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NTIS 바로가기한국추진공학회지 = Journal of the Korean Society of Propulsion Engineers, v.11 no.5 = no.42, 2007년, pp.60 - 71
박순영 (한국항공우주연구원 엔진팀) , 설우석 (한국항공우주연구원 엔진팀)
The startup characteristic of liquid propellant rocket engine should be focused on the stable ignition of combustion chamber and gas generator. Also, to lessen the propellants consumption during this period which doesn't contribute to the flight thrust, the engine has to be transferred to the nomina...
Kanumuri, A., Wakamatsu, Y., Shimura, K., Toki, K., and Torii, Y., "Start Transient Analysis of Turbopump-fed LOx/LH2 Rocket Engine (LE-5)," AIAA-89-2736
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한영민, 김승한, 문일윤, 김홍집, 김종규, 설우석, 이수용, 권순탁, 이창진, "충돌형 분사기 형태의 액체로켓 엔진용 가스발생기 연소성능시험," 한국추진공학회지, 제8권 제2호, 2004, pp.10-17
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