Volume 36 Issue 3
May  2016
Turn off MathJax
Article Contents
ZHOU Yangeng. A Balanced Satellite Thermal Control Optimization Method for Different Orbit and Attitude[J]. Chinese Journal of Space Science, 2016, 36(3): 380-385. doi: 10.11728/cjss2016.03.380
Citation: ZHOU Yangeng. A Balanced Satellite Thermal Control Optimization Method for Different Orbit and Attitude[J]. Chinese Journal of Space Science, 2016, 36(3): 380-385. doi: 10.11728/cjss2016.03.380

A Balanced Satellite Thermal Control Optimization Method for Different Orbit and Attitude

doi: 10.11728/cjss2016.03.380
  • Received Date: 2015-11-12
  • Rev Recd Date: 2016-03-02
  • Publish Date: 2016-05-15
  • Based on analysis of the thermal control design of traditional satellites,an optimization method for satellite thermal design which is applicable to both Sun-synchronous orbit and lowinclination orbit is presented.Using this optimization method,thermal simulation analysis is made for a satellite under both orbit conditions,and the satellite thermal balance test and in-orbit validation are conducted for the Sun-synchronous orbit.Combined with thermal simulation results,it is shown that the thermal design of low-inclination orbit satellite conditions can reduce the ground test verification,shorten the satellite development cycle and save the costs significantly.This research work can provide reference for the design optimization of satellite thermal control.

     

  • loading
  • [1]
    MA Wei, XUAN Yimin. Thermal design and infrared characteristics of the satellite[J]. Spacecraft Eng., 2009, 18(2):48-54(马伟, 宣益民. 卫星系统热特性分析[J]. 航天器工程, 2009, 18(2):48-54)
    [2]
    MIN Guirong. Satellite Thermal Control Technology[M]. Beijing:China Astronautics Press, 1991(闵桂荣. 卫星热控制技术[M]. 北京:中国宇航出版社, 1991)
    [3]
    HE Zhi, XU Xiaodong. Design of thermal control subsystem for flying satellite simulator[J]. Spacecraft Eng., 2011, 20(1):82-87(何治, 许晓冬. 一种卫星飞行模拟器的热控分系统模型设计[J].航天器工程, 2011, 20(1):82-87)
    [4]
    HOU Zengqi, HU Jingang. Spacecraft Thermal Control Techniques-Principles and Application[M]. Beijing:China Science and Technology Press, 2007(侯增祺, 胡金刚. 航天器热控制技术-原理及其应用[M]. 北京:中国科学技术出版社, 2007)
    [5]
    XU Xianghua, CHENG Xuetao. Analysis on space thermal environment for circular Sun-synchronous orbit[J]. J. Astron., 2012, 33(3):399-405(徐向华, 程雪涛. 圆形太阳同步轨道卫星的空间热环境分析[J]. 宇航学报, 2012, 33(3):399-405)
    [6]
    LIU Jia, LI Yunze. A review of small satellite thermal control system[J]. Spacecraft Envir. Eng., 2011, 28(1):77-82(刘佳, 李运泽. 微小卫星热控系统的研究现状及发展趋势[J]. 航天器环境工程, 2011, 28(1):77-82)
    [7]
    HOU Xinbin, SAO Xinguo. Thermal design and numerical results of Chang'E-1 orbiter[J]. Spacecraft Eng., 2006, 15(4):21-26(侯兴宾, 邵兴国. 嫦娥一号卫星热设计及计算分析[J]. 航天器工程, 2006, 15(4):21-26)
    [8]
    HAN Yuge, XUAN Yimin. Parameter sensitivity analysis for the satellite thermal design[J]. Chin. J. Comput. Phys., 2004, 21(5):455-460
    [9]
    MEGAHED A, EL-DIB A. Thermal design and analysis for battery module for a remote sensing satellite[J]. J. Spacecraft Rockets, 2007, 44(4):920-926
    [10]
    BALDAUFF R W, ARMIGER W J. Design and analysis of the thermal control system for the TacSat-4 spacecraft COMMx payload[J]. Featured Res., 2009, 11(3):113-124
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article Views(1072) PDF Downloads(925) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return