시스템엔지니어링학술지 (Journal of the Korean Society of Systems Engineering)

  • 제1권1호
  • /
  • Pages.67-72
  • /
  • 2005
  • /
  • 1738-480X(pISSN)
  • /
  • 2288-3592(eISSN)
한국시스템엔지니어링학회 (The Korean Society of Systems Engineering)
권호 표지

초음속 공중발사로켓의 임무형상 최적설계

Optimal Mission Design of the Supersonic Air-launching Rocket

  • 최영창 (건국대학교 항공우주공학과) ;
  • 이재우 (건국대학교 항공우주공학과) ;
  • 변영환 (건국대학교 항공우주공학과)
  • Choi, Youngchang (Department of Aerospace Engineering, Konkuk University) ;
  • Lee, Jaewoo (Department of Aerospace Engineering, Konkuk University) ;
  • Byun, Yunghwan (Department of Aerospace Engineering, Konkuk University)
  • 발행 : 2005.01.31
PDF 다운로드
⟨ 이전 논문 다음 논문 ⟩

초록

Design and optimization study has been performed to obtain a supersonic air.launching mission for the nanosat launcher. Given mission is to launch 10kg payload to target orbit of $700km{\times}700km$. Additional design constraints are imposed by the mother plane. After the required velocity is obtained, the stag ing optimization is carried out. Serial analyses for the propulsion system and aerodynamics are performed then, the rocket trajectory optimization has been carried out. After several mission design and optimization iterations, the optimized mission which satisfies the mission target is obtained. Total weight of the three-staged air-launching rocket is 1231.4kg and the payload weight is 10 kg.

키워드