항공우주시스템공학회지 (Journal of Aerospace System Engineering)

  • 제10권1호
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  • Pages.66-73
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  • 2016
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  • 1976-6300(pISSN)
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  • 2508-7150(eISSN)
항공우주시스템공학회 (The Society for Aerospace System Engineering)
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우주추진용 모노메틸하이드라진 반응에 대한 주요 해외연구 동향 조사 Part I : 모노메틸하이드라진의 열분해 반응

A Review on Major Foreign Research Trend of Monomethylhydrazine Reaction for Space Propulsion Part I : Thermal Decomposition Reaction of Monomethylhydrazine

  • 투고 : 2015.12.10
  • 심사 : 2016.01.13
  • 발행 : 2016.03.31
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초록

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. For example, monomethylhydrazine-dinitrogen tetroxide, liquid hydrogen-liquid oxygen and RP-1-liquid oxygen are conventional combinations of liquid propellants used for the liquid propulsion system. Among several liquid propellants, the monomethylhydrazine is expecially preferred for a satellite fuel due to its better storability in liquid phase during a relatively long mission period under a space environment. Thus, a development importance of a bipropellant system using the monomethylhydrazine fuel is recognized recently as the national space program proceeds on a large scale. The objective of the present study is to review a foreign research trend of a thermal decomposition reaction of monomethyhydrazine to understand a fundamental basis of its chemical reaction to prepare for domestic development in future.

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참고문헌

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