航天器工程2025，Vol.34Issue(1)：160-165,6.DOI:10.3969/j.issn.1673-8748.2025.01.026
亚太6E卫星太阳电池阵优化设计与验证
Optimization Design and Performance Evaluation of Solar Array Applied for APSTAR-6E Satellite
李键 1章玄 1李大伟 1邹世纯 2王磊 1张子亮 1魏强 1王敏 1潘宇倩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
- 2. 中国电子科技集团公司第十八研究所,天津 300384
- 折叠
摘要
Abstract
By analyzing mission requirements of the APSTAR-6E satellite built based on DFH-3E all-electric propulsion platform,the design characteristics of the solar array are identified,inclu-ding more severe irradiation and thermal environment,the influence of electric propulsion plumes,and the first application of Power Control and Distribution Unit(PCDU).An optimiza-tion design for the solar array of the all-electric propulsion satellite is proposed,including the high efficiency,radiation resistance and lightweight solar cell and thickened cover design,solar array layout and connection design,and thermal environment adaptability design.The evaluation of the telemetry data during the orbit transfer and in orbit phases is conducted.Results show that the performance can meet the design requirements.This case can provide design reference for so-lar array of future all-electric propulsion satellites.关键词
全电推卫星/亚太6E卫星/太阳电池阵/辐照Key words
all-electric propulsion satellite/APSTAR-6E satellite/solar array/irradiation分类
航空航天引用本文复制引用
李键,章玄,李大伟,邹世纯,王磊,张子亮,魏强,王敏,潘宇倩..亚太6E卫星太阳电池阵优化设计与验证[J].航天器工程,2025,34(1):160-165,6.
