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