Experimental Study of N2O/Ethanol Propulsion Systems

Bibliographic Information

Other Title
  • 亜酸化窒素(N_2O)/エタノール推進系の実験研究

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Description

A nitrous oxide (N2O)/ ethanol propulsion system is distinguished as the liquid propulsion with non-toxic, user-friendly, and storable bipropellant. The current target of the present study is to build a quickresponse and maneuverable main engine of a sounding-rocket like flying test bed which will be applied to the hypersonic air-breathing propulsion researches in the near future. The application to the spacecraft propulsion is also considered due to its compatibility in low-temperature operation environment. Two series of static firing tests were performed with 700 N class gas generator models so far. Current test results showed that valuable design data were collected and operational procedure was verified. Potential of application of composite materials to the combustion chamber was also examined from the chamber wall heat flux data obtained and the result of firing test using a thick SFRP chamber.

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Details 詳細情報について

  • CRID
    1573950402327556736
  • NII Article ID
    110007016982
  • NII Book ID
    AA1192675X
  • ISSN
    13491113
  • Text Lang
    ja
  • Data Source
    • CiNii Articles

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