According to a predetermined trajectory, ballistic missile with rocket engine propulsion takes a flight to intended targets under the action of the controlsystem.
弹道导弹是用火箭发动机推进，在控制系统作用下按预定的弹道飞行至预定攻击的目标。
2
The paper presents the composition, functions, technical performance and research of the solid rocket ramjet engine ground test equipment and measurement controlsystem in detail.
介绍了固体火箭冲压发动机地面实验装置及测控系统组成、功能、技术指标和可以开展的研究工作。
3
The practical applications of this controlsystem to the hypergolic bipropellant attitude control rocket engines at 30kg and 100kg thrust levels respectively are stated.