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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
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 Title & Authors
A Review on Major Foreign Research Trend of Monomethylhydrazine Reaction for Space Propulsion Part II : Chemical Reaction of Monomethylhydrazine-Dinitrogen Tetroxide
Jang, Yohan; Lee, Kyun Ho;
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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.
 Keywords
Space Propulsion;Bipropellant;Monomethylhydrazine;Dinitrogen Tetroxide;Chemical Reaction;
 Language
Korean
 Cited by
 References
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