亚太6E卫星构型布局设计  

Configuration and Layout Design of APSTAR-6E Satellite

作　　者：靖法[1] 郭琳[1] 魏强[1] 王敏[1] 侯卫国[1] JING Fa;GUO Lin;WEI Qiang;WANG Min;HOU Weiguo(Institute of Telecommunication and Navigation Satellites,China Academy of Space Technology,Beijing 100094,China)

机构地区：[1]中国空间技术研究院通信与导航卫星总体部,北京100094

出　　处：《航天器工程》2025年第1期57-62,共6页Spacecraft Engineering

摘　　要：在亚太6E卫星构型设计中,提出主星与独立推进舱自串联构型及可分离设计方案,实现了中小型全电推进卫星低总价、一箭一星发射目标。在卫星布局设计中,提出兼容离子、霍尔电推进的主星布局方案,同时能满足离子和霍尔电推进系统对卫星的差异化需求,实现了这2种电推进系统优势的综合运用。文章提出的构型布局方案,在国内外全电推进卫星总体设计中均属首次,其在轨应用验证了设计的正确合理,实现了我国全电推进卫星构型布局技术的突破。In the field of APSTAR-6E satellite configuration design,the self-combination configuration and separable design scheme of main satellite and independent propellant module is proposed,achieving the goal of a small-medium sized all electric propulsion satellite launch with single launch vehicle at low total price.In the field of satellite layout design,the main satellite layout 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 comprehensive application of the advantage of ion and hall electric propulsion systems.The configuration 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 application 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 

分 类 号：V474.2[航空宇航科学与技术—飞行器设计]