DEVELOPMENT AND PERFORMANCE VALIDATION OF INTEGRATED ELECTRONIC UNIT FOR NANOSATELLITE

나노위성용 통합형 전장박스의 개발 및 성능검증

  • Chang Jin-Soo (Space System Research Lab, Hankuk Aviation University) ;
  • Kim Dong-Woon (Space System Research Lab, Hankuk Aviation University) ;
  • Lee Byung-Hoon (Space System Research Lab, Hankuk Aviation University) ;
  • Moon Byoung-Young (Space System Research Lab, Hankuk Aviation University) ;
  • Chang Young-Keun (Space System Research Lab, Hankuk Aviation University)
  • 장진수 (한국항공대학교 우주시스템 연구실) ;
  • 김동운 (한국항공대학교 우주시스템 연구실) ;
  • 이병훈 (한국항공대학교 우주시스템 연구실) ;
  • 문병영 (한국항공대학교 우주시스템 연구실) ;
  • 장영근 (한국항공대학교 우주시스템 연구실)
  • Published : 2006.04.01

Abstract

Unlike large satellites, small satellites, such as nanosatellite and microsatellite, provide a limited interior space for components mounting. In order to mitigate this issue, the compact Bus Electronic Unit (BEU) that integrates satellite electronic modules, combining most of bus subsystems and payloads electronic modules into one unit, has been developed for HAUSAT-2 nanosatellite. This paper addresses the design and environmental test result analyses of BEU.