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Toray EX-1522

Toray EX-1522 is a high performance toughened modified epoxy resin system. The material displays both excellent mechanical and thermal properties, in addition to very low moisture absorption. EX-1522 has a flammability rating of V-0, which lends itself to usage in low flammability Applicationss. EX-1522’s ideal electrical properties make it a lower cost option for radome, antennas, and other critical electrical Applicationss. Finally, EX-1522 is an outstanding resin selection for use where self-adhesion to honeycomb without the use of a film adhesive is desirable. This resin bonds to honeycomb under vacuum or pressure cure and displays cohesive honeycomb failure during destructive testing. 177°C (350°F) Cure* Toughened Epoxy Resin System

Properties

Physical Form
Prepreg

Product families

Applications

Automotive & Transportation — Transportation
  • Aerospace & Aviation

Product Families

Composite Materials — Prepregs & Molding Compounds
  • Thermoset Prepregs

Other characteristics

Functions
Prepreg
Polymer Name
Epoxy Resins & Compounds
Processing Methods
Compression Molding
Markets
Automotive & Transportation
Shelf LIfe
Out Life
21 days at ≤ 21°C (70°F) and ≤ 60% RH
Frozen Storage Life
12 months at ≤ 18°C (0°F)
Out life is the maximum time allowed at ≤ 21°C (70°F) and ≤ 60% RH before cure, after a single frozen storage cycle in the original unopened packaging at ≤ -18°C (0°F) for a period not exceeding the frozen storage life noted above. * May be cured at 121°C (250°F) or 150°C (300°F)
Technology
Composite Materials
Material Features
  • Flame Retardant
  • Good Mechanical Properties
  • Low Water Absorption
HIGHLIGHTS

Robust processing under vacuum, autoclave, or press; Low dielectric and loss tangent for radome Applicationss; Low flammability, V-0; Self-adhesive to core; Lower cost vs. cyanate ester resins; Low outgassing for space/satellite Applicationss

Recommended Applications
  • Space & Satellite
  • Aerostructures
  • Radome
  • antennas
  • Reflectors
  • Low observables
  • Radar transparent structures
Composite Materials Functions
Prepreg
Composites Processing Methods
Compression Molding

Technical data

Table 1 of 3

2 rows
CharacteristicValueUnit
Tensile Modulus4 (0.58)Gpa (Msi)
Tensile Strength66.2 (9.6)MPa (Ksi)

Table 2 of 3

7 rows
CharacteristicValueUnit
Coefficient of Thermal Expansion (CTE)88 (49)ppm/°C (ppm/°F)
Dry Tg with 121°C/250°F cure126 (259)°C (°F)
Dry Tg with 149°C/300°F cure169 (336)°C (°F)
Dry Tg with 177°C/350°F cure180 (356)°C (°F)
Wet Tg with 121°C/250°F cure123 (253)°C (°F)
Wet Tg with 149°C/300°F cure159 (318)°C (°F)
Wet Tg with 177°C/350°F cure166 (331)°C (°F)

Table 3 of 3

10 rows
CharacteristicValueUnitMethod
Density1.36–1.46g/cc—
Dielectric Constant at 10 GHz2.8——
FlammabilityV-0——
JP4 Fuel Resistance No effect after 30 days25 (77)°C (°F)—
Loss Tangent at 10 GHz0.008——
Moisture Absorption at saturation after 100 hr water boil1.2%—
Outgassing (CVCM)0.01%ASTM E 595
Outgassing (TML)0.28%ASTM E 595
Outgassing (TML-WVR)0.12%ASTM E 595
Outgassing (WVR)0.16%ASTM E 595

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