Analysis of Residual Propellant Gauging System Using Thermal Pumping of Satellite Employing Multi-tank System (다중탱크를 갖는 인공위성의 열펌핑을 이용한 잔여연료량 측정방법 연구)
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- Proceedings of the Korean Society of Propulsion Engineers Conference
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- 2004.10a
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- pp.141-145
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- 2004