To catalogue

Toray TC420

Toray TC420 is a flow-controlled high temperature cyanate ester resin, toughened to resist microcracking. TC420 is specifically formulated to facilitate production of large out-of-autoclave structures. It can act as a self-adhesive system and is resistant to microcracking. This resin represents a new family of next generation high temperature resins, film adhesives, syntactic paste and expanding foams for ultra-high temperature conditions. TC420 is easy to process, and yields low void laminates with a flexible cure cycle under vacuum-only pressure. This system is also autoclave processable. TC420 is an attractive alternative to bismaleimide (BMI) and polyimide resins.

Properties

Physical Form
Prepreg

Product families

Applications

Automotive & Transportation — Automotive
  • Chassis & Brake
  • Exterior & Body
  • Interior
  • Powertrain & UTH
Industrial — Chemical & Industrial Manufacturing
  • Equipment & Parts
Automotive & Transportation — Transportation
  • Aerospace & Aviation

Product Families

Composite Materials — Prepregs & Molding Compounds
  • Thermoset Prepregs

Other characteristics

End Uses
Motorsport, Radomes, Satellites, Tanks
Functions
Prepreg
Polymer Name
Cyanate Ester Resin
Processing Methods

Out of Autoclave Prepreg, Prepreg Processing, Vacuum Bagging

Markets
  • Automotive & Transportation
  • Industrial
Shelf LIfe
Out Life
21 days at 21°C (70°F) or below and 60% RH or lower
Frozen Storage Life
6 months at -18°C (< 0°F) or below
Out life is the maximum time allowed at the conditions noted before cure, after a single frozen storage cycle in the original unopened packaging at -18°C (0°F) or below for a period not exceeding the frozen storage life noted above.
Product Type

177°C (350°F) Cure Cyanate Ester High Temperature Toughened Cyanate Ester Resin System

Technology
Composite Materials
Composites End Use
  • Motorsport
  • Radomes
  • Satellites
  • Tanks
Material Features
Good Thermal Stability
HIGHLIGHTS

High temperature stability and resistance to microcracking; Capable of 260°C (500°F) extended dry service with short-term capability to 316°C (600°F); Low void content with OOA/VBO cure; Utilizes standard 177°C (350°F) cure temperature with optional freestanding post cure at 232–260°C (450–500°F) to develop full high temperature capability

Recommended Applications
  • Launch
  • Space & Satellite
  • Motorsport & Formula 1
  • Automotive
  • Aerostructures
  • Radome
  • Industrial
  • Heat shields
Composite Materials Functions
Prepreg
Composites Processing Methods
  • Out of Autoclave Prepreg
  • Prepreg Processing
  • Vacuum Bagging

Technical data

Table 1 of 3

3 rows
CharacteristicValueUnit
Poisson’s Ratio0.38—
Shear Modulus1.45 (0.21)Gpa (Msi)
Tensile Modulus3.93 (0.57)Gpa (Msi)

Table 2 of 3

6 rows
CharacteristicValueUnit
Coefficient of Thermal Expansion (CTE) at (500°F ) Post Cure55ppm/°C
Coefficient of Thermal Expansion (CTE) at 177°C (350°F) Cure60ppm/°C
Dry Tg 2 hours (177°C/350°F) Cure176 (349)°C (°F)
Dry Tg After post cure 1 hour (260°C/500°F)348 (658)°C (°F)
Wet Tg 2 hours (177°C/350°F) Cure167 (333)°C (°F)
Wet Tg After post cure 1 hour (232°C/450°F)289 (552)°C (°F)

Table 3 of 3

5 rows
CharacteristicValueUnitMethod
Density at 177°C (350°F) Cure1.22g/cc—
Density at 260°C (500°F ) Post Cure1.2g/cc—
Outgassing (CVCM)max. 0.01%ASTM E595
Outgassing (TML)0.41%ASTM E595
Outgassing (WVR)0.28%ASTM E595

The Omnichem website uses cookies. By continuing to use the site, you consent to their use in accordance with our Privacy Policy and to the collection of analytics.