Proceedings of the KSME Conference (대한기계학회:학술대회논문집)

The Korean Society of Mechanical Engineers (대한기계학회)
권호 표지

Structural Analysis of Thruster Heat Shield for Satellite Propulsion System

인공위성 추진시스템용 추력기 열차폐막의 구조해석

  • 이균호 (한국항공우주연구원 위성기술연구부) ;
  • 김정수 (한국항공우주연구원 위성기술연구부) ;
  • 한조영 (한국항공우주연구원 위성기술연구부)
  • Published : 2003.04.23
Download PDF
⟨ Previous Next ⟩

Abstract

MRE-1 dual thruster module(DTM) which will be installed to the present under development KOMPSAT(Korea Multi-Purpose Satellite) can provide reliable and cost-effective means of propulsive control for attitude and maneuvering control system. Thruster heat shield, one of the main components of DTM, is designed to intercept the radiative heat exchange between thruster and satellite during firing. The inside diameter of the current configuration will be decreased a little compared with that of the previous one due to manufacturing method change. Therefore, the possibility of interference between thruster and heat shield due to configuration change is investigated through structural analysis and their results are described in this paper.

Keywords