High temperature resistance TG350℃; high transparency and low dielectric; cyanate ester quartz prepreg：

It is a special modified cyanate ester resin system, which can be formulated at 130℃ and cured at 150 to 220 degrees, with a TG point (DMA method) of 350 degrees Celsius. It has a high degree of cure and extremely low absorption rate, low internal stress, and few micro cracks; it also has low vacuum mass loss, dielectric constant, and loss angle tangent. It has good compatibility with quartz fiber can be used to manufacture and produce satellite secondary load-bearing or non-load-bearing components and antenna domes. 

High temperature resistance TG200℃; high transparency and low dielectric; cyanate ester quartz prepreg：

It is a specially modified cyanate ester resin system that can be formulated at 130°C and cured at 50 to 220C, with a TG point (DMA method) of 180-200°C. It features high curing, extremely low absorption, low internal stress, and minimal microcr; simultaneously, it has low vacuum mass loss, a low dielectric constant, and a low loss tangent. Due to its excellent compatibility with quartz fibers, it can be used to manufacture and produce satellite load-bearing or non-load-bearing components as well as antenna radomes.

Cyanate ester carbon fiber prepreg：

High-end thermoset prepreg with continuous carbon fiber (unidirectional UD / plain / twill fabric) as the reinforcement substrate, impregnated with pure modified cyanate ester resin, double-sided covered with release film, and stored at low temperature. During curing, the cyanate ester undergoes cyclotrimerization to form a dense triazine ring cross-linked network, combining the ultra-high modulus of carbon fiber with the four core advantages of cyanate ester: low dielectric constant, high temperature resistance, low outgassing, and extremely low moisture absorption. It is a specialized material for support structures in aerospace, satellites, and high-frequency radar.