캐비테이션 환경에서의 액체로켓엔진용 산화제펌프의 고주파 신호 분석

목차 (Table of Contents)

• ABSTRACT
• 초록
• 1. 서론
• 2. 시험 개요
• 3. 시험 결과 및 분석
• 4. 결론
• References

참고문헌 (Reference)

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2 Tsujimoto, Y., "New Types of Cavitation Instabilities in Inducers" 2002

3 Tani, N., "Influence of Flow Coefficient and Flow Structure on Rotational Cavitation in Inducer" 134 (134): 2012

4 Hong, S., "Experimental Study on Cavitation Instabilities of Small Turbopump for Rocket Engine" 60 (60): 230-234, 2017

5 Hashimoto, T., "Experimental Study of Rotating Cavitation of Rocket Propellant Pump Inducers" 13 (13): 488-494, 1997

6 Kamijo, K., "Experiences in the Development of Japanese Rocket Engines" 106 (106): 286-288, 2003

7 Lee, Y. H., "Experiences in the Development of Japanese Rocket Engines" 6 (6): 111-114, 2003

8 Ryan, R. S., "Developmental Problems and Their Solution for the Space Shuttle Main Engine Alternate Liquid Oxygen High-pressure Turbopump" NASA 1995

9 Kim, D. J., "Cavitation Instabilities of LOX Pump for KSLV-II" 2016

10 Kim, D. J., "Cavitation Instabilities of Fuel Pump for KSLV-II" 2016

11 김대진, "75톤급 액체로켓엔진용 산화제펌프의 수류시험" 한국항공우주연구원 10 (10): 122-128, 2011