前言 从一九七五年开始到一九七九年底,北京航空学院、沈阳一一一厂设计所同八四五厂科研一所协作,对含铝固体贫氧推进剂先后做过点火试验,发生器地面试验和火箭——冲压组合发动机连管试验。通过这些地面试验,对含铝固体贫氧推进剂的燃烧有了一些初步的认识。本文是针对试验中发生的一些问题进行初步的总结,并提出一些看法。 Foreword From 1975 to the end of 1979, the Beijing Institute of Aeronautics and Astronautics, the 111th Shenyang Plant Design Institute, in collaboration with the No. 845 Research Institute, conducted an ignition test on aluminum-containing solid oxygen-poor propellant, Generator ground test and rocket - ram combination engine tube test. Through these ground tests, some preliminary understanding of the combustion of aluminum-bearing solid oxygen-poor propellant has been made. This article is a preliminary summary of some problems occurred in the experiment and put forward some views.