Journal of Aerospace System Engineering (항공우주시스템공학회지)

The Society for Aerospace System Engineering (항공우주시스템공학회)
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A Review on Major Foreign Research Trend of Monomethylhydrazine Reaction for Space Propulsion Part II : Chemical Reaction of Monomethylhydrazine-Dinitrogen Tetroxide

우주추진용 모노메틸하이드라진 반응에 대한 주요 해외연구 동향 조사 Part II : 모노메틸하이드라진-사산화이질소의 화학반응

  • Received : 2015.12.27
  • Accepted : 2016.01.13
  • Published : 2016.03.31
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Abstract

Space propulsion system produces required thrust for satellites and space launch vehicles by using chemical reactions of a liquid fuel and a liquid oxidizer typically. Among several liquid propellants, the monomethylhydrazine-dinitrogen tetroxide is expecially preferred for a GEO satellite propellants due to their better storability in liquid phase during a long mission life under a freezing space environment. Recently, a development of the monomethylhydrazine-dinitrogen tetroxide bipropellant system becomes important as the national space program requires the heavier and the more efficient space system. Thus, the objective of the present study is to review a foreign research trend of a chemical reaction between the monomethyhydrazine fuel and the dinitrogen tetroxide oxidizer to understand a fundamental basis of their characteristics to prepare for domestic development in future.

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References

  1. 장요한, 이균호, "인공위성 궤도전이 및 자세제어용 이원추진제 로켓엔진의 개발현황," 한국추진공학회지, 19권 1호, pp.50-60, 2015.
  2. Sutton, G. P., Rocket Propulsion Elements, 8th ed., John Wiley & Sons Inc., 2010.
  3. 한조영, "영국산 화학추진시스템의 기술이력과 통신해양기상위성 이원추진제 추진시스템", 항공우주시스템공학회지, 2권 1호, pp.28-36, 2008.
  4. 장요한, 이균호, "우주추진용 모노메틸하이드라진 반응에 대한 주요 해외연구 동향 조사 Part I : 모노메틸하이드라진의 열분해 반응", 항공우주시스템공학회지, 10권 1호, 2016.
  5. Catoire, L., Chaumeix, N., Paillard, C., "Chemical Kinetic Model for Monomethylhydrazine/Nitrogen Tetroxide Gas Phase Combustion and Hypergolic Ignition," Journal of Propulsion and Power, vol. 20, no. 1, pp.87-92, 2004. https://doi.org/10.2514/1.9234
  6. Ray J., Ariane 5 Failure Investigation Focuses on Upper Stage, https://spaceflightnow.com/ariane/v142/010713followup.html, Spaceflight Now Inc., 2001.
  7. Frank, I., Hammerl, A., Klapotke, T. M., Nonnenberg, C., Zewen, H., "Processes during the Hypergolic Ignition between Monomethylhydrazine (MMH) and Dinitrogen Tetroxide ($N_2O_4$) in Rocket Engines," Propellants, Explosives, Pyrotechnics, vol. 30, no. 1, pp.44-52, 2005. https://doi.org/10.1002/prep.200400084
  8. Liu, Y., Zybin, S. V., Guo, J., van Duin, A. C. T., Goddard III, W. A., "Reactive Dynamics Study of Hypergolic Bipropellants: Monomethylhydrazine and Dinitrogen Tetroxide," The Journal of Physical Chemistry B, vol. 116, pp.14136-14145, 2012. https://doi.org/10.1021/jp308351g
  9. Liu, W. G., Wang, S., Dasgupta, S., Thynell, S. T., Goddard III, W. A., Zybin, S., Yetter, R. A., "Experimental and Quantum Mechanics Investigations of Early Reactions of Monomethylhydrazine with Mixtures of $NO_2$ and $N_2O_4$," Combustion and Flame, vol. 160, pp.970-981, 2013. https://doi.org/10.1016/j.combustflame.2013.01.012