A Global Partner Connecting the Future of Aerospace, SYENSQO
SYENSQO (formerly Solvay) is a global leader in aerospace composite materials. As an reseller, Target Aerospace (TA) goes beyond simple supply; we contribute to innovation in the aerospace industry by providing expert technical support alongside our products.
We are capable of supplying SYENSQOโs aerospace materials not only to the Korean market but also to customers anywhere in the worldโincluding Asia, the Americas, and Europe.
From commercial aircraft and defense to Advanced Air Mobility (AAM), we support the success of your projects with SYENSQOโs proven quality and technology.
Composite and Speciality Materials for Aerospace
Solvay Composite Materials Qualified by NCAMP
Solvay Composite and Speciality Materials for Advanced Air Mobility
Composite Materials for aircraft Propulsion System : Engines and Nacelles
Composites Materials for Space Launch
Composite Tooling
Lightweight composite materials for defense applications
Composite Materials for Automotive Applications
World Leading Portfolio of Composite Materials for Motorsport Applications
SYENSQO/SOLVAY PRODUCTS LIST with SPECIFICATION
| CATEGORY | OEM | SPECIFICATIONS | PART NUMBER | DESCRIPTION |
|---|---|---|---|---|
| Bonding Primer | Boeing | BMS 5-89 | BR 127 | BRยฎ 127 CORROSION INHIBITING EPOXY PRIMER |
| Bonding Primer | MIL-A-25463 | BR 127 | BRยฎ 127 CORROSION INHIBITING EPOXY PRIMER | |
| Bonding Primer | Boeing | BMS 5-89 | BR 127 NC | BRยฎ 127 NC NON-CHROMATED CORROSION INHIBITING PRIMER |
| Bonding Primer | Boeing | BMS 5-89 (NC) | BR 127 NC ESD | BRยฎ 127 NC ESD NON-CHROMATED ELECTRICALLY CONDUCTIVE PRIMER |
| Bonding Primer | BR 179 | BRยฎ 179 NON-CHROMATE BONDING PRIMER (ONE-PART MODIFIED EPOXY) | ||
| Bonding Primer | BR 252 | BRยฎ 252 NON-CHROMATED BONDING PRIMER (ONE-PART MODIFIED EPOXY) | ||
| Bonding Primer | BR 6747-1 | BRยฎ 6747-1 WATER-BASED ADHESIVE BONDING PRIMER (ZERO VOC) | ||
| Bonding Primer | BR 6747-1 NC | BRยฎ 6747-1 NC NON-CHROMATED WATER-BASED BONDING PRIMER | ||
| Film Adhesive โ 250ยฐF Cure | Boeing | BMS 5-101 Ty II Gr 10 | FM 73 | FMยฎ 73 TOUGHENED GENERAL PURPOSE EPOXY FILM ADHESIVE (POLYESTER KNIT CARRIER, BOTH SIDES TACKY) โ 180ยฐF MAX SERVICE |
| Film Adhesive โ 250ยฐF Cure | Boeing | BMS 5-101 Ty II Gr 10 | FM 73M | FMยฎ 73M TOUGHENED EPOXY FILM ADHESIVE (POLYESTER MAT CARRIER, BOTH SIDES TACKY) โ SUPERIOR HANDLING |
| Film Adhesive โ 250ยฐF Cure | Boeing | BMS 5-101 Ty II Gr 10 | FM 73M OST | FMยฎ 73M OST TOUGHENED EPOXY FILM ADHESIVE (MAT CARRIER, ONE SIDE TACKY) โ LARGE AREA BONDING, UP TO 72" WIDTH |
| Film Adhesive โ 250ยฐF Cure | Boeing | BMS 5-101 Ty II Gr 5 | FM 73U | FMยฎ 73U TOUGHENED EPOXY FILM ADHESIVE (UNSUPPORTED) โ HONEYCOMB CORE RETICULATION |
| Film Adhesive โ 250ยฐF Cure | Boeing | BMS 5-101 Ty II Gr 10 | FM 94 | FMยฎ 94 MODIFIED EPOXY FILM ADHESIVE โ HIGH TEMP VERSION OF FMยฎ 73 |
| Film Adhesive โ 250ยฐF Cure | FM 209-1 | FMยฎ 209-1 OUT-OF-AUTOCLAVE STRUCTURAL BONDING FILM ADHESIVE | ||
| Film Adhesive โ 250ยฐF Cure | FM 300-2 | FMยฎ 300-2M DUAL CURE FILM ADHESIVE / SURFACING FILM (250ยฐF CURE VERSION OF FM 300) | ||
| Film Adhesive โ 350ยฐF Cure | Boeing | BMS 5-104 | FM 300 | FMยฎ 300 HIGH SHEAR STRENGTH MODIFIED EPOXY FILM ADHESIVE |
| Film Adhesive โ 350ยฐF Cure | Boeing | BMS 5-104 | FM 300-1 | FMยฎ 300-1 MODIFIED EPOXY FILM ADHESIVE (POLYESTER CARRIER) |
| Film Adhesive โ 350ยฐF Cure | Boeing | BMS 5-137 Ty II Cl I Gr 10 | FM 377S | FMยฎ 377S TOUGHENED EPOXY FILM ADHESIVE โ 350ยฐF (KNIT/SUPPORTED CARRIER) |
| Film Adhesive โ 350ยฐF Cure | Boeing | BMS 5-137 Ty II Cl II Gr 5 | FM 377U | FMยฎ 377U TOUGHENED EPOXY FILM ADHESIVE โ 350ยฐF (UNSUPPORTED) |
| Film Adhesive โ 350ยฐF Cure | Boeing | SMS-116102 Rev E Ty II Gr 10 | FM 377S | FMยฎ 377S TOUGHENED EPOXY FILM ADHESIVE โ 350ยฐF (KNIT/SUPPORTED CARRIER) |
| Film Adhesive โ 350ยฐF Cure | FM 309-1M | FMยฎ 309-1M NEXT GENERATION COMPOSITE BONDING FILM ADHESIVE (MAT CARRIER) | ||
| Film Adhesive โ 350ยฐF Cure | FM 309-1K | FMยฎ 309-1K NEXT GENERATION COMPOSITE BONDING FILM ADHESIVE (KNIT CARRIER) | ||
| Film Adhesive โ 350ยฐF Cure | FM 385 | FMยฎ 385 MODIFIED HIGH TEMPERATURE EPOXY FILM ADHESIVE FOR NACELLE STRUCTURES | ||
| Film Adhesive โ 350ยฐF Cure | Metlbondยฎ 1515-4 | METLBONDยฎ 1515-4 MODIFIED EPOXY FILM ADHESIVE (CO-CURE / CO-BONDING) | ||
| High Temp Film Adhesive (BMI) | FM 450-1 | FMยฎ 450-1 NEXT GENERATION BMI FILM ADHESIVE (MAX SERVICE 450ยฐF / 232ยฐC) | ||
| High Temp Film Adhesive (BMI) | Metlbondยฎ 2550 | METLBONDยฎ 2550 MODIFIED BMI FILM ADHESIVE (OUT-OF-AUTOCLAVE CAPABLE) | ||
| High Temp Film Adhesive (BMI) | Metlbondยฎ 2555 | METLBONDยฎ 2555 MODIFIED CYANATE ESTER FILM ADHESIVE (RADOME / SATELLITE) | ||
| High Temp Film Adhesive (Polyimide) | FM 57 | FMยฎ 57 CONDENSATION POLYIMIDE FILM ADHESIVE (MAX SERVICE 550ยฐF / 287ยฐC) | ||
| High Temp Film Adhesive (Polyimide) | HTยฎ 424 | HTยฎ 424 ALUMINUM-FILLED MODIFIED EPOXY-PHENOLIC FILM ADHESIVE (THERMAL PROTECTION) | ||
| Paste Adhesive | Aeropasteยฎ 1006 | AEROPASTEยฎ 1006 TWO-PART LOW-TEMPERATURE CURING PASTE ADHESIVE (OOA) | ||
| Paste Adhesive | Aeropasteยฎ 1100 | AEROPASTEยฎ 1100 PASTE ADHESIVE FOR HIGH-RATE ASSEMBLY (FAN BLADE LEADING EDGE) | ||
| Paste Adhesive | BRยฎ 4535A | BRยฎ 4535A ALUMINUM-FILLED 100% SOLIDS EPOXY PASTE ADHESIVE (250โ300ยฐF CURE) | ||
| Core Splice Foam | Boeing | BMS 5-90 Ty III Cl I Gr 50 | FM 490A | FMยฎ 490A MODIFIED EPOXY CORE SPLICE ADHESIVE FOAM (350ยฐF MAX SERVICE) |
| Core Splice Foam | FM 490B | FMยฎ 490B MODIFIED EPOXY CORE SPLICE ADHESIVE FOAM | ||
| Core Splice Foam | FM 410-1 | FMยฎ 410-1 MODIFIED EPOXY ADHESIVE FOAM FOR HONEYCOMB SPLICING (AMBIENT PRESSURE) | ||
| Core Splice Foam | FM 6604-1 | FMยฎ 6604-1 MODIFIED BMI CORE SPLICE FOAM (NON-METALLIC CORE SPLICE, 450ยฐF MAX) | ||
| Potting Compound | BR 623P4 | BRยฎ 623P4 ONE-PART EPOXY POTTING / EDGE FILL FOR HONEYCOMB STRUCTURES | ||
| Potting Compound | BR 624 | BRยฎ 624 ONE-PART LOW DENSITY POTTING COMPOUND FOR HONEYCOMB INSERT / EDGE FILL | ||
| Potting Compound | CORFILยฎ 658 | CORFILยฎ 658 EPOXY SYNTACTIC POTTING COMPOUND (AUTOCLAVE CURE, 250ยฐF) | ||
| Potting Compound (BMI) | CORFILยฎ 5250-4 | CORFILยฎ 5250-4 BMI SYNTACTIC POTTING COMPOUND (INSERT POTTING / EDGE FILL, HIGH TEMP) | ||
| Surfacing Film | SurfaceMasterยฎ 905 | SURFACEMASTERยฎ 905 COMPOSITE SURFACING FILM & LIGHTNING STRIKE PROTECTION (ATL COMPATIBLE) | ||
| Surfacing Film | FM 3500EZP | FMยฎ 3500EZP RESIN-IMPREGNATED PEEL PLY (EASY ONE-PIECE REMOVAL, COMPOSITE SURFACE PREP) | ||
| Epoxy Prepreg โ Primary Structure | Boeing / Airbus / Embraer | BMS 8-276 / AIMS 05-01-002 / EMPS 2-0009 | CYCOMยฎ 977-2 | CYCOMยฎ 977-2 TOUGHENED EPOXY PREPREG FOR PRIMARY & SECONDARY STRUCTURES (350ยฐF CURE) |
| Epoxy Prepreg โ Primary Structure | Boeing | BMS 8-276 | CYCOMยฎ 5276-1 | CYCOMยฎ 5276-1 HIGHLY-TOUGHENED EPOXY PREPREG FOR PRIMARY STRUCTURES (350ยฐF CURE) |
| Epoxy Prepreg โ Primary Structure | CYCOMยฎ EP2190 | CYCOMยฎ EP2190 ADVANCED TOUGHENED EPOXY PREPREG FOR PRIMARY STRUCTURES (AFP / ATL CAPABLE) | ||
| Epoxy Prepreg โ Primary Structure | CYCOMยฎ EP2750 | CYCOMยฎ EP2750 TOUGHENED EPOXY PREPREG FOR PRESS CURE (HIGH-VOLUME, COST-EFFECTIVE) | ||
| Epoxy Prepreg โ Primary Structure | CYCOMยฎ 5320-1 | CYCOMยฎ 5320-1 TOUGHENED EPOXY OOA PREPREG FOR PRIMARY STRUCTURES (VBO / OVEN CURE) | ||
| Epoxy Prepreg โ Secondary Structure | CYCOMยฎ 977-3 | CYCOMยฎ 977-3 TOUGHENED EPOXY PREPREG (AUTOCLAVE OR PRESS MOLDING, 350ยฐF CURE) | ||
| Epoxy Prepreg โ Secondary Structure | CYCOMยฎ 970 | CYCOMยฎ 970 EPOXY PREPREG FOR NONPOROUS HONEYCOMB SANDWICH STRUCTURES (350ยฐF CURE) | ||
| Epoxy Prepreg โ Secondary Structure | CYCOMยฎ 2050 | CYCOMยฎ 2050 EXTREMELY TOUGH MEDIUM-TEMPERATURE CURING MODIFIED EPOXY RESIN | ||
| Epoxy Prepreg โ Secondary Structure | CYCOMยฎ 2040 | CYCOMยฎ 2040 VERY TOUGH MODIFIED EPOXY โ HIGH TEMPERATURE PERFORMANCE | ||
| Epoxy Prepreg โ Secondary Structure | CYCOMยฎ 2035 | CYCOMยฎ 2035 VARIABLE CURING MODIFIED EPOXY FOR HIGH PERFORMANCE APPLICATIONS | ||
| Epoxy Prepreg โ General | CYCOMยฎ 114 | CYCOMยฎ 114 UNIDIRECTIONAL GLASS-REINFORCED EPOXY PREPREG (325ยฐF CURE, 250ยฐF SERVICE) | ||
| Epoxy Prepreg (MTMยฎ โ OOA) | MTMยฎ 45-1 | MTMยฎ 45-1 TOUGHENED EPOXY PREPREG FOR PRIMARY & SECONDARY STRUCTURES (OOA / AUTOCLAVE) | ||
| Epoxy Prepreg (MTMยฎ โ OOA) | MTMยฎ 44 | MTMยฎ 44 FLEXIBLE CURING TEMPERATURE TOUGHENED EPOXY (VBO PROCESSING) | ||
| Epoxy Prepreg (MTMยฎ โ OOA) | MTMยฎ 45 | MTMยฎ 45 HIGH PERFORMANCE TOUGHENED EPOXY (VACUUM BAG OR AUTOCLAVE CURE) | ||
| Epoxy Prepreg (MTMยฎ โ OOA) | MTMยฎ 46 | MTMยฎ 46 TOUGHENED EPOXY MATRIX SYSTEM FOR PAYLOAD FAIRINGS AND SPACE STRUCTURES | ||
| Epoxy Prepreg (MTMยฎ โ OOA) | MTMยฎ 49-L | MTMยฎ 49-L TOUGHENED EPOXY OPTIMIZED FOR FAN CASES, ACOUSTIC PANELS, TRENCH FILLERS | ||
| BMI Prepreg | CYCOMยฎ 5250-4 | CYCOMยฎ 5250-4 BMI PREPREG FOR PRIMARY STRUCTURES (SERVICE -75ยฐF TO 400ยฐF) | ||
| BMI Prepreg | CYCOMยฎ 5250-4HT | CYCOMยฎ 5250-4HT BISMALEIMIDE PREPREG โ HIGH TEMPERATURE VARIANT | ||
| RTM / Liquid Resin | PRISMยฎ EP2400 | PRISMยฎ EP2400 HIGHLY TOUGHENED RTM RESIN FOR PRIMARY STRUCTURES (LOW VISCOSITY) | ||
| RTM / Liquid Resin | CYCOMยฎ 890 | CYCOMยฎ 890 RTM RESIN (30-DAY OUTLIFE AT ROOM TEMPERATURE, 350ยฐF CURE) | ||
| RTM / Liquid Resin | CYCOMยฎ PR 520 | CYCOMยฎ PR 520 HIGHLY TOUGHENED RTM RESIN (350ยฐF CURE) | ||
| RTM / Liquid Resin | CYCOMยฎ PR 520N | CYCOMยฎ PR 520N RTM RESIN FOR FAN BLADES, CASES, NOSE CONES (HIGH TOUGHNESS) | ||
| RTM / Liquid Resin (BMI) | CYCOMยฎ 5250-4 RTM | CYCOMยฎ 5250-4 BMI RTM RESIN FOR PRIMARY STRUCTURES (SERVICE UP TO 400ยฐF) | ||
| Phenolic Prepreg โ Interior | CYCOMยฎ 2265 | CYCOMยฎ 2265 SELF-ADHESIVE PHENOLIC PREPREG FOR AIRCRAFT INTERIORS (PRESS / MOP CURE) | ||
| Phenolic Prepreg โ Interior | CYCOMยฎ 6070 | CYCOMยฎ 6070 RAPID-CURE PHENOLIC (STOW BINS, SIDE WALLS, CEILING PANELS) | ||
| Phenolic Prepreg โ Interior | CYCOMยฎ 2400-1 | CYCOMยฎ 2400-1 SELF-ADHESIVE PHENOLIC FOR COMPLEX DRAPEABLE PARTS (PRESS / AUTOCLAVE) | ||
| Phenolic Prepreg โ Interior | L-591 | L-591 GENERAL PURPOSE PHENOLIC FOR AIRCRAFT INTERIORS (PRESS / AUTOCLAVE CURE) | ||
| Phenolic Prepreg โ Ducting | L-728 | L-728 AIRTIGHT REINFORCED PHENOLIC FOR ENVIRONMENTAL CONTROL SYSTEM DUCTING | ||
| Phenolic Prepreg โ Interior | CPHยฎ 2280/7576 | CPHยฎ 2280/7576 HIGH TEMPERATURE LOW FREE PHENOL PHENOLIC RESIN ON GLASS FABRIC | ||
| Phenolic Prepreg โ Interior | CAยฎ 6304 | CAยฎ 6304 ELASTOMER MODIFIED PHENOLIC RESIN ON 1583 STYLE GLASS FABRIC (HIGH TEMP) | ||
| Phenolic Prepreg โ Ablative | MIL-R-9299 | MXG 175 | MXG 175 PLAIN WEAVE GRAPHITE CLOTH WITH MIL-R-9299 PHENOLIC RESIN (CARBON FILLER) | |
| Polyimide Prepreg | AVIMIDยฎ S | AVIMIDยฎ S NON-MDA ADDITION TYPE POLYIMIDE (WET SERVICE 550ยฐF / DRY SERVICE 630ยฐF) | ||
| Cyanate Ester Prepreg | CYCOMยฎ 5575-2 | CYCOMยฎ 5575-2 MODIFIED CYANATE ESTER โ HIGH TEMP, LOW DIELECTRIC (RADOME) | ||
| Cyanate Ester Prepreg | CYCOMยฎ 5577-1 | CYCOMยฎ 5577-1 VBO CAPABLE LOW FLOW MODIFIED CYANATE ESTER (RADOME / ANTENNA) | ||
| Thermoplastic Composite (APC) | Airbus / Bell / Dassault | Airbus A320, A400M; F-18; F-22; Dassault Rafale qualified | APC-2 PEEK | APC-2 PEEK THERMOPLASTIC COMPOSITE TAPE (AS4 12K CARBON FIBER / PEEK MATRIX) |
| Thermoplastic Composite (APC) | Airbus / Bell / Leonardo | AW101 / Airbus A320 qualified | APC PEKK-FC | APC PEKK-FC THERMOPLASTIC COMPOSITE TAPE (AS4D 12K / PEKK MATRIX) |
| Specialty Polymer โ PEEK | Boeing | BMS (Multiple grades โ lot-specific testing required) | KetaSpireยฎ KT-880 NT | KETASPIREยฎ PEEK KT-880 NT (STRUCTURAL BRACKETS, FASTENERS, WEAR COMPONENTS) |
| Specialty Polymer โ PEEK | Boeing | BMS Ty III | KetaSpireยฎ PEEK (Various) | KETASPIREยฎ PEEK โ GENERAL GRADES (BUSHINGS, HEAT SHIELDS, HYDRAULIC COMPONENTS) |
| Specialty Polymer โ PAEK | Boeing | BMS (AvaSpire grades) | AvaSpireยฎ PAEK (Various) | AVASPIREยฎ PAEK โ BOEING-APPROVED GRADES (STRUCTURAL AEROSPACE COMPONENTS) |
| Specialty Polymer โ PAI | Torlonยฎ PAI | TORLONยฎ PAI POLYAMIDE-IMIDE โ HIGHEST PERFORMING MELT-PROCESSABLE THERMOPLASTIC | ||
| Specialty Polymer โ PPS | Rytonยฎ PPS | RYTONยฎ PPS POLYPHENYLENE SULFIDE โ STRUCTURAL COMPONENTS, CHEMICAL RESISTANCE | ||
| Ablative Material | MX 4926N | MX 4926N ABLATIVE MATERIAL โ EXCELLENT DIMENSIONAL STABILITY AT HIGH TEMPERATURES | ||
| Ablative Material | MIL-R-9299 | FM-5504 | FM-5504 HIGH-PURITY SILICA-REINFORCED PREPREG (SHORT-TERM INSULATION 3000โ4000ยฐF) | |
| Space / Launch โ Epoxy Prepreg | CYCOMยฎ 950-1 | CYCOMยฎ 950-1 250ยฐF CURING EPOXY WITH 350ยฐF PERFORMANCE (AUTOCLAVE / OVEN VBO, SPACE) | ||
| Space / Launch โ Epoxy Prepreg | CYCOMยฎ 1908 | CYCOMยฎ 1908 EPOXY TOWPREG FOR ROCKET MOTOR CASE WINDING & THICK-WALL COMPOSITES | ||
| Space / Launch โ Epoxy Prepreg | CYCOMยฎ 1908-6 | CYCOMยฎ 1908-6 RESIN-IMPREGNATED CARBON FIBER TOW (PRESSURE VESSELS / ROCKET MOTOR CASES) | ||
| Space / Launch โ Film Adhesive | FMยฎ 309-1 | FMยฎ 309-1 NEXT-GENERATION FILM ADHESIVE FOR LAUNCH VEHICLE PRIMARY STRUCTURES (HIGH Tg 360ยฐF) | ||
| Composite Bonding Technology | FusePlyโข 350 | FUSEPLYโข 350 COMPOSITE BONDING TECHNOLOGY (COVALENT BONDING, ELIMINATES RIVETS/FASTENERS) | ||
| Composite Bonding Technology | FusePlyโข 250 | FUSEPLYโข 250 COMPOSITE BONDING TECHNOLOGY (250ยฐF CURE, OOA CAPABLE) |