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