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The Development of Air-based Space Launch Vehicle for small satellites

초소형위성 발사를 위한 공중기반 우주발사체 발전방안

  • Cho, Taehwan (Defense Policy Research Center, Korea National Defense University) ;
  • Lee, Soungsub (Department of Aerospace System Engineering, Sejong University)
  • 조태환 (국방대학교 국방정책연구센터) ;
  • 이성섭 (세종대학교 항공시스템공학과)
  • Received : 2021.07.15
  • Accepted : 2021.08.20
  • Published : 2021.08.31

Abstract

The end of the ROK-U.S. missile guidelines opened up the possibility of developing space launch vehicles for various platforms based on air and sea. In particular, the air-based space launch vehicle is an essential space power projection capability compared to the ground-based space launch vehicle in consideration of the geographical location of the Korean Peninsula, such as the deployment of various satellite orbits and the timely launch of satellite. In addition, compared to the ground-based launch vehicle, the cost reduction effect is large, and it has the merit of energy gain because it can be launched with the advantage of the aircraft's altitude and speed. Therefore, in this paper, the necessity of air-based space launch vehicle in the strategic environment of the Korean Peninsula is clearly presented, and through technology trend analysis of various air launch vehicle, the three methods are proposed to have the most efficient air-based space launch vehicle capability in the Korean situation.

한미 미사일 지침 종료를 계기로 공중, 해상기반의 다양한 플랫폼에 의한 우주발사체 개발 가능성이 열렸다. 특히, 공중기반 우주발사체는 지상기반 우주발사체 대비 다양한 궤도 운용, 적시적인 위성발사 등 한반도의 지리적 위치를 고려할 때 필수적인 우주전력투사 능력이다. 또한, 지상기반 발사체 대비 비용절감 효과가 크고, 항공기의 고도, 속도의 이점으로 발사할 수 있어 에너지 이득의 장점이 있다. 따라서 본 논문에서는 한반도의 전략적 환경하에서 공중기반 우주발사체의 필요성을 명확히 제시하고, 다양한 공중발사체에 대한 기술동향 분석을 통해서 현재의 우리나라 상황에서 가장 효율적으로 공중기반 우주발사체 능력을 확보할 수 있는 3가지 방안을 제시한다.

Keywords

Acknowledgement

본 연구는 세종대학교 미래전략연구의 일환으로 산학협력단의 연구회지원사업으로 수행된 연구입니다.

References

  1. J. I. Kim, "South Korea's missile deterrence strategy after Moon Jae-in administration's missile guideline amendment," Strategic Studies, Vol. 26, No. 1, pp. 163-198, 2019. https://doi.org/10.46226/jss.2019.03.26.1.163
  2. S. Y. Park, "Microsatellite System: A study on operation options for air-launch vehicles," Yonsei University, Seoul: Korea, 2019.
  3. S. S. Lee and S. W. Choi, "A plan to establish a Korean microsatellite system focusing on the defense reform task to equip rapid response capabilities," Aerospace Research, Vol. 6, pp. 139-165, 2019.
  4. The introduction of ALASA [Internet]. Available: https://www.darpa.mil/program/airborne-launch-assist-space-access
  5. J. W. Lee and B. K. Park, "Development and prospect of air launch vehicle," Journal of the Korean Society for Aeronautical & Space Sciences, Vol. 32, No. 3, pp. 124-130, 2004. https://doi.org/10.5139/JKSAS.2004.32.3.124
  6. The introduction of Virgin Orbit Launch One [Internet]. Available: https://virginorbit.com/launch/
  7. DARPA and NASA, "Report of the horizontal launch study," 2011.
  8. Orbital ATK, "Pegasus user's guide, release 8.0," 2015.
  9. Virgin Orbit, "Launcher One service guide, Version 1.1," 2018.
  10. K. Okamura, Y. Noguchi, S. Matsuda, T. Fuji, H. Kanayama, and J. Wallace, "ALSET-Japanese Air Launch System Ground Tests and Applications," 29th Annual AIAA/USU Conference on Small Satellites, pp. 20. 2015.
  11. M. Sarigul-Klijn, N. Sarigul-Klijn, G. Hudson, B. McKinney, B. Menzel, and E. Grabow, "Trade studies for air launching a small launch vehicle from a cargo aircraft." in 43rd AIAA Aerospace Sciences Meeting and Exhibit pp. 621. 2005.
  12. T. Arime, "An overview of air launch system and baseline sequence based on flight analysis," Space Works Enterprises Inc. 2015.
  13. J. W. Lee and J. Y. Hwang, "Concept plan of micro air-launch space vehicle mirinae-1," Korea Aerospace Academic Journal, Vol. 29, No. 2, pp.117-124, 2001.
  14. C. Park, "Prospectors for launch system development in Korea," The First International Aerospace Technomart, pp.79-104, 1996.
  15. S. S. Lee and T. H. Cho, "A Study on the Development of Air Launch Vehicle using Combat Aircraft," in 2021 Proceeding of the Journal of the Korean Society for Aeronautical & Space Sciences, pp. 378-379, 2021. 7.