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한국형 달 탐사용 원자력전지의 열제어 구조 연구

Study on the Thermal Design of Nuclear Battery for Lunar Mission

  • 홍진태 (한국원자력연구원 하나로이용연구본부) ;
  • 손광재 (한국원자력연구원 하나로이용연구본부) ;
  • 김종범 (한국원자력연구원 하나로이용연구본부) ;
  • 박종한 (한국원자력연구원 하나로이용연구본부) ;
  • 안동규 (조선대학교 기계공학과) ;
  • 양동열 (한국과학기술원 기계공학과)
  • Hong, Jintae (Department of Hanaro Utilization and Research, Korea Atomic Energy Research Institute) ;
  • Son, Kwang-Jae (Department of Hanaro Utilization and Research, Korea Atomic Energy Research Institute) ;
  • Kim, Jong-Bum (Department of Hanaro Utilization and Research, Korea Atomic Energy Research Institute) ;
  • Park, Jong-Han (Department of Hanaro Utilization and Research, Korea Atomic Energy Research Institute) ;
  • Ahn, Dong-Gyu (Department of Mechanical Engineering, Chosun University) ;
  • Yang, Dong-Yol (Department of Mechanical Engineering, Korea Advanced Institute of Science and Technology)
  • 투고 : 2016.02.25
  • 심사 : 2016.03.17
  • 발행 : 2016.04.01

초록

For a stable electric power supply in the space, nuclear batteries have been used as the main power source in a spacecraft owing to their long lifetime and high reliability. In accordance with the plan for lunar mission in Korea, nuclear batteries will supply electricity to the rover that needs to be developed. According to the information about the estimated payload, Korea Atomic Energy Research Institute started with the conceptual design based on the previous studies in USA and Russia. Because a nuclear battery converts the decay heat of the radioisotope into electricity, thermal design, radiation shield, and shock protection need to be considered. In this study, two types of nuclear batteries, radial type and axial type, were designed according to the alignment of the thermoelectric module. Heat transfer analyses were performed to compare their thermoelectric efficiency, and test mockups were fabricated to evaluate their performances.

키워드

참고문헌

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