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NTIS 바로가기한국추진공학회지 = Journal of the Korean Society of Propulsion Engineers, v.24 no.6, 2020년, pp.93 - 100
김대진 (Turbopump Team, Korea Aerospace Research Institute) , 강병윤 (Turbopump Team, Korea Aerospace Research Institute) , 최창호 (Turbopump Team, Korea Aerospace Research Institute)
The turbopump of the liquid rocket engine adapts an inducer to minimize the cavitation due to the variations of the propellants supply condition. However, the inducer introduces cavitation instabilities which are well-known problems in the engine development. In this paper, operational characteristi...
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