The thermal decomposition characteristics of GAP simulated low oxygen fuel rich propellant were studied by using DSC method. The effect of TMO catalysts on the thermal decomposition characteristics is investigated in this paper.

• 采用 DSC方法研究了 GAP模拟贫氧推进剂的常压热分解特性 ,同时考察了 TMO催化剂对 GAP模拟贫氧推进剂热分解特性的影响。