首页 | 本学科首页   官方微博 | 高级检索  
     

精密热控技术在太极一号卫星上的应用
引用本文:刘红,张晓峰,冯建朝,诸成,蔡志鸣,徐雨. 精密热控技术在太极一号卫星上的应用[J]. 空间科学学报, 2021, 41(2): 337-341. DOI: 10.11728/cjss2021.02.337
作者姓名:刘红  张晓峰  冯建朝  诸成  蔡志鸣  徐雨
作者单位:中国科学院微小卫星创新研究院 上海 201203
基金项目:中国科学院空间科学战略性先导科技专项资助
摘    要:为探测空间引力波,中国科学院提出了太极计划,其第一步是通过近地轨道卫星太极一号对核心载荷的关键技术进行验证.由于温度稳定性直接影响干涉仪测距和加速度的测量精度,太极一号卫星提出了(T±0.1)K的高精度、高稳定度温控指标.针对该指标要求设计热控方案,从热组件的选取到单机设备的应用均依照高指标进行控制.为了保证方案实施的...

关 键 词:高精度  高稳定度  多级温控  控温仪
收稿时间:2019-11-12

Application of Precision Thermal Control Techniques in Taiji-1 satellite
LIU Hong,ZHANG Xiaofeng,FENG Jianchao,ZHU Cheng,CAI Zhiming,XU Yu. Application of Precision Thermal Control Techniques in Taiji-1 satellite[J]. Chinese Journal of Space Science, 2021, 41(2): 337-341. DOI: 10.11728/cjss2021.02.337
Authors:LIU Hong  ZHANG Xiaofeng  FENG Jianchao  ZHU Cheng  CAI Zhiming  XU Yu
Affiliation:Institute of micro-satellite Innovation, Chinese Academy of Sciences, Shanghai 201203
Abstract:In order to detect gravitational waves in space, the Chinese Academy of Sciences has drawn up the Taiji plan. The first step of the Taiji plan is to verify the key techniques of the core payload through the Taiji-1 satellite in low Earth orbit. Because the temperature stability directly affects the measurement accuracy of the interferometer ranging and acceleration, the temperature control index of (T±0.1) K with high precision and high stability is proposed for the Taiji-1 satellite. Based on this requirement, an efficient thermal control scheme was designed. In the scheme, the thermal control from the selection of thermal components to the application of stand-alone equipment was controlled according to high indicators. At the same time, in the process of thermal implementation, in order to ensure the efficiency of the scheme, detailed control was also carried out. The thermal control scheme adopts the “constant temperature cage” as the design concept, adopts the means of three-stage temperature control, and combines the principle of active and passive. Finally, the high stability index of on-orbit flight temperature control of (T±0.005) K is obtained. Through the application research of high precision and high stability technology, it is found that thermal control heating scheme, heat leakage control, single resolution of temperature controller, temperature measuring circuit, control algorithm, control precision, temperature measuring resolution of temperature measuring element are still the important factors that restrict high precision temperature control technology. 
Keywords:
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《空间科学学报》浏览原始摘要信息
点击此处可从《空间科学学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号