| HS Code | 877704 |
| Manufacturer | Rogers Corporation |
| Product Name | MOX-TAPE T2040 |
| Part Number | T2040-B004-12 |
| Color | Black |
| Material | Silicone rubber |
| Tape Type | Self-fusing |
| Width | 1.00 in (25.4 mm) |
| Length | 12 ft (3.66 m) |
| Thickness | 0.020 in (0.51 mm) |
| Operating Temperature Minimum | -54 °C (-65 °F) |
| Operating Temperature Maximum | 204 °C (400 °F) |
| Dielectric Strength | 400 V/mil (15.7 kV/mm) |
| Tensile Strength | 700 psi (4.8 MPa) |
| Elongation At Break | 300% |
| Dielectric Constant | 2.8 at 1 MHz |
| Volume Resistivity | 1 x 10^14 ohm-cm |
| Durometer | 60 Shore A |
| Water Absorption | 0.1% |
As an accredited Rogers Corporation MOX-TAPE T2040-B004-12 Self-fusing tape factory, we enforce strict quality protocols—every batch undergoes rigorous testing to ensure consistent efficacy and safety standards.
| Packing | MOX-TAPE T2040-B004-12 is packaged as 12 rolls per case; each self-fusing tape roll is 0.5 inch wide and 36 feet long. |
| Container Loading (20′ FCL) | Loading Rogers Corporation MOX-TAPE T2040-B004-12 self-fusing tape into a 20′ FCL container, securely palletized, braced, and protected for ocean transport. |
| Shipping | Rogers Corporation MOX-TAPE T2040-B004-12 Self-fusing tape is not classified as hazardous for transport by DOT, IATA, IMDG, or ADR. Ship in original packaging, keep dry, avoid extreme temperatures, and label with product ID, lot, and quantity. No UN number, hazard class, or packing group required. Follow SDS guidance. |
| Storage | Store Rogers Corporation MOX-TAPE T2040-B004-12 in a cool, dry, well-ventilated area away from direct sunlight, heat, sparks, flames, and incompatible materials. Keep original packaging tightly closed. Maintain moderate temperature, typically 15–30°C, and low humidity. Protect from dust, moisture, solvents, ozone, and physical damage. Do not store near food or beverages. Follow local regulations and manufacturer instructions. |
| Shelf Life | Shelf life is 12 months from manufacture when stored unopened in original packaging at room temperature, away from sunlight and moisture. |
In airframe harness fabrication, Rogers Corporation MOX-TAPE T2040-B004-12 is incorporated as an adhesive-free fused silicone overwrap at wire branch-outs, engine sensor lead transitions, and pylon feeder splices. Compliance for the resulting assembly is assessed under MIL-I-46852 for self-fusing silicone insulating tape, SAE AS50881 for aerospace wiring harness routing and support, and ASTM D4388-20 for electrical-grade rubber tape properties. The downstream formulation addition ratio is 0 wt% adhesive; the tape constitutes 100 wt% of the fused elastomeric layer. A half-lapped spiral with 50% overlap produces 2 continuous silicone layers over the original cable jacket. The downstream production process begins with cleaning the wire jacket using 99% isopropanol and warming the work surface to 20–25°C. The tape is applied under hand or spindle-winder tension until its width decreases by 10–15%; this controlled elongation initiates interfacial polymer interdiffusion and eliminates detectable ply boundaries within 24 h at 23°C. Finished product types include engine fan-case sensor lead assemblies, wing-root harness branch-outs, pressurization-system cable transitions, and p-clamp isolation wraps. In production-scale harness shops, incomplete interfacial fusion has been observed when the tape is stored below 5°C before application; pre-warming the roll to 25°C restores ply-to-ply cohesion. Wrapping over silicone oils or uncured RTV is not recommended because residual plasticizer and cure by-products can retard fusion.
The processing window for heat-trace cable outer jacket repair narrows when ambient temperature falls below 10°C because silicone self-fusion becomes progressively slower while the underlying cable jacket remains rigid. Compliance follows IEEE 515-2017 for resistance trace heating systems and IEC/IEEE 60079-30-1:2015 where the repaired cable may remain in a hazardous location. The addition ratio in the repair area is 50% tape overlap, yielding 2 half-lapped layers; this increases to 3 half-lapped layers at cable-to-connector interfaces and splice entries. Process control requires the cable jacket surface to be preheated with a hot-air tool to 25–35°C and the roll to be conditioned at 20–30°C for 12 h before wrapping. The installer winds from the cable entry toward the termination with constant spiral tension sufficient to produce 10–20% width reduction, then reverses the helical direction for each subsequent layer to reduce leak paths. Terminal product types include self-regulating electric heat-trace cable splice kits, junction box entry seals, thermostat sensor lead repairs, and flange heating element terminations. Below -20°C, published field data for reliable self-fusion of silicone tape joints is limited; supplemental mechanical clamping or a heated enclosure is recommended. The tape is not intended to replace primary conductor insulation or termination glands in wet-service heat-trace circuits.
For subsea control umbilical and offshore topside cable-splice sealing, the T2040-B004-12 tape is applied over solvent-cleaned cable jackets and metal connector backshells where pressure-sensitive adhesive tapes lose adhesion under long-term saltwater exposure and temperature cycling. Compliance is verified under IEC 60092-354:2020 for marine cable insulation and IEEE 1580-2020 for shipboard propulsion and control cables; material-level characterization references ASTM D4388-20 and dielectric strength per ASTM D149-20. The formulation addition ratio is 0% adhesive and 100% fused silicone. The repair zone receives 3 half-lapped layers applied at 50% overlap, with the first layer directly on the cable jacket and subsequent layers reversed in helix direction. In offshore maintenance operations, the splice bay is enclosed to maintain 55–65% relative humidity because condensation on the cable jacket reduces initial surface contact. Technicians clean the jacket with 99% isopropanol, lightly abrade the outer cable surface with 120-grit emery cloth where mechanical keying is required, and apply a first tensioned wrap with width reduction of 15%. Interlayer fusion is considered complete after 24–72 h at 20–25°C; dielectric megger testing at 500 V DC is performed after 72 h. Terminal product types include subsea pump motor lead splices, ROV tether repair sleeves, topside lighting transformer cable connections, and offshore instrument branch cables. Direct immersion without a mechanical outer jacket is outside standard practice; published data for this specific configuration is limited.
| Application environment | Primary standard designation | Overlap geometry | Process control limit |
|---|---|---|---|
| Airframe harness splice | MIL-I-46852 | 50% lapped; 2 layers | 20–25°C work surface |
| Heat-trace cable repair | IEEE 515-2017 | 50% lapped; 3 layers at terminations | 25–35°C preheat |
| Offshore cable splice | IEC 60092-354:2020 | 50% lapped; 3 reversed layers | 55–65% relative humidity |
| High-voltage motor lead | IEEE 43-2013 | 50% lapped; 4 layers at step-down | 10–15% width reduction |
Generator and form-wound motor lead connections in mining and primary metals processing are overwrapped with the T2040-B004-12 tape to fill irregular lug geometries without adhesive voids. Compliance is tied to IEC 60034-1:2022 for rotating electrical machine insulation and IEEE 43-2013 for insulation resistance testing. Material-level validation references ASTM D149-20 for dielectric breakdown and UL 94 V-0 for flammability in ventilated enclosures. The addition ratio is 100% tape at 50% lapped coverage, giving 2 fused layers over field-approved stress-control mastic; at cable lug joints, 4 half-lapped layers are used to bridge the step-down from busbar to cable. The downstream production process removes oxide layers from the copper lug with a non-chlorinated contact cleaner, dries the surface, and applies a thin stress-control mastic before tape winding. A hand-tensioning spindle or slow-speed winding fixture maintains width reduction at 10–15%; razor cuts are made at a 30–45° angle to prevent square-edge lift. Final assemblies are subjected to 1 kV DC 10-min insulation resistance tests in the coil shop. Terminal product types include 460 V and 6.6 kV motor lead extensions, generator terminal box connections, and cable-to-busbar transition sleeves. Amine-based RTV coatings applied immediately before wrapping are incompatible because residual amine or acetic acid can create interfacial haze and retard self-fusion.
In electric vehicle battery busbar and motor inverter harness fabrication, polyimide tapes may develop edge lift and loss of dielectric integrity under repeated thermal cycling; the T2040-B004-12 tape is substituted as a fused silicone overwrap where repetitive exposure to 150°C is required. Compliance for the downstream harness is evaluated under IEC 62660-1:2018 for secondary lithium-ion cell performance and SAE J1742 for high-temperature automotive connection durability. Volume resistivity of the fused layer is verified using ASTM D257-14. The application addition ratio is 50% overlap, yielding 2 fused layers on straight busbar sections; tight bend radii receive 3 half-lapped layers to compensate for thinning during elongation. The production process uses semi-automatic spiral winding equipment with adjustable elongation rollers rather than conventional adhesive-tape heads because self-fusion requires sustained circumferential tension and a degree of tape width reduction. Wrapped subassemblies are held at 23°C and 50% relative humidity for 24 h before dielectric testing. Terminal product types include high-voltage busbar assemblies, motor inverter phase lead connectors, and battery service disconnect harnesses. The tape should not be used as the sole insulation at potentials above 600 V without additional dielectric testing because void formation at tight bends can reduce partial discharge resistance.
Chemical processing vessels with immersion heaters require jacketing repair that resists silicone oil, steam, and moderate acid exposure; the tape is applied over damaged fluoropolymer cable jackets after degreasing and lockout-tagout isolation. Compliance follows ASTM D4388-20 for electrical insulating rubber tape, IEC 60502-1:2021 for low-voltage cable construction, and ASTM D471-16a for fluid resistance of the fused elastomer. The formulation addition ratio is 50% overlap with 3 half-lapped layers over the damaged zone, each layer wound in the opposing helical direction to prevent straight-line moisture ingress. The downstream production process de-energizes the circuit, abrades the fluoropolymer cable jacket with 240-grit aluminum oxide paper to create mechanical keying, and cleans the surface with 99% isopropanol before wrapping. Each wrap is tensioned until the tape width reduces by 10–15%; the completed repair is held at 25°C for 24 h before re-energization. Terminal product types include polytetrafluoroethylene-insulated immersion heater cable assemblies, thermocouple lead transitions, and liquid-level sensor cable entries. Continuous immersion in ketone-containing process streams is not recommended without an outer polytetrafluoroethylene wrap or mechanical boot; published data for this exact chemical exposure configuration is limited.
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Rogers Corporation MOX-TAPE T2040-B004-12 is classified as a self-fusing, self-amalgamating silicone elastomer tape supplied without a pressure-sensitive adhesive. The product is intended for electrical insulation, environmental sealing, and mechanical protection of cable splices, harness breakouts, and connector backshell geometries. Interlayer adhesion develops through siloxane chain interdiffusion when the tape is overlapped onto itself under controlled wrapping tension. A fully fused wrap forms a homogeneous, void-free silicone jacket that does not leave an adhesive residue on the substrate or on adjacent braided sleeving.
The T2040-B004-12 designation is manufacturer-specific. Published data for this exact suffix configuration is limited in open industrial sources; the base MOX-TAPE family is offered in unsupported silicone tape form with thickness and width increments that must be verified against the certified drawing or lot-specific certificate of conformance. The suffix should not be decoded as a simple thickness or width statement without consulting Rogers Corporation because the B004 and 12 segments may encode internal batch, liner, or slitting identifiers.
Silicone self-fusing tape is typically calendered onto a release liner to prevent blocking during storage and handling. The material is preferably stored in sealed polyethylene packaging below 30°C and protected from ultraviolet exposure, because extended UV exposure can promote surface oxidation that reduces interlayer tack. Shelf-life control is application-specific. Procurement specifications often require verification of fusion performance on a representative mandrel before releasing the material to the production floor, rather than relying solely on date-code age.
Unlike adhesive-backed PVC or polyester tapes, the product does not develop peel adhesion to the substrate. Initial holding strength on vertical or overhead surfaces depends entirely on wrapping tension and interlayer contact area. Substrates contaminated with silicone oil, hydrocarbon grease, or plasticizer migrating from plasticized PVC can act as interlayer release films. Solvent wiping with 99% isopropanol or another volatile aliphatic cleaner is common before wrapping, but the surface must be fully dry before the tape is applied. Residual solvent films can become trapped under the wrap and reduce the interlayer diffusion rate.
Compatibility with soft PVC insulation is limited because plasticizer migration can soften the overlying wrap and create a weak boundary layer. When the tape is applied over PVC-insulated conductors in rail or transit applications, a short compatibility trial at maximum operating temperature is advised. Rogers Corporation can supply regulatory declarations for REACH and RoHS status for the T2040-B004-12 configuration, but the absence of lead, cadmium, mercury, hexavalent chromium, and selected phthalates should be confirmed through the supplier compliance certificate rather than inferred from the base polymer.
In connector boot sealing, the wrap functions as an environmental barrier and strain-relief cushion, not as a structural adhesive or a waterproof connector boot. Low-pressure splash and condensation environments can be addressed with multiple layers of T2040-B004-12; pressurized fluid ingress or immersion service requires an overboot or potting compound because unfused edges and overlapped seams can transmit fluid at pressure. Rework is straightforward: a single longitudinal cut permits the fused wrap to be removed as a resilient monolith, leaving no adhesive residue. However, unsupported silicone has low cut-through resistance. In abrasion zones the silicone wrap is placed beneath braided polyester or aramid sleeving rather than used as the outermost sacrificial layer.
Interlayer fusion is controlled by surface contact and chain mobility. Silicone elastomers are nonpolar and have low surface energy; any contamination layer with lower surface energy or weak boundary properties can prevent siloxane interdiffusion. Production harness shops have observed delamination when operators handled the tape with gloves contaminated by fluoropolymer release sprays or when wrapping was performed over residual wire-drawing lubricants. Cleaning before wrapping must remove ionic contamination as well as organic films, because trapped ions can initiate electrochemical corrosion at connector metal surfaces when moisture penetrates an unfused overlap. This failure mechanism is accelerated under salt-fog exposure.
Fusion kinetics are temperature-dependent. Self-fusing silicone tapes of this class generally develop handling strength within minutes but require 24 to 72 h at 23°C ± 2°C for maximum interlayer strength. At surface temperatures below 5°C, chain mobility is reduced, and fusion time extends. Moderate warming to 40–60°C can accelerate fusion. But forced thermal cycling before full fusion may induce interlaminar shear stress at the overlapped edges because the inner and outer layers respond differently to thermal expansion. Condensation films from high-humidity handling above 60% RH also retard initial tack. Production controls often include wrapping in a conditioned area and delaying subsequent tube or sleeve installation until the wrap has stabilized.
Electrical testing of self-fusing tape is preferably performed on a fused wrap rather than on a single ply. Single-layer dielectric breakdown values to ASTM D149-97a(2013) may not predict the performance of a spirally wrapped harness, because the overlap geometry creates a repeating region of twice the nominal wall thickness and a potential capillary path at each seam. Partial discharge and insulation resistance measurements to ASTM D257-14 are therefore applied to mandrel-wrapped test pieces after a defined fusion period. Volume resistivity above 1 × 1015 ohm-cm is characteristic of unfilled silicone elastomers used in electrical tape compounds, but product-specific data for T2040-B004-12 should be taken from the manufacturer’s certified datasheet.
Thermal cycling reveals differences in linear coefficient of thermal expansion between the silicone wrap, copper conductors, and polymer wire insulation. A silicone wrap that is tightly applied at room temperature can develop loosening at high temperature because the silicone expands more than the copper substrate. If the wrap is not fully fused, thermal movement promotes seam opening and contaminant ingress. Fully interlayer-fused tape reduces this risk by creating a monolithic tube with hoop stress distribution rather than a series of independent layers. Accelerated thermal cycling to SAE AS22759 or customer-specific profile can be used to evaluate seam integrity before production release. In some harness designs, a light overstress wrap is used to compensate for thermal expansion differences.
Below -40°C, the retained elongation of silicone is useful in applications subject to vibration. PVC and polyester tapes can embrittle at these temperatures and crack along bundle flex points. The low-temperature flexibility of self-fusing silicone is related to its siloxane backbone, which retains segmental motion at temperatures where hydrocarbon or vinyl polymers stiffen. However, low-temperature flexibility does not improve cut-through resistance; cold environments with ice accumulation and sharp-edge contact still require an overwrap.
Heat-shrink tubing requires installation before the connector is terminated or must be expanded and recovered over the termination, which can be impossible on large backshells and breakout tees. Self-fusing tape can be applied after final assembly and over irregular geometries without heat recovery. Adhesive-lined heat-shrink provides a high-strength moisture seal and strain relief, but it is rigid after recovery and cannot be removed without cutting. Self-fusing silicone, by contrast, can be removed and rewrapped during rework. However, adhesive-lined heat-shrink generally exceeds self-fusing tape in fluid pressure resistance and mechanical resistance. The two products are often used together: heat-shrink boot as primary environmental barrier and self-fusing tape as filler or edge sealing.
Self-adhesive silicone tapes contain a pressure-sensitive silicone adhesive that provides immediate peel adhesion to substrates. They are easier to apply on vertical or overhead installations because the adhesive holds the tape in place before overwrap. However, the adhesive interlayer is a separate phase with different permeability and thermal stability. In humid and thermally cycled environments, loss of adhesion at the adhesive-substrate interface can create ingress paths. Self-fusing tape eliminates that interface once full fusion is achieved but demands higher operator skill. If fusion is incomplete, the self-fusing product can be less forgiving than adhesive-backed silicone because it has no adhesive to maintain temporary positioning.
Skived PTFE tape offers high temperature resistance and very low surface energy, but it does not fuse to itself and cannot form a continuous watertight wrap on complex shapes. PTFE tape is used as a release layer or as a low-friction overwrap, not as an environmental seal. Glass cloth and polyimide tapes provide better cut-through and abrasion resistance than unsupported silicone but introduce adhesives and higher stiffness. The self-fusing silicone product occupies a middle position: it provides conformable electrical insulation and sealing but is not an outer armor layer.
Fusion deficiency is not always visible during final inspection. A more reliable approach is to wrap a witness sample on a polished metal mandrel and then slit the wrap longitudinally after the specified fusion period. If the overlap seam peels apart with minimal force, the lot is rejected or the process is adjusted. Mechanical property measurements can be performed to ASTM D412-16 for tensile strength and elongation, ASTM D2240-15 for durometer, and ASTM D570-98(2018) for water absorption. These tests provide release-lot trend data but do not directly measure interlayer fusion. Fusion-specific testing is usually a mandrel wrap plus peel or burst test because standards for adhesive tapes assume pressure-sensitive adhesive, which is absent from this product.
| Property | Method | Failure indicator |
|---|---|---|
| Dielectric breakdown | ASTM D149-97a(2013) | Premature breakdown at unfused seam |
| Insulation resistance | ASTM D257-14 | Resistance drop after humidity exposure |
| Tensile and elongation | ASTM D412-16 | Loss of elongation after heat aging |
| Durometer | ASTM D2240-15 | Hardening after UV/ozone exposure |
| Water absorption | ASTM D570-98(2018) | Mass gain above manufacturer limit |
Production application of unsupported self-fusing silicone tape requires controlled tension to avoid necking and premature tearing. Manual wrapping on 25 mm wide tape is often conducted with back-tension between 2 N and 5 N; automated spiral wrapping stations use closed-loop dancer control to maintain constant tension across changing bundle diameters. Recommended overlap in harness shops is typically 50% to 67%, producing a nominal double-wall thickness at the overlap. Overlap below 33% can yield gaps under bending; overlap above 75% can increase bundle diameter without improving fusion integrity.
On automated wrapping stations, variations in bundle diameter across a harness can cause tension spikes if the dancer arm response is too slow. A tension spike above 8 N on thin unsupported silicone can create a transverse tear that may not be visible until after fusion. Pre-production setup records should include tape spool brake torque, dancer air pressure, and wrap speed. Production operators should also stagger the start and finish overlaps by at least 30 mm around the bundle circumference to prevent a single seam line from running parallel to the cable axis.
When termination of the wrap is required, the tail is preferably pressed into the underlying layer with a short overlap of at least 10 mm. Because there is no adhesive, a short tail with low residual tension can lift and create an ingress path. After the tail is pressed down, the wrap should not be disturbed until the fusion period has elapsed. In production, movable tags or temporary markers should not be attached over uncured seams.
The absence of adhesive simplifies rework and extends service life in high-humidity electrical enclosures. Adhesive-backed tapes can lose peel strength as plasticizers migrate or as adhesive systems hydrolyze; self-fusing silicone does not rely on adhesive bond to the substrate. However, the product cannot provide structural support for loose connector accessories or act as a substitute for mechanical strain relief. It is installed over a mechanically secured junction and overwrapped or potted where abrasion or fluid pressure exceed the capability of unsupported silicone. At elevated service temperatures above 200°C, the user should validate the exact T2040-B004-12 compound because published data for this specific configuration is limited.