| HS Code | 703758 |
| Manufacturer | Saint-Gobain |
| Brand | CHR |
| Product Name | CHR 2995-11R |
| Product Type | Pressure Sensitive Tape |
| Backing Material | Glass-Foil |
| Backing Construction | Glass cloth laminated with aluminum foil |
| Adhesive Type | Silicone |
| Total Thickness | 11 mil |
| Color | Silver/White |
| Temperature Range | -100°F to 500°F |
| Tensile Strength | 100 lb/in |
| Adhesion To Steel | 40 oz/in |
| Elongation | 5% |
| Dielectric Strength | 500 V/mil |
| Width | 1 in |
| Length | 36 yd |
| Core Diameter | 3 in |
As an accredited Saint-Gobain CHR 2995-11R Glass-Foil Backing Silicone Adhesive Pressure Sensitive Tape factory, we enforce strict quality protocols—every batch undergoes rigorous testing to ensure consistent efficacy and safety standards.
| Packing | Packaged as one roll per box, individually wrapped and labeled with product name, quantity, lot number, and handling information. |
| Container Loading (20′ FCL) | 20′ FCL container loaded with palletized Saint-Gobain CHR 2995-11R glass-foil backing silicone pressure-sensitive adhesive tape, securely braced and shrink-wrapped. |
| Shipping | Ship in original sealed packaging in a cool, dry, well-ventilated area. Protect from moisture, heat, sunlight, and physical damage. This tape is typically non-hazardous and not classified as dangerous goods for transport. Follow all applicable local, national, and international shipping regulations. No special labeling or placards are usually required. |
| Storage | Store Saint-Gobain CHR 2995-11R tape in a cool, dry, well-ventilated area away from direct sunlight, heat, sparks, and flames. Keep in original sealed packaging, clean and dry, away from oxidizing agents and incompatible materials. Maintain moderate temperature and humidity; avoid freezing or excessive heat. Protect rolls from crushing and contamination. Rotate stock and follow manufacturer shelf-life recommendations. |
| Shelf Life | Shelf life is typically 12 months from manufacture when stored in original packaging at 21°C (70°F) and 50% relative humidity. |
During restoration of gas-turbine hot-section components, Saint-Gobain CHR 2995-11R glass-foil backing silicone adhesive tape is applied to internal passages and machined surfaces prior to grit blasting under 0.5 MPa alumina pressure and HVOF or plasma deposition of MCrAlY bond coats. The glass-foil backer withstands radiant heat transfer from a Sulzer Metco 9MC plasma torch at standoff distances of 110–140 mm and transient part surface temperatures between 180°C and 220°C. Masking edges are set back 1.5–2.5 mm from the desired coating boundary to create a controlled feather edge at bond-coat termination and prevent step defects that promote oxide breakaway during subsequent yttria-stabilized zirconia topcoat application. The process-equivalent formulation addition ratio is expressed as lineal tape consumption per masked geometry: 1.30–1.80 m of 25 mm-wide tape per 100 mm bore circumference, corresponding to 12–18% surface coverage on an inlet housing. The downstream production sequence includes vapor degreasing, fluorescent penetrant inspection, grit blast, masking, HVOF deposition, tape removal, diffusion heat treatment, and final airflow inspection. Tape removal is completed before vacuum diffusion heat treatment at 1080°C because the silicone adhesive converts to silica ash above 260°C, leaving a non-conductive residue that can alter gas-path surface roughness. Compliance is verified against AMS 2430D for thermal spray masking operations, ASTM D3330/D3330M-22 for peel adhesion retention after 30 min at 220°C, and RoHS 2011/65/EU for outsourced components. End products in this application include turbine blades, nozzle guide vanes, diffuser cases, and fuel nozzle shrouds.
In CFRP prepreg consolidation, the tape serves as a removable edge-dam and release interface between the tool flange and the vacuum bag surface. The glass-foil backing blocks branched epoxy resin flash from migrating into the tool vacuum seal; the silicone PSA separates cleanly because its crosslinked methylphenylsiloxane network exhibits lower peel force after 177°C exposure than acrylic transfer adhesives. The equivalent formulation addition ratio is the flange coverage coefficient: 0.10–0.15 m² of tape per square meter of autoclave tool face, with butt splices at bag edges rather than overlapped splices to avoid double-thickness print-through onto the part surface. Process parameters include layup debulk at 0.2 MPa vacuum, bagging under 0.6 MPa autoclave pressure, ramp at 1.0–2.0°C/min to 177°C, dwell 120–180 min, and cool-down below 60°C before demolding. Tool flanges are inspected by water-break-free testing per ASTM F22-21; any tape residue that survives the cycle is measured by ASTM D3330/D3330M-22 peel separation and must remain below 0.05 N/cm residual adhesion transfer. The silicone PSA is not compatible with free amine curatives that migrate from uncured benzoxazine resin films; side-testing with the specific prepreg system is required before production use. Compliance standards include AS9100D for aerospace tooling operations, ASTM F22-21 for clean-surface verification, and REACH Regulation (EC) No 1907/2006 Article 33 SVHC disclosure. Published data for this specific configuration is limited beyond 190°C; validation on sacrificial tooling is therefore conducted before production runs. End products include autoclave-cured CFRP access panels, spar caps, and radome frames for commercial airframes.
Inside automotive OEM wheel coating cells, the tape is die-cut into seat masks and removed after stoving at 180°C for 15 min; the process-equivalent formulation addition ratio is 1.6 m of 12 mm tape per 19 in wheel face, representing 5% area coverage. Powder application uses electrostatic corona guns at 60–100 kV, and coating adhesion is checked by ASTM D3359-23 cross-cut; compliance anchors are ASTM D3451-21, IATF 16949:2016, and AAMA 2605-20. End products are OEM alloy wheels, suspension knuckles, and battery tray edge seals.
On formed coil lead loops in 5 kV class traction motors, the tape is half-lapped over mica paper and copper lead exits to create a 0.22–0.33 mm final insulation build-up. The half-lap application ratio is 50% overlap, equivalent to 2 passes of backing thickness per spiral wrap, with 25 mm-wide tape applied at 3.2–4.0 m/min linear speed under 18–22 N tension. The glass-foil backing provides tear resistance during subsequent vacuum-pressure impregnation with epoxy or unsaturated polyester varnish in a VPI autoclave at 150°C and 0.4 MPa overpressure. Process sequence includes stator winding, lead brazing, hand taping of phase barriers, VPI impregnation, oven cure at 160°C for 6 h, and insulation resistance testing at 2.5 kV. The silicone PSA maintains tack at -54°C and avoids brittle peeling when coils are handled in cold storage prior to VPI. Compliance is verified against IEC 60454-3-19:2017, UL 510, and IEEE Std 1553 for qualifying insulation in hydro generator windings. End products include traction motors, wound rotors, and industrial generator sets built for Class H thermal operation at 180°C continuous.
In airframe repainting, methylene chloride-free stripper systems based on benzyl alcohol and formic acid remain on the fuselage surface for 8–24 h; butyl rubber and polyester masking tapes swell and lose edge adhesion within the first 45–90 min because the adhesive layer absorbs the organic phase. The silicone adhesive on CHR 2995-11R has lower swell in benzyl alcohol/formic acid media and maintains masking integrity over the dwell window. The glass-foil backing resists the mechanical abrasion of nylon scrapers and high-pressure water rinses at 8–10 MPa. The equivalent formulation addition ratio is expressed as edge-band coverage per fuselage skin panel: 1.10–1.30 m of 75 mm-wide tape per 1 m² of skin surface around windows, static ports, and antenna cutouts, corresponding to 8–11% of the panel area. The production process includes alkaline wash, hand-masking of apertures, brush or airless spray stripper application at 20–40°C, dwell, softened-coating removal with scrapers, neutralization with pH-adjusted rinse water, tape peel, and solvent wipe per ASTM F22-21. Operational boundary: continuous immersion in formic acid at temperatures above 40°C can etch the glass-foil backing and reduce tensile strength; maximum exposure at 35°C is therefore limited to 8 h. Compliance references include SAE AMS 1375D for chemical paint remover compatibility, ASTM D471-16a for swell resistance of elastomeric materials, and REACH Regulation (EC) No 1907/2006 for chemical handling documentation. End products include stripped and repainted fuselage skins, engine nacelle cowls, and ground support equipment panels.
Engine harness assembly benches use the tape as an outer binder over PFA-insulated sensor leads before stainless steel overbraid conduit insertion; the process-equivalent formulation addition ratio is 25 mm spiral pitch on a 3.2 mm cable outer diameter giving 20–25% overlap. Process steps include wire cutting, stripping, crimp termination, resistance check, spiral taping, conduit insertion, and a 22 N maximum pull test; compliance is verified against SAE AS50881F, EN 3197:2014, and RoHS 2011/65/EU. End products include turbine engine harness assemblies, thermocouple leads, and aftertreatment sensor cable segments.
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Saint-Gobain CHR 2995-11R is a glass-foil backing silicone adhesive pressure-sensitive tape supplied in roll form for high-temperature masking, surface protection, and thermal-spray shielding. The backing is a composite of woven glass cloth and aluminum foil, giving the product a reflective, cut-resistant face combined with the dimensional stability of glass reinforcement. Manufacturer-published typical values include a total thickness of 0.18 mm (7.0 mil), a continuous service temperature range from -73°C to 260°C, a peel adhesion to stainless steel of approximately 13.7 N/25 mm (50 oz/in) when tested in accordance with ASTM D3330, and a tensile strength at break of approximately 657 N/25 mm (150 lbf/in) when tested in accordance with ASTM D3759. The silicone adhesive is selected for high-temperature stability and clean removal from metals after thermal exposure, although removal characteristics are substrate-dependent and require process validation.
| Property | Typical Value | Reference Method |
|---|---|---|
| Total thickness | 0.18 mm (7.0 mil) | ASTM D3652 |
| Peel adhesion to stainless steel | 13.7 N/25 mm (50 oz/in) | ASTM D3330 |
| Tensile strength at break | 657 N/25 mm (150 lbf/in) | ASTM D3759 |
| Elongation at break | 5% | ASTM D3759 |
| Continuous service temperature | -73°C to 260°C | Manufacturer data |
| Backing construction | Woven glass cloth laminated to aluminum foil | Manufacturer data |
The aluminum foil face is electrically conductive. The tape is therefore not intended for primary dielectric isolation in high-voltage circuits unless the design explicitly accounts for the conductive foil layer and the potential for short-circuit paths at cut edges. In electrical applications, the product is more commonly used as an abrasion-resistant reflective facing or heat-shielding wrap rather than as a replacement for insulating polyimide or polyester films.
The glass-foil backing of CHR 2995-11R distinguishes it from polyimide/silicone masking tapes in conformability, thermal reflectance, and resistance to grit-blast erosion. Polyimide/silicone tapes typically have a total thickness of 0.06–0.08 mm and an elongation at break above 50%, which permits wrapping around complex contours and maintaining contact on small-radius features. The glass-foil laminate has a lower elongation at break of approximately 5%, meaning it is less conformable around tight radii but substantially more resistant to cut-through and scoring under angular alumina or silicon carbide grit. The foil face reflects a larger fraction of incident radiant load than polyimide film, reducing heat transfer into some masked regions, while the glass cloth layer contributes tensile strength and limits the tearing that can occur in unsupported foil tapes. Peel force after thermal exposure is controlled by the silicone adhesive rather than by the backing, but the laminate construction can influence removal by resisting stretch and by allowing a controlled near-180° peel without tensile deformation of the tape.
| Parameter | CHR 2995-11R glass-foil/silicone | Polyimide/silicone | PTFE-glass/silicone |
|---|---|---|---|
| Total thickness | 0.18 mm typical | 0.06–0.08 mm typical | 0.13–0.18 mm typical |
| Upper continuous temperature | 260°C | 260°C | 260°C |
| Elongation at break | 5% low conformability | ≥50% high conformability | 5–10% moderate conformability |
| Reflective foil face | Present | Absent | Absent |
| Grit-blast cut resistance | High | Low | Moderate |
| Silicone contamination risk | Present | Present | Present |
On plasma spray lines, the tape is applied over dovetail roots, cooling holes, threads, and adjacent zones prior to alumina or yttria-stabilized zirconia deposition. Substrate preparation normally consists of wiping the surface with a low-residue solvent such as isopropanol or a ketone-based cleaner and allowing full evaporation. The tape is burnished with a hand roller or squeegee to minimize air entrapment at the tape edge. Overlapping of tape edges by at least 3 mm is a common process practice to reduce grit intrusion, though the required overlap depends on blast angle, blast pressure, and gun-to-part distance. Masking failures in plasma spray operations are most frequently observed at tape termini that face the gun path, where the adhesive edge is exposed to rebound grit. This failure mode is mitigated by orienting splices away from the line of sight and by inspecting edges after each cycle.
The silicone adhesive system is chosen for its ability to withstand short-duration thermal loads during masking operations. After exposure at elevated temperatures, the adhesive builds adhesion to metal substrates, particularly stainless steels, titanium alloys, and nickel-based superalloys. Removal force increases with temperature and dwell time. When the tape has been exposed at 200°C for 60 min, removal is typically performed at a near-180° peel angle and a controlled peel rate below 300 mm/min to reduce adhesive splitting and foil-to-cloth delamination. These removal parameters are process-sensitive: high peel rates can produce adhesive transfer to the substrate, while very low peel rates may leave degraded backing material at the edge. Quantitative peel-build curves for CHR 2995-11R after extended thermal dwell are not fully published in public literature; removal parameters should therefore be established by trial on the actual substrate and with the actual thermal profile.
Silicone pressure-sensitive adhesives are known to migrate at elevated temperatures and can contaminate surfaces that will later receive wet paint, adhesive bonding, or plasma-enhanced chemical vapor deposition. Areas masked with CHR 2995-11R should be treated as silicone-contaminated until verified clean. Post-removal cleaning may require solvent wiping, plasma treatment, or mechanical abrasion depending on the downstream process. The tape is not recommended for masking components that are sensitive to silicone residues and cannot be cleaned after masking removal.
Autoclave cure cycles for epoxy and bismaleimide composite parts often reach 180°C to 230°C. General-purpose acrylic or rubber-based tapes lose adhesion, soften, or leave carbonaceous residue before these temperatures are reached. CHR 2995-11R is appropriate where a silicone adhesive is required to survive the cure temperature without adhesive breakdown, and where the glass-foil backing provides a barrier to resin bleed and reduces mark-off on tooled surfaces. The tape is applied to composite bagging films, tool plates, or caul plates as a flash breaker or protective edge mask. Because the foil face is nonporous, it can limit resin penetration into the tape edge, although resin flow under pressure may still intrude where the tape is not firmly burnished against the tool surface.
The operational boundary for this product is defined by the silicone adhesive rather than by the glass or foil components. Continuous use above 260°C is not supported by manufacturer-published data. Short excursions above 260°C may be possible in non-loaded conditions, but published data for repeated excursions in this specific configuration are limited. The tape should not be used as a fire barrier or as a substitute for ceramic or metallic shielding when process temperatures exceed the continuous rating by more than 30°C for periods longer than several minutes.
For aircraft interior masking applications, burn compliance may need to be demonstrated under FAR 25.855(a). The user should request test data from Saint-Gobain for the specific product and lot because flammability performance can be affected by adhesive thickness, backing lamination, and contamination. REACH and RoHS status should be verified through Saint-Gobain’s product compliance documentation for the specific lot, since raw-material changes can affect declarations.
Silicone pressure-sensitive adhesives typically exhibit time-dependent adhesion build. Initial adhesion after application is lower than adhesion measured after a 24 h dwell at 23°C and 50% relative humidity. This behavior is relevant when the tape is applied and then immediately exposed to grit blasting or high-temperature cure. Where maximum adhesion is required, the tape should be dwelled for at least 24 h at controlled room temperature before thermal exposure, provided the substrate is clean and dry. Adhesion build is slower on low-energy surfaces such as PTFE, acetal, and some powder-coated surfaces, and the tape may not achieve the published peel values on those substrates.
Storage of CHR 2995-11R should follow standard pressure-sensitive tape handling practices: rolls should be kept in their original packaging at 21°C and 50% relative humidity, protected from ultraviolet light, and not stored near strong oxidizing agents or solvent vapors. Material life is commonly stated by manufacturers as 12 months from date of manufacture when stored under these conditions, but the user should confirm shelf-life requirements against the current Saint-Gobain technical bulletin because product revisions can alter storage classifications. Rolls should be allowed to reach room temperature before application in cold environments because condensation on the adhesive can reduce initial tack and lead to edge lift during subsequent heating.
The tape is not a direct substitute for polyester/silicone masking tapes in low-temperature, low-abrasion operations because the glass-foil backing is stiffer and carries a higher material cost. It is also not a direct substitute for PTFE-glass tapes where a low-friction release surface or chemical barrier is the dominant requirement. Selection between CHR 2995-11R and alternative high-temperature tapes should be based on the specific balance of thermal load, grit erosion, conformability, electrical conductivity, and post-removal surface cleanliness defined by the manufacturing specification.