In order to know combustion process of hybrid rocket,pyrolysis test of solid fuel was carried out by using hot-plate heat conduction mode,then chemical kinetic parameters of solid fuel were obtained.

• 为了认清固液火箭发动机混合燃烧过程,采用热平板导热方式对固体燃料进行热分解实验,得到了固体燃料的化学动力学参数。