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http://dx.doi.org/10.5139/JKSAS.2003.31.8.115

Design and Integration of STM Propulsion System for LEO Observation Satellite Development  

Kim,Jeong-Su (한국항공우주연구원 위성기술실)
Lee,Gyun-Ho (한국항공우주연구원 위성기술실)
Han,Jo-Yeong (한국항공우주연구원 위성기술실)
Jang,Gi-Won ((주)한화)
Choe,Jin-Cheol ((주)스페이스솔루션)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.31, no.8, 2003 , pp. 115-124 More about this Journal
Abstract
To guarantee the proper functions of a satellite in the extreme space environment, the several test models are developed generally. There are advantages that the design and the analysis of Flight Model(FM) can be validated through these test models, and the functional reliabilities can be increased by reflecting the modifications on the final design of FM. The integration and test of Structure & Thermal Model(STM) of KOMPSAT, being currently developed, have been completed. In this paper, the processes of design/analysis and integration of the STM propulsion system, one of the KOMPSAT modules, are described.
Keywords
Propulsion System; FM; STM; KOMPSAT;
Citations & Related Records
Times Cited By KSCI : 2  (Citation Analysis)
연도 인용수 순위
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