Gas flow control techniquc of rocket ramjct is discussed,and then some base idea and research achievements in the design of that are also expressed in the paper.

• 对固体火箭冲压发动机燃气流量调节技术进行了论述,阐述了固体火箭冲压发动机燃气流量调节技术在设计上的一些基本思想及研究成果。