首页 | 本学科首页   官方微博 | 高级检索  
     检索      

空间对接机构技术及其研制
引用本文:陈宝东,唐平.空间对接机构技术及其研制[J].上海航天,2005,22(5):6-8,61.
作者姓名:陈宝东  唐平
作者单位:上海宇航系统工程研究所,上海,201108
摘    要:给出了空间对接机构的传动缓冲、捕获、连接密封、结构与附件,以及控制等子系统的组成和功能,阐述了对接和分离基本过程。以及其中的备份操作。分析了对接机构的总体设计、动力学仿真、部件研制和地面试验等关键技术。

关 键 词:载人航天工程  对接机构  总体设计  动力学仿真  部件研制  地面试验
文章编号:1006-1630(2005)05-0006-03
收稿时间:2005-10-10
修稿时间:2005-10-10

The Technology Development of Docking Mechanism System
CHEN Bao-dong,TANG Ping.The Technology Development of Docking Mechanism System[J].Aerospace Shanghai,2005,22(5):6-8,61.
Authors:CHEN Bao-dong  TANG Ping
Institution:Aerospace System Engineering Shanghai, Shanghai 201108, China
Abstract:The composition and function of driving buffer, capture, joint and sealing, structure and fix, and control subsystems in docking mechanism system were put forward in this paper. The general process of docking and separation and backup measures in operation were also described. The key technologies such as system design, dynamic simulation, parts development and ground test were analyzed.
Keywords:Manned spaceflight engineering  Docking mechanism system  System design  Dynamic simulation  Parts development  Ground test
本文献已被 CNKI 维普 万方数据 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号