航天器工程2023，Vol.32Issue(6)：18-24,7.DOI:10.3969/j.issn.1673-8748.2023.06.003
超低轨道卫星热控分系统原子氧防护设计
Design of Atomic Oxygen Protection for Thermal Control System of Ultra-low Orbit Satellites
任红艳 1杨昌鹏 1赵欣 1许峰 1李挺豪1
作者信息
- 1. 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
- 折叠
摘要
Abstract
In order to meet the requirements for long-term use of Ultra-low orbit(ULO)satel-lites,it is necessary to perform atomic oxygen protection for thermal control materials exposed to high cumulative doses of atomic oxygen or select thermal control materials that are resistant to a-tomic oxygento ensure that the onboard instruments and equipment can maintain a favorable working environment throughout its entire operational lifecycle.The research results on the influ-ence of atomic oxygen on commonly used thermal control materials on domestic and foreign spacecraft are analyzed,and the erosion mechanism and rate of atomic oxygen on various materials are summarized.Based on this,suggestions for thermal control design of ULO satellites at an or-bital altitude of 268km are given,providing reference for the thermal control design of domestic ULO satellites.关键词
超低轨道卫星/原子氧防护/热控分系统Key words
Ultra-low orbit satellites/atomic oxygen protection/thermal control system分类
航空航天引用本文复制引用
任红艳,杨昌鹏,赵欣,许峰,李挺豪..超低轨道卫星热控分系统原子氧防护设计[J].航天器工程,2023,32(6):18-24,7.
