摘要
介绍了我国神舟八号飞船和天宫一号目标飞行器对接试验的对接机构分系统的组成、控制时序、设计方案,以及可靠性与安全性。给出了对接机构分系统研制中总体设计、动力学仿真、试验和关键部件研制等关键技术,以及整机特性测试、连接分离试验、热真空对接与分离试验、寿命试验等验证情况。回顾了对接机构分系统的研制过程。
The composition, control scheduling, design, and reliability and safety of the docking subsystem of China＇s Shenzhou-8 spaceship and Tiangong-1 target spacecraft were introduced in this paper. The key technologies of the general design, dynamic simulation, test and important part design in the design of the docking subsystem were given out. The tests, such as the general characteristic test, docking and separating test, docking test system in thermal vacuum, and life test, and test results were presented briefly. The whole research phase of the docking subsystem was reviewed.
出处
《上海航天》
2011年第6期1-6,共6页
Aerospace Shanghai
基金
上海市科学技术委员会资助(10XD1422900)
