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Research Trend Analysis on Modeling and Simulation of Liquid Propellant Supply System

액체 추진제 공급 시스템의 모델링 및 시뮬레이션 연구 동향 분석

  • Lee, Juyeon (Department of Aerospace Engineering, Inha University) ;
  • Cha, Seung-Won (Department of Aerospace Engineering, Inha University) ;
  • Ha, Donghui (Department of Aerospace Engineering, Inha University) ;
  • Kee, Wonkeun (Department of Aerospace Engineering, Graduate School of Chungnam National University) ;
  • Lee, Jaecheong (Department of Aerospace Engineering, Graduate School of Chungnam National University) ;
  • Huh, Hwanil (Department of Aerospace Engineering, Chungnam National University) ;
  • Roh, Tae-Seong (Department of Aerospace Engineering, Inha University) ;
  • Lee, Hyoung Jin (Department of Aerospace Engineering, Inha University)
  • Received : 2019.10.08
  • Accepted : 2019.11.12
  • Published : 2019.12.01

Abstract

Modeling and Simulation(M&S) for a liquid propellant supply system is a technique to predict the performance of components and systems under certain conditions based on mathematical modeling for each component of the engine. In this paper, the basic structure of M&S for the supply system applied to liquid rocket engines was obtained by analyzing the related research conducted. The basic mathematical modeling of components was organized and the characteristics of each study result were analyzed. Based on the analysis and validation results, M&S method of advanced foreign research institutes was also identified, and factors related to its accuracy were described.

액체 추진제 공급 시스템에 대한 Modeling and Simulation(M&S)는 엔진의 각 구성품을 수학적으로 모델링하여 특정 조건에서의 성능을 예측하는 기법이다. 본 논문에서는 국내외에서 수행된 관련 연구를 분석하여 액체 로켓엔진에 적용되는 공급 시스템에 대한 M&S의 기본 구성을 파악하였다. 구성요소의 보편적인 수학적 모델링을 정리하고 각 연구 결과에 대한 특징을 분석하였다. 또한 해석 및 검증 결과를 바탕으로 선진 해외 연구 기관의 M&S 수준을 확인하였고, M&S 기법의 정확도와 관련한 요인을 기술하였다.

Keywords

References

  1. Mason, J.R. and Southwick, R.D., "Large liquid rocket engine transient performance simulation system," NASA-CR-184099, 1991.
  2. Kimura, T., Takahashi, M., Wakamatsu, Y., Hasegawa, K., Yamanishi, N., and Osada, A., "Rocket Engine Dynamic Simulator (REDS)," JAXA-1349-1113, 2004.
  3. Binder, M., "An RL10A-3-3A rocket engine model using the Rocket Engine Transient Simulator(ROCETS) software," 29th Joint Propulsion Conference and Exhibit, Monterey, CA, pp. 2357, June 1993.
  4. Yamanishi, N., Kimura, T., Takahashi, M., Okita, K., Atsumi, M., and Negishi, H., "Transient analysis of the LE-7A rocket engine using the rocket engine dynamic simulator (REDS)," 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Fort Lauderdale, Florida, pp. 3850, July 2004.
  5. Moral, J., Perez Vara, R., Steelant, J., and De Rosa, M., "ESPSS simulation platform," Space Propulsion, May 2010.
  6. Binder, M., "A transient model of the RL10A-3-3A rocket engine," 31st Joint Propulsion Conference and Exhibit, San Diego, U.S.A., pp. 2968, July 1995.
  7. Di Matteo, F., De Rosa, M., and Onofri, M., "Transient simulation of the RL-10A-3-3A rocket engine," Space Propulsion Conference, Bordeaux, France, May 2012.
  8. Devereaux, A. and Francois, C., "Development testing of a new bipropellant propulsion system for the GMP-T spacecraft," 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Nashville, U.S.A., pp. 6649, July 2010.
  9. Wei, L., Liping, C., Gang, X., Ji, D., Haiming, Z., and Hao, Y., "Modeling and simulation of liquid propellant rocket engine transient performance using modelica," Proceedings of the 11th International Modelica Conference, Versailles, France, No. 118, pp. 485-490, September 2015.
  10. Mota, F.A.D.S., Hinckel, J.N., Rocco, E.M., and Schlingloff, H., "Modeling and Analysis of a LOX/Ethanol Liquid Rocket Engine," Journal of Aerospace Technology and Management, Vol. 10, 2018.
  11. Sangbok, L., Taekyu, L., and Tae-Seong, R., "Design Optimization of Liquid Rocket Engine Using Genetic Algorithms," Journal of the Korean Society of Propulsion Engineers, Vol. 16(2), pp. 25-33, 2012. https://doi.org/10.6108/KSPE.2012.16.2.025
  12. Soon-Young, P., Won-kook, C., and Woo-Seok, S., "A Mathematical Model of Liquid Rocket Engine Using Simulink," Aerospace Engineering and Technology, Vol. 8(1), pp. 82-97, 2009.
  13. Hyun-Duck, K., Sejin, K., and Chang-Ho, C., "Performance assessment of electrically driven pump-fed LOX/Kerosene cycle rocket engine: Comparison with gas generator cycle," Aerospace Science and Technology, Vol. 77, pp. 67-82, 2018. https://doi.org/10.1016/j.ast.2018.02.033
  14. Ernst, R.R.L., "Liquid Rocket Analysis (LiRA): development of a liquid bi-propellant rocket engine design, analysis and optimization tool," Master. Dissertation, Department of Science in Spaceflight, Delf University of Technology, 2014.
  15. Manfletti, C., "Transient Simulation of Liquid Rocket Engines: A Step Towards A More Educated propellant Choice Between Kerosene And Methane," Proceedings of the 2nd International Conference on Green Propellants for Space Propulsion, Sardinia, Italy, pp. 1-6, June 2004.
  16. Binder, M., Thomas T., and Joseph P.V., "RL10A-3-3A rocket engine modeling project," NASA Technical Memorandum 107318, 1997.
  17. Di Matteo, F., "Modelling and simulation of liquid rocket engine ignition transients." Ph. D. Dissertation, Department of Technologia Aeronautica, Sapienza University, Roma, 2012.