调节固体推进剂高压下燃烧性能是该研究领域的难题之一。传统的催化剂在中低压区间能很好地调节其燃烧性能，但难以使固体推进剂在高压区呈现平台燃烧。本课题创新性的提出了"高压平台燃烧含能催化剂"，不仅可以实现燃烧催化剂能量化，而且能够在高压区较好地调节固体推进剂的燃烧性能，使其在高压区出现平台燃烧。主要开展高压平台燃烧含能催化剂的设计、构筑及表征，对该类化合物的合成反应进行热力学研究，为该类化合物的制备提供依据；进行TG-DSC-MS联动研究，确定其分解气相产物，得到其对固体推进剂主要组分RDX和NC在高压下的催化热分解参数和其本征热分解动力方程；找出催化性能较好的化合物，揭示其在高压区的作用机理，这对于高能、高燃速固体推进剂的发展具有重要的理论意义和应用价值。

Modifying the combustion performance of the solid propellant is one difficult problem at high pressure. Traditional catalyst can well modify the combustion performance in middle-low pressure range, but it is very difficult to make solid propellant to realize plateau combustion in high pressure. Energetic combustion catalyst of high pressure plateau was creatively proposed, which can give it some energetic, and also adjust the combustion performance in high pressure and make it plateau combustion. The design, construction and characterization of energetic combustion catalysts are carried out, and study the thermodynamics of the reaction to provide support for the production design of the compounds. Research the thermal decomposition by TG-DSC-MS simultaneous techniques to determine the gaseous products of decomposition of the compounds, and get the parameters and kinetic equation of thermal decomposition of RDX/NC main ingredients of the solid propellant catalyzed by the compounds. Better compounds are found, and catalysis combustion mechanism is proposed. Which has the important theoretical meaning and practical value for the development of high energy and high burning rate solid propellant.