한국추진공학회지 (Journal of the Korean Society of Propulsion Engineers)

  • 제22권2호
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  • Pages.125-130
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  • 2018
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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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정지궤도위성용 한국형 우주발사체를 위한 고성능 상단 엔진 개발 현황 및 계획

Development Status and Plan of the High Performance Upper Stage Engine for a GEO KSLV

  • Yu, Byungil (Engine Test & Evaluation Team, Korea Aerospace Research Institute) ;
  • Lee, Kwang-Jin (Engine Test & Evaluation Team, Korea Aerospace Research Institute) ;
  • Woo, Seongphil (Engine Test & Evaluation Team, Korea Aerospace Research Institute) ;
  • Im, Ji-Hyuk (Engine Test & Evaluation Team, Korea Aerospace Research Institute) ;
  • So, Younseok (Engine Test & Evaluation Team, Korea Aerospace Research Institute) ;
  • Jeon, Junsu (Engine Test & Evaluation Team, Korea Aerospace Research Institute) ;
  • Lee, Jungho (Engine Test & Evaluation Team, Korea Aerospace Research Institute) ;
  • Seo, Daeban (Engine Test & Evaluation Team, Korea Aerospace Research Institute) ;
  • Han, Yeoungmin (Engine Test & Evaluation Team, Korea Aerospace Research Institute) ;
  • Kim, Jinhan (Engine Test & Evaluation Team, Korea Aerospace Research Institute)
  • 투고 : 2017.02.20
  • 심사 : 2018.01.05
  • 발행 : 2018.04.01
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⟨ 이전 논문 다음 논문 ⟩

초록

항공우주연구원에서는 정지궤도용 우주발사체에 적용 가능한 고성능 상단 엔진에 대한 선행기술 개발이 진행 중에 있다. 한국형발사체(KSLV)는 gas generator를 이용한 개방형 사이클 엔진이며, 저궤도 위성 발사를 위한 발사체로 향후 정지궤도위성 발사체를 위해서는 이보다 높은 비추력을 가진 고효율의 상단엔진이 필요하게 된다. 이러한 요구조건을 충족시키기 위해 다단 연소방식의 엔진이 필요하며, 본 논문에서는 당 연구원이 진행 중인 다단 연소 사이클 엔진 개발 진행 현황과 향후 계획을 기술하였다.

The technology development of a high performance upper stage engine for a GEO(GEostationary Orbit) KSLV(Korea Space Launch Vehicle) is undergoing in Korea Aerospace Research Institute. KSLV is composed of an open cycle engine with gas generator, which is for a low orbit launch vehicle. However the future GEO launch vehicle requires a high performance upper stage engine with a high specific impulse. The staged combustion cycle engine is necessary for this mission. In this paper, current progress and future plan for staged combustion cycle engine development is described.

키워드

참고문헌

  1. Im, J.H., Woo, S.P., Jeon, J.S., Lee, K.J., Yu, B.I. and Han, Y.M., "Conceptual Design of Combustion Chamber for 9 Tonf-Class Staged Combustion Cycle Engine," KSPE Fall Conference, Kangwon, Korea, pp. 1044-1046, Dec. 2016.
  2. Woo, S.P., Lee, K.J., Im, J.H., Jeon, J.S., Hwang, C.H. and Han, Y.M., "The Design of Technology Demonstration Model for Tests of Staged Combustion Cycle Engine," KSPE Fall Conference, Kangwon, Korea, pp. 934-937, Dec. 2016.
  3. So, Y.S., Woo, S.P., Lee, K.J., Yu, B.I., Kim, J.H., Cho, H.R., Bang, J.S. and Han, Y.M., "Results of cold flow test and design of injectors for Oxidizer-rich preburner," KSPE Fall Conference, Kangwon, Korea, pp. 1016-1021, Dec. 2016.
  4. Lee, K.J., Kim, S.R., Kim, S.H., Kim, S.H., Kim, C.H., Seo, D.B., Woo, S.P., Yu, B.I., So, Y.S., Yi, S.J., Lee, J.H., IM, J.H., Jeon, J.S., Cho, N.K., Hwang, C.H. and Han, Y.M., "Development Test Status of 7 tonf-class Engine for KSLV-II," KSPE Fall Conference, Kangwon, Korea, pp. 874-882, Dec. 2016.
  5. Kim, S.R., Yi, S.J. and Han, Y.M., "An Startup Analysis of reconstructed Staged combustion Engine PowerPack," KSPE Fall Conference, Kangwon, Korea, pp. 909-912, Dec. 2016.