GAP贫氧推进剂的常压热分解特性研究

Thermal Decomposition Characteristics of GAP Propellant

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。实验结果表明 ,TMO催化剂对 GAP、AP和 KP的催化作用不同 ,复配催化剂可能是

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. The results show the different catalytical effect of TMOs on the thermal decomposition reactions of GAP, AP and KP. The mixture of some special TMOs is perhaps the best catalyst for the thermal decomposition process of the GAP fuel-rich propellant.