探月三期月地高速再入返回飞行器技术设计与实现  

Technique design and realization of the circumlunar return and reentry spacecraft of 3rd phase of Chinese lunar exploration program

作　　者：杨孟飞[1] 张高[2] 张伍[2] 彭兢[2] 王勇[3] 王晓磊[3] 陈春亮[2] 杜颖[2] 张正峰[2] 

机构地区：[1]中国空间技术研究院,北京100094 [2]北京空间飞行器总体设计部,北京100094 [3]北京控制工程研究所,北京100190

出　　处：《中国科学：技术科学》2015年第2期111-123,共13页Scientia Sinica(Technologica)

基　　金：国家中长期科技发展规划重大专项资助项目

摘　　要：探月三期月地高速再入返回任务是我国首个深空探测再入返回任务,研制目的是突破和掌握月地高速再入返回关键技术,为嫦娥五号任务研制奠定基础.本文给出了月地高速再入返回飞行器的任务特点,进行了任务概貌和研制过程介绍,阐述了双平台和多目标飞行器方案设计及飞行过程设计情况,并给出了在轨飞行结果.结果表明,月地高速再入返回飞行器所有功能性能均满足任务要求,在轨飞行状态正常,技术设计正确可行.The circumlunar return and reentry spacecraft of 3rd phase of Chinese lunar exploration program is the first deep space reentry mission of China. The purpose of the mission is to break through the key technique of moon-earth hyper speed reentry, and lay foundations of the Chang＇E-5 probe. This report introduces the characteristics, overiew and development history of the mission, gives a Comprehensive to the double-platform and multi-target scheme, on-orbit procedure, and presents on-orbit results of the mission. The on-orbit results show that all function and capacity meets the requierments of the mission, the spacecraft is in good condition when flying, and the scheme design is correct and feasible.

关 键 词：探月三期 月地返回 高速再入 双平台 

分 类 号：V476.3[航空宇航科学与技术—飞行器设计]