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Development of System Analysis Program of Liquid Rocket Engine II

액체로켓엔진 시스템 통합 해석 프로그램 개발 2

  • Lee, Sangbok (Department of Aerospace Engineering, Inha University) ;
  • Son, Min (Department of Aerospace Engineering, Korean Aerospace University) ;
  • Seo, Jongcheol (Department of Aerospace Engineering, Pusan National University) ;
  • Lim, Taekyu (Department of Aerospace Engineering, Inha University) ;
  • Roh, Tae-Seong (Department of Aerospace Engineering, Inha University) ;
  • Koo, Jaye (School of Aerospace and Mechanical Engineering, Korea Aerospace University) ;
  • Kim, Kuisoon (Department of Aerospace Engineering, Pusan National University)
  • Received : 2012.12.01
  • Accepted : 2013.12.28
  • Published : 2014.02.01

Abstract

The system analysis and design program of the liquid rocket engine has been developed for preliminary conceptual design process. The program consists of modular programs analyzing the main thruster, the gas-generator, turbo-pumps, the turbine, pipes, valves and so on. Each module has been developed in order to estimate performance, weight, and shape parameters of the components. The results of them have been verified with experimental data or other programs.

초기 개념설계를 위한 액체로켓엔진 시스템 통합 해석 프로그램을 개발하였다. 개발된 프로그램은 주추력실, 가스발생기, 터보펌프, 터빈, 파이프, 밸브 등의 부품 해석 모듈로 구성되었다. 각 해석 모듈은 구성품의 성능과 개략적인 형상, 무게를 추산할 수 있도록 개발되었으며 각기 결과의 타당성을 입증하였다.

Keywords

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