한국추진공학회지 (Journal of the Korean Society of Propulsion Engineers)

  • 제19권6호
  • /
  • Pages.72-80
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  • 2015
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  • 1226-6027(pISSN)
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  • 2288-4548(eISSN)
한국추진공학회 (The Korean Society of Propulsion Engineers)
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램제트 연료 적용을 위한 보론의 연소에 대한 고찰

A Study of the Boron Combustion for the Purpose of the Application for the Ramjet Fuel

  • Lee, Tae Ho (ReSeat Program, Korea Institute of Science and Technology Information) ;
  • Lee, Chang-Hoan (Informetrics Research Team, Korea Institute of Science and Technology Information)
  • 투고 : 2015.08.04
  • 심사 : 2015.09.29
  • 발행 : 2015.12.01
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⟨ 이전 논문 다음 논문 ⟩

초록

최근 기존의 통상적인 추진기관에서 새로이 공기 흡입 추진기관에 대한 관심이 커지고 있으며, 우리나라에서도 고체 램제트에 관한 기초 연구도 수행되는 등, 이 분야의 연구개발이 활발히 진행되고 있다. 고체 램제트의 연료에는 보론의 높은 열량 때문에 적용되고 있는데, 이 보론은 복잡한 연소 특성을 가지고 있어 이에 대한 연구도 많이 수행되어 오고 있다. 본 조사에서는, 램제트 연료 적용을 위하여 이러한 보론의 연소 특성을, 연구 개발되어 발표된 논문을 중심으로 하여 작성하였다.

Recently air breathing propulsion system is much interested in relatively comparing to the conventional chemical propulsion, and the R&D of this area is performed much more including the basic research of the solid ramjet in our country. The boron is applied to the solid fuel because of its high heating value, but it has a complicated combustion characteristics. therefore many researches have been studied in this area. In this paper the combustion characteristics of the boron have been investigated through the published papers for the purpose of the ramjet fuel application.

키워드

참고문헌

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