航天器工程2025，Vol.34Issue(1)：57-62,6.DOI:10.3969/j.issn.1673-8748.2025.01.010
亚太6E卫星构型布局设计
Configuration and Layout Design of APSTAR-6E Satellite
靖法 1郭琳 1魏强 1王敏 1侯卫国1
作者信息
- 1. 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
In the field of APSTAR-6E satellite configuration design,the self-combination configu-ration and separable design scheme of main satellite and independent propellant module is pro-posed,achieving the goal of a small-medium sized all electric propulsion satellite launch with sin-gle launch vehicle at low total price.In the field of satellite layout design,the main satellite lay-out scheme being compatible with ion and hall electric propulsion is proposed to meet the diffe-rent requirements of ion and hall electric propulsion systems for satellite and to achieve the com-prehensive application of the advantage of ion and hall electric propulsion systems.The configu-ration and layout scheme proposed in this paper represents the first instance in both domestic and international system design practices for all-electric propulsion satellite and its on-orbit applica-tion has verified the correctness and rationality of the design,which achieves a breakthrough in the configuration and layout technology of all-electric propulsion satellites in China.关键词
亚太6E卫星/全电推进/构型布局/独立推进舱Key words
APSTAR-6E satellite/all-electric propulsion/configuration and layout/independent propellant module分类
航空航天引用本文复制引用
靖法,郭琳,魏强,王敏,侯卫国..亚太6E卫星构型布局设计[J].航天器工程,2025,34(1):57-62,6.
