AP/HTPB推进剂凝聚相反应对燃速的影响

作     者：张炜 张仁 

作者机构：国防科技大学 

出 版 物：《航空动力学报》 (Journal of Aerospace Power)

年 卷 期：1991年第6卷第2期

页      面：115-117页

核心收录：

学科分类：080703[工学-动力机械及工程] 082502[工学-航空宇航推进理论与工程] 08[工学] 0807[工学-动力工程及工程热物理] 0825[工学-航空宇航科学与技术] 

主　　题：固体推进剂 凝聚相反应 燃速 

摘      要：The effects of transition metal oxides TMO on the thermal decomposition characteristics of AP and AP/HTPB propellants and on the burning rates of AP/HTPB and AP/Al/HTPB propellants are *** results show that the burning rate of AP/Al/HTPB/TMO propellant depends on the thermo-decomposition characteristics of AP/TMO and burning rate of AP/HTPB/TMO propellant depends on the thermo-decomposition characteristics of *** results also indicate that the aluminum decreases the burning rate of the *** is suggested that the aluminum reduce the rate of condensed phase reactions and the stress effect of AP thermal decomposition properties on the burning rate of aluminized propellant.