Journal of Aerospace System Engineering (항공우주시스템공학회지)

The Society for Aerospace System Engineering (항공우주시스템공학회)
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Development and Flight Test of Educational Water Rocket CULV-1 for Implementation of Launch Vehicle Separation Sequence and Imaging Data Acquisition

발사체 분리과정모사 및 단계별 영상획득이 가능한 교육용 물로켓 CULV-1 개발 및 비행시험

  • Lee, Myeongjae (Space Technology Synthesis Lab, Dept. of Aerospace Engineering, Chosun University) ;
  • Park, Taeyong (Space Technology Synthesis Lab, Dept. of Aerospace Engineering, Chosun University) ;
  • Kang, Soojin (Space Technology Synthesis Lab, Dept. of Aerospace Engineering, Chosun University) ;
  • Jang, Sueun (Space Technology Synthesis Lab, Dept. of Aerospace Engineering, Chosun University) ;
  • Oh, Hyunung (Space Technology Synthesis Lab, Dept. of Aerospace Engineering, Chosun University)
  • 이명재 (조선대학교 항공우주공학과 우주기술융합연구실) ;
  • 박태용 (조선대학교 항공우주공학과 우주기술융합연구실) ;
  • 강수진 (조선대학교 항공우주공학과 우주기술융합연구실) ;
  • 장수은 (조선대학교 항공우주공학과 우주기술융합연구실) ;
  • 오현웅 (조선대학교 항공우주공학과 우주기술융합연구실)
  • Received : 2015.08.24
  • Accepted : 2015.12.14
  • Published : 2016.06.30
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Abstract

In this study, we proposed a water rocket CULV-1 (Chosun University Launch Vehicle-1). Unlike a conventional water rocket, CULV-1 can perform the booster rocket, fairing, and payload separation like an actual launch vehicle and also the imaging data acquisition. The conceptual and critical design of the proposed CULV-1 have been performed considering the operation characteristics. The verification tests have been performed from subsystem to system level in accordance with the established test specifications and verification procedures. Through the final launch test of the flight model, we have verified the design effectiveness of the proposed separation mechanisms for water rocket applications and the mission requirements of the CULV-1 also have been complied.

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References

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