摘要
20世纪80年代中期以来,小卫星技术发展十分迅速,并带动了卫星向小型化发展.介绍了微型航天器温度环境分析方法,使用简单热分析模型和整星热分析模型分析了某微型航天器的温度情况,并介绍了其热控系统设计方案.
Since the mid eighties, the technology of microsatellites have developed very rapidly and it promoted the miniaturization of the satellites. The paper introduces the method of analyzing the microspacecraft's thermal. Through the simple thermal model and a integrative satellite thermal model, it analyzes the temperature of the microspacecraft and introduces the project of the thermal design.
出处
《装备指挥技术学院学报》
2002年第5期44-46,共3页
Journal of the Academy of Equipment Command & Technology
基金
国家教委骨干教师资助项目 (2 0 0 0 10 2 7 0 10 5 613 3 )
关键词
微型航天器
热控系统
热量
辐射
microspacecraft
thermal control system
radiation
