航天器工程2025，Vol.34Issue(1)：118-125,8.DOI:10.3969/j.issn.1673-8748.2025.01.020
亚太6E卫星连接与分离机构设计与验证
Design and Verification of Connection and Separation Mechanism of APSTAR-6E Satellite
孙国鹏 1刘学 1柳翠翠 1乔心全 2方耀鹏 3王敏 3潘宇倩3
作者信息
- 1. 北京空间飞行器总体设计部,北京 100094
- 2. 北京空间飞行器总体设计部 航天器热控全国重点实验室,北京 100094
- 3. 中国空间技术研究院通信与导航卫星总体部,北京 100094
- 折叠
摘要
Abstract
According to the configuration characteristics of the APSTAR-6E satellite,a"clamp-band-and-separation-spring"type of inter-satellite connection and separation mechanism has been proposed.The design of separable plug and inter-satellite clamp-band retraction devices effective-ly eliminate the interference to the attitude of the independent propulsion module after separation caused by the separable plug and clamp-band.A multi-factor sensitivity analysis of separation dy-namics was conducted to identify the primary factors affecting separation safety.Based on the working environment and conditions of the connection and separation mechanism,a three-level ground test verification scheme was established and implemented.The analysis and test results demonstrate that the design,analysis,and verification methods for the APSTAR-6E satellite's connection and separation mechanism are correct and reasonable,providing significant reference value for the development of similar inter-satellite separation mechanisms in the future.关键词
全电推平台/机构/分离/设计/验证Key words
all-electric propulsion platform/mechanism/separation/design/verification引用本文复制引用
孙国鹏,刘学,柳翠翠,乔心全,方耀鹏,王敏,潘宇倩..亚太6E卫星连接与分离机构设计与验证[J].航天器工程,2025,34(1):118-125,8.
