空间交会对接技术

doi:10.3969/j.issn.0253-9608.2011.06.001

自然杂志 ›› 2011, Vol. 33 ›› Issue (6): 311-314.doi: 10.3969/j.issn.0253-9608.2011.06.001

• 特约专稿 • 下一篇

空间交会对接技术

郑永煌

研究员，发射场系统副总设计师，中国酒泉卫星发射中心，兰州 732750

收稿日期:2011-11-05 修回日期:2011-11-15 出版日期:2011-12-25 发布日期:2011-12-25

Rendezvous and Docking Technology for Space Flight

ZHENG Yong-huang

Researcher，Launch Site System assistant General Designer, Jiuquan Satellite Launch Center, Lanzhou 732750, China

Received:2011-11-05 Revised:2011-11-15 Online:2011-12-25 Published:2011-12-25

摘要/Abstract

摘要： 空间交会对接是载人航天工程非常重要的基本技术。在介绍空间交会对接技术发展历史和中国首次交会对接取得圆满成功的基础上，阐述了空间交会对接技术的基本概念、技术难点、控制方式和交会对接过程，并着重介绍了四种交会对接机构的特点。最后介绍了中国首次交会对接任务规划、天宫一号目标飞行器和神舟八号飞船的特点以及两次空间交会对接过程。

关键词: 交会对接, 对接机构, 天宫一号, 神舟八号

Abstract: Rendezvous and Docking is a very important basic technology of Manned Space Engineering. Firstly, rendezvous and docking technology development history is provided, and the significance of China first rendezvous and docking success is presented.Secondly, the basic conception, technology difficulty, control mode and docking process of rendezvous and docking technology are explained. Thirdly, four docking mechanism characteristics are special provided. Finally, China first rendezvous and docking mission planning,characteristic of Tiangong-1 target flight vehicle and Shenzhou-8 spacecraft and two rendezvous and docking successes are presented.

郑永煌. 空间交会对接技术[J]. 自然杂志, 2011, 33(6): 311-314.

ZHENG Yong-huang. Rendezvous and Docking Technology for Space Flight[J]. Chinese Journal of Nature, 2011, 33(6): 311-314.

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https://www.nature.shu.edu.cn/CN/Y2011/V33/I6/311

空间交会对接技术

Rendezvous and Docking Technology for Space Flight

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