燃速调节剂对RDX/AP/HTPB推进剂热分解的影响

利用高压差示扫描量热法（DSC）研究了含不同燃速调节剂（亚铬酸铜、草酸铵、碳纤维）的RDX／AP／HTPB推进剂热分解性能，研究发现，调速剂对推进剂燃速的影响与其对推进剂主要组分（RDX、AP和HTPB）峰温、推进剂初始放热量的影响密切相关，燃烧催化剂亚铬酸铜和碳纤维使RDX，AP的分解峰温降低，使推进剂的初始分解阶段放热量增大，分解放热峰增多，故导致推进剂燃速增加，而草酸铵使RDX的分解峰温升高，使推进剂的初始分解阶段放热量降低，所以导致推进剂燃速降低。

Effect of the burning rate regulator on the thermal behavior of RDX/AP/HTPB propellant

The effects of different burning rate regulators on the thermal behavior of RDX/AP HTPB propellant were studied. The results show the relationship between the effect of the burning rate regulator on the burning rate and that on the thermal behavior of RDX/AP/HTPB propellant is close. The decomposition peak temperature of RDX and AP is decreased, and the first decomposition stage of RDX/AP/HTPB propellant releases more heat, at the same time the number of the decomposition exothermic peak increases because of the affect of CuGr 2O 4 and carbon fiber, so the burning rates of propellant increase. The decomposition peak temperature of RDX becomes higher and the first stage decomposition heat of RDX/AP/HTPB propellant reduces at the effect of the combustion inhibitor (ammonium oxalate), accordingly, the burning rate of propellant containing the combustion inhibitor is lower.