달탐사용 탑재체 개발을 위한 전산응용 개념 설계

CONCEPTUAL DESIGN BY APPLIED COMPUTATIONAL ENGINEERING FOR THE MOON EXPLORER PAYLOAD DEVELOPMENT

  • 김정훈 (한국항공우주연구원 위성열/추진팀) ;
  • 전형열 (한국항공우주연구원 위성열/추진팀) ;
  • 주광혁 (한국항공우주연구원 정지궤도위성체계팀) ;
  • 김병수 (충남대학교 항공우주공학과)
  • 발행 : 2011.05.26

초록

Nowadays, SELENE-2 is under development for the moon explorer rover in Japan. AXS(Active X-ray Spectrometer) sensor development among the candidated payloads will be on going by the world-wide co-operation. The thermal design, analysis and test will be specially performed by Korean institutes. CFD techniques are used for the conceptual design and analysis. Thin-shell plate meshes being applied by Monte-Carlo Ray Tracing Method are generated for the thermal radiation analysis. Lumped capacity model is employed for the thermal conduction simulation of the AXS payload itself. Various shapes of the payload configuration with thermal boundary conditions are proposed and selected on the purpose of the analysis of the initial design. The results of the analysis are supposed to be used as the baseline for the further detailed design of the AXS payload in the future.

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