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1£©With the development of space technology, in particular the spacecraft and payload flight speed and quality than structure of the enhanced high-temperature advanced composite materials is becoming a major aerospace structures and new materials, particularly resistant to high temperature above 400 ¡æ of composite materials, the Matrix resin must have a very good high temperature performance and high-temperature resins such as the commonly used BMI, polyimide resin has been unable to meet the actual requirements.
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2£©Epoxy resin is a type of excellent performance of the polymer resin, but with its large number of epoxy groups, cross-linked when cured density, and therefore fragile, and poor heat resistance. As a result, we will be the synthesis of quaternary amine monomer used in curing the Epoxy resin, such as the use of non-temperature scanning calorimetry (DSC) technology quaternary amine curing of epoxy resin and had a follow-up, and to achieve the curing power Parameters. In recent years, the thermoplastic resin used to toughened epoxy resin with a view to raising the temperature, to improve its fragile.
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