히트 파이프가 장착된 정지궤도 위성 패널 열해석 프로그램 개발

DEVELOPMENT OF THERMAL ANALYSIS PROGRAM FOR HEAT PIPE INSTALLED PANEL OF GEOSTATIONARY SATELLITE

  • 전형열 (한국항공우주연구원 위성기술실 위성 열/추진팀) ;
  • 기정훈 (한국항공우주연구원 위성기술실 위성 열/추진팀) ;
  • 한조영 (한국항공우주연구원 위성기술실 위성 열/추진팀) ;
  • 채종원 (한국항공우주연구원 위성기술실 위성 열/추진팀)
  • 발행 : 2010.05.13

초록

The north and south panel of a geostationary satellite are used for radiator panels to reject internal heat dissipation of electronics units and utilize several heat pipe networks to control the temperatures of units and the satellite within proper ranges. The design of these panels is very important and essential at the conceptual design and preliminary design stage so several thousands of nodes of more are utilized in order to perform thermal analysis of panel. Generating a large number of nodes(meshes) of the panel takes time and is tedious work because the mesh can be easily changed and updated by locations of units and heat pipes. Also the detailed panel model can not be integrated into spacecraft thermal model due to its node size and limitation of commercial satellite thermal analysis program. Thus development of a program was required in order to generate detailed panel model, to perform thermal analysis and to make a reduced panel model for the integration to the satellite thermal model. This paper describes the development and the verification of panel thermal analysis program with ist main modules and its main functions.

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