한국항공우주학회지 (Journal of the Korean Society for Aeronautical & Space Sciences)

  • 제30권3호
  • /
  • Pages.155-163
  • /
  • 2002
  • /
  • 1225-1348(pISSN)
  • /
  • 2287-6871(eISSN)
한국항공우주학회 (The Korean Society for Aeronautical and Space Sciences)
권호 표지
DOI QR코드

DOI QR Code

특집 : 하이브리드 로켓의 개념 소개 및 연구개발 동향 분석 2 - 대학 및 아마추어 -

Special Issue : Recent Progress in Research and Development of Hybrid Rocket / PART 2 . - Research activities of University and Amateurs -

  • 발행 : 2002.05.31
PDF 다운로드
⟨ 이전 논문 다음 논문 ⟩

초록

키워드

참고문헌

  1. Uni. of Arkansas, http://hybrid.ualr.edu/
  2. R. Shank, M. K. Hudson, "A Labscale Hybrid Rocket Motor for Instrumentaion Studies", Journal of Pyrotechnics, Issue 11, Summer 2000.
  3. Uni. of Arizona, http://www.ame.arizona.edu/
  4. NASA Brief NPO-20195, http://www.nasatech.com/
  5. NASA Brief NPO-20387, http://www.nasatech.com/
  6. Uni. of Purdue, http://roger.ecn.purdue.edu/
  7. Penn. State Uni., http://www.hpcl.psu.edu/
  8. 김선진, 한재섭, 김유, 지평삼, 조석, “GO2/HTPB를 사용하는 Hyrid Rocket의 추진제 침투율에 관한 연구”, 한국추진공학회지, KSPE 97-1-2.
  9. Dr. Kuo, http://www.me.psu.edu/kuo/html/
  10. IPT, htp://www.eb.uah.edu/ipt/
  11. Paxton, J. Aehenbch, Patterson, P. Pyburn, J., Thomas, M., Federick, R. A.,Jr, "Design of Turbopump-Fed Hybrid Launch Vehicle", AIAA Paper 93-2549.
  12. LaSarge, P. A., Ford, S. I., Fredrick, R. A., "Conceptual Design of Hybrid Rocket Powered Upper Stage (HRPUS) Demonstration", AIAA Paper 96-2841.
  13. Unit IV, http://www.et.byu.edu/~unitiv/
  14. UoSAT, http://ee.surrey.ac.uk/
  15. SSTL, http://www.sstl.co.uk/
  16. "Orbit Transfer of Small Space Craft with a Vortex Flow Hybrid Rocket", ISIS 00 (Morioka , Japan 28 May-4 June 00)
  17. Y. Aoki, R. Akiba, K. Seiyu, H. Naguta, S. Satai, "Development of the Staged Combustion Hybrid Rocket", IAF-01-S.2.08
  18. K. Mizobata, H. Nagata, K. Ioth, R. Akiba, S. Stari, "A Reusable Hybrid Rocket System: Concept Outlines and Feasibility Winged Flight", ISTS-00-g-4
  19. AspireSpace, http://www.cartman.clara.net
  20. MARS, http://www.mars.org.uk/
  21. HALO, http://hiwaay.net/~hal5/HALO/
  22. NERO, htp://www.nerorockets.org/

피인용 문헌

  1. Experimental Study on the Static Stability of a Sounding Rocket Model in the Supersonic Wind Tunnel vol.38, pp.9, 2010, https://doi.org/10.5139/JKSAS.2010.38.9.856