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Toray Cetex® TC1100

Toray Toray Cetex® TC1100 is a high-end but cost-effective thermoplastic composite material, utilizing a semi-crystalline PPS polymer for excellent mechanical properties and an outstanding chemical and solvent resistance. With over 7 million parts in flight and qualified for structural Applications at Airbus, Boeing, and many other airframe OEMs, Toray Cetex® TC1100 offers a great balance between cost and performance, both mechanical and chemical. The material is inherently flame resistant (< 35/35 OSU) with low smoke emission. Besides Applications in aerospace, Toray Cetex® TC1100 is often the material of choice for demanding industrial Applicationss. Toray Cetex® TC1100 is available as a UD tape, a fabric prepreg, and as reinforced thermoplastic laminates (RTLs) of varying thicknesses. RTLs can be equipped with lightning strike protection, and carbon reinforced RTLs can be supplied with a thin glass top layer to protect a partly metallic assembly against galvanic corrosion. PPS (PolyPhenyleneSulfide) Thermoplastic Resin System.

Product families

Applications

Automotive & Transportation — Transportation
  • Aerospace & Aviation

Product Families

Composite Materials — Prepregs & Molding Compounds
  • Laminates

Other characteristics

Brand
Toray Cetex
Functions
Laminate
Processing Methods
Compression Molding
Markets
Automotive & Transportation
Technology
Composite Materials
Material Features
  • Chemical Resistant
  • Excellent Toughness
  • Flame Retardant
HIGHLIGHTS

Qualified and certified to aerospace OEM specifications; Outstanding performance-to-cost ratio; Service temperature can exceed Tg depending on part design; Lightning strike material as well as galvanic corrosion protection can be incorporated on laminates; Inherently flame retardant; Outstanding chemical and solvent resistance; Indefinite shelf life at ambient temperature storage

Recommended Applications

Aircraft Interiors; Aerostructures; Primary and secondary aircraft structures: wing leading edges, engine pylon structures, clips and cleats for fuselage structure; Aircraft interiors: acoustic structures, structural components of seats, galleys, stowage boxes; High-end industrial Applicationss where corrosive environments, dimensional stability, or vibration dampening play a role

Composite Materials Functions
Laminate
Composites Processing Methods
Compression Molding
Product Safety and Shelf Life
Health and safety information on handling and processing Toray composite materials is described in the Safety Data Sheet available from Toray Advanced Composites.
Out Life
Indefinite at ambient temperature storage
Frozen Storage Life
Not applicable—product does not require freezing

Technical data

Table 1 of 2

3 rows
CharacteristicValueUnit
Glass Transition Temperature (Tg)90 (194)°C (°F)
Tm (melt)280 (536)°C (°F)
Tp (processing)300–330 (570–625)°C (°F)

Table 2 of 2

3 rows
CharacteristicValueUnit
Specific Gravity1.35g/cm³
Specific Gravity84.3—
Density1.35g/cm³

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