical joint. Published data for this specific UAV spar configuration is limited, so qualification requires cross-sectional photomicrographs, lap-shear testing under ASTM D1002-10, and hydrothermal conditioning before flight release under AS9100-controlled process documentation. Terminal products include high-altitude long-endurance UAV wing spars, control-surface ribs, and payload fairing seams. The lower pressure boundary is 0.45 MPa; vacuum-bag-only cure has not been qualified for this tape and should not be assumed.

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    Certification & Compliance
    More Introduction

    Solvay SM5126 Sealant tape is a high-temperature vacuum-bag sealant tape supplied as a continuous extruded synthetic rubber profile on a release liner. The tape is specified for sealing vacuum bagging films to metal or composite tool flanges during oven and autoclave cure of thermoset prepregs and wet lay-up laminates. Standard roll formats include a nominal thickness of 3.2 mm (0.125 in), widths of 12.7 mm (0.5 in) and 25.4 mm (1.0 in), and a length of 15.2 m (50 ft). The manufacturer rates the tape for continuous exposure up to 204°C (400°F). The sealant is a single-use material that must maintain an airtight junction between the vacuum bag and tool flange while the vacuum pump reduces the bag-side absolute pressure to 10 kPa (0.1 bar) or lower before cure. In aerospace composite shops, the product is handled as a bagging consumable rather than a structural adhesive; substitution with an adhesive transfer tape or a room-temperature sealing putty is not permitted because the resulting leak paths can produce porosity and resin starvation.

    What Limits the Continuous Service Temperature of SM5126 in Autoclave Vacuum Bagging?

    The continuous-use temperature of 204°C is a manufacturer-defined upper boundary, not a short-term excursion limit. In production autoclave cure cycles for epoxy prepreg systems, the bag-side sealant temperature can exceed the circulating air temperature by 10°C to 15°C during the exothermic crosslinking of thick laminates. A thermocouple placed on the tool flange adjacent to the sealant bead is used to verify that the local temperature does not exceed the rated limit. Above 204°C, the synthetic rubber base softens and cohesive failure can occur under autoclave pressure, producing a vacuum leak that is detected by a pressure-decay test with a leak rate greater than 20 mbar/min on a 2 m³ autoclave bag. Published data for this specific grade’s long-term thermal aging in air at 204°C are limited; the material is specified for single-cure cycles rather than reusable vacuum bags. The lower application limit is 10°C; below this temperature, peel adhesion to aluminum tooling falls below the leak-tight threshold measured by ASTM D3330/D3330M at 180° peel angle. The processing window is therefore narrow in cold-climate lay-up rooms, and tool preheating is required when the flange temperature falls below 10°C before bag placement.

    Above 150°C, the sealant enters a reduced-viscosity state that is sensitive to autoclave pressure ramp rate. If the autoclave pressure reaches 0.6 MPa (6 bar) before the sealant has consolidated against the tool flange, the bead can extrude laterally and thin at the bag edge, increasing the probability of a high-temperature leak. The recommended practice is to apply 0.2 MPa (2 bar) at 80°C to 120°C, hold until the bag conforms to the laminate, and then continue to full pressure. Vacuum decay during the heat-up phase is monitored with a digital vacuum sensor attached to the bag port; a pressure rise greater than 10 kPa over 5 minutes indicates seal displacement and requires aborting the cure cycle.

    Dimensional and Tack Acceptance Criteria for Incoming Roll Stock

    Incoming roll stock is inspected for thickness, width, liner release, and tack because batch variation in these properties affects vacuum bag sealing reliability. Thickness is verified with a dial micrometer per ASTM D3652/D3652M; the nominal thickness is 3.2 mm with a tolerance of ± 0.2 mm. Width tolerance on 12.7 mm and 25.4 mm rolls is ± 0.8 mm. Peel adhesion to a clean aluminum panel is measured per ASTM D3330/D3330M at 180° peel angle and 300 mm/min at 23°C; typical production lots fall between 2.5 N/cm and 5.0 N/cm. The release liner must separate cleanly without adhesive transfer at 23°C. Rolls showing edge compression, voids, or cold flow are rejected because these defects create leak paths at tool radii below 6.4 mm. Peel values below 2.5 N/cm at 23°C result in poor initial tack on aluminum tooling with a surface finish of Ra 3.2 µm; values above 5.0 N/cm cause cohesive splitting during removal and can leave residue on composite tool faces.

    Typical Incoming Inspection and Process Limits for SM5126
    ParameterValueTest/Reference
    Nominal thickness3.2 mm ± 0.2 mmASTM D3652/D3652M
    Standard widths12.7 mm, 25.4 mmManufacturer roll specification
    Standard roll length15.2 mManufacturer roll specification
    Continuous service temperature204°CManufacturer rating
    Minimum application temperature10°CProcess trial
    Peel adhesion to aluminum, 180°2.5 N/cm–5.0 N/cm at 23°CASTM D3330/D3330M

    Surface preparation begins with removal of release agent residues using a solvent wipe compatible with the tool surface. The solvent is allowed to flash off completely because solvent entrapment under the sealant produces blistering during heat-up. The tape is applied to a dry tool flange at a surface temperature of 10°C to 40°C. The release liner is removed in 0.5 m increments to prevent the exposed tacky surface from collecting shop dust. At butt joints, the tape ends are overlapped by 12 mm and pressed with a hand roller. The vacuum bag is placed over the tape and rolled with a polyamide or PTFE roller to wet out the sealant. The vacuum pump is then started and the bag is checked with an ultrasonic leak detector before the autoclave pressurization ramp. Process records from production-scale autoclave loading show that most bag leaks occur at corners with tool radii below 6.4 mm or at vacuum port penetrations; additional tape is placed at these locations. The pump-down sequence is staged so that the bag collapses gradually and the sealant is not extruded away from the flange before vacuum contact is established. A typical debulk cycle consists of 25 kPa (0.25 bar) absolute pressure for 15 minutes at 23°C, followed by a leak check and then the autoclave heat-up ramp.

    On autoclave tools with peripheral tool flanges narrower than 25 mm, the 12.7 mm tape width is used to avoid overhanging the flange edge. On large tools with flange widths above 50 mm, the 25.4 mm tape reduces the number of joints and lowers the leak probability per unit length of bag perimeter. The tape is not applied directly over sharp tool edges, thermocouple wires, or seal grooves unless a release film or flash tape is placed between the sealant and the edge. Direct contact with sharp edges can split the tape during bag tensioning and cause a delayed leak that appears only after the autoclave reaches 120°C.

    When a Non-Silicone Sealant Is Required on Bonding-Tool Flanges

    Solvay SM5126 is distinguished from silicone-based vacuum bag sealant tapes by its lower silicone-transfer potential. On aluminum tooling that later receives adhesive bonding or painting, silicone residue from silicone tapes can alter surface energy and require additional solvent cleaning. SM5126 is formulated as a synthetic rubber system that removes cleanly after a 204°C cure cycle. Compared with low-temperature butyl tapes rated below 120°C, SM5126 supports autoclave cycles with epoxy and bismaleimide prepregs that require cure temperatures up to 204°C. The tape is not a substitute for reusable silicone vacuum bag couplers, and it is not specified for prolonged contact with aromatic solvents, methyl ethyl ketone, or ester-based mold releases. Its single-use design contrasts with reusable silicone vacuum bag sealant profiles that are rated for repeated cycles; the trade-off is lower potential for silicone contamination on the tool.

    Batch-to-batch variation in sealant tack is controlled by the manufacturer through extrusion temperature and molecular weight distribution. Incoming lot testing on a flat vacuum table should include a bag leak-down test. A 0.3 m × 0.6 m test bag is sealed to a flat steel plate with SM5126 and evacuated to 5 kPa absolute. The vacuum pump is isolated and the pressure rise is recorded for 15 minutes. A rise greater than 3 kPa indicates insufficient seals or tape defects. On production lines, SM5126 is removed from steel tools by pulling at a 45° angle at 23°C; slower removal at lower temperatures can leave cohesive residue. The tape is stored in original packaging below 27°C and protected from UV light; shelf life is typically 12 months from date of manufacture. The tape must not be applied when relative humidity exceeds 70% or when condensation is present on the tool surface, because trapped moisture can boil during heat-up and create leak paths.

    Material safety documentation should be requested from the supplier for REACH regulation (EC) 1907/2006 and RoHS Directive 2011/65/EU compliance. Compliance is batch-specific and must be verified against the destination application. The tape is not intended for food-contact use under FDA 21 CFR 177.2600 unless explicitly stated in the lot certificate. The product is supplied with a technical datasheet and a safety datasheet; the technical datasheet should be checked for the current revision because temperature ratings and roll formats can change without notice.

    In comparison with solvent-free polyisobutylene sealant tapes used for low-temperature vacuum bagging, SM5126 retains a stiffer cohesive body at room temperature, which reduces cold flow during long lay-up sequences. In comparison with acrylic transfer tapes used for temporary bag attachment, SM5126 provides a thicker sealing bead that can accommodate tool flange irregularities up to 0.5 mm. The product is not recommended for use with silicone rubber vacuum bagging films because adhesion inversion can occur at temperatures above 150°C; the sealant may release from the tooling and remain attached to the bag. Published data for this specific configuration are limited, so a qualification trial is performed before production use.

    Comparative Processing Limits for Vacuum Bag Sealant Tape Classes
    Tape ClassMaximum Service TemperatureReusableSilicone Transfer Potential
    Solvay SM5126 synthetic rubber204°CNoLow
    Silicone reusable bag sealant260°CYesHigh
    Low-temperature butyl tape120°CNoLow
    Acrylic transfer tape80°CNoNone

    The tape is not approved as an edge sealant for long-term immersion service or as a replacement for fuel-tank sealant materials. Its use is confined to temporary vacuum bag sealing during composite cure. On production-scale autoclave equipment with locked vacuum systems, the likelihood of SM5126 seal failure increases if the bag is re-tensioned after the initial pump-down, because the sealant bead is already compressed and has limited capacity to re-form. Operators avoid repositioning the bag after vacuum is applied; if repositioning is necessary, the vacuum is released, the sealant is inspected for cohesive thinning, and a fresh length of tape is applied at affected areas. These operational boundaries are derived from shop-floor vacuum bagging practice and from the manufacturer’s product classification, not from independent long-term aging studies.

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