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日本航空宇宙學會論文集 = Journal of the Japan Society for Aeronautical and Space Sciences, v.54 no.629 = no.629, 2006년, pp.242 - 249
北川 幸樹 (東京都立科学) , 湯浅 (技術大学) , 三郎 (大学)
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We have proposed a swirling oxidizer type hybrid rocket engine. In this paper, liquid oxygen (LOX) was used as oxidizer. Combustion tests of a hybrid rocket engine with a swirling LOX flow were conducted by changing the swirl strength. Ignition was rapid and reliable, and combustion of PMMA with swi...
10.2514/6.1997-2804 1) Boardman, T. A., Abel, T. M., Claflin, S. E. and Shaeffer, C. W.: Design and Test Planning for a 250-klbf-Thrust Hybrid Rocket Motor under the Hybrid Propulsion Demonstration Program, AIAA Paper 97-2804, 1997.
10.2514/6.2001-4503 2) Karabeyoglu, M. A., Cantwell, B. J. and Altman, D.: Development and Testing of Paraffin-Based Hybrid Rocket Fuels, AIAA Paper 2001-4503, 2001.
10.2514/6.2002-3576 3) Risha, G., Boyer, E., Wehrman, R. and Kuo, K.: Performance Comparison of HTPB-Based Solid Fuels Containing Nano-Sized Energetic Powder in a Cylindrical Hybrid Rocket Motor, AIAA Paper 2002-3576, 2002.
4) Nagata, H., Watanabe, M., Sanda, T., Satori, S., Aoki, Y., Kudo, I., Akiba, R. and Kudo, I.: Improvement of Fuel Regression Rate by Impinging Jet for High Thrust Hybrid Rocket Motors, Proceedings of the International Symposium on Space Technology and Science, 2000, pp. 121-126.
10.2514/6.1999-2322 5) Yuasa, S., Shimada, O, Imamura, T., Tamura, T. and Yamoto, K.: A Technique for Improving the Performance of Hybrid Rocket Engines, AIAA Paper 99-2322, 1999.
6) Tamura, T., Yuasa, S. and Yamamoto, K.: Effects of Swirling Oxidizer Flow on Fuel Regression Rate of Hybrid Rockets, AIAA Paper 99-2323, 1999.
10.2514/6.2001-3537 7) Yuasa, S., Yamamoto, K., Hachiya, H., Kitagawa, K. and Oowada, Y.: Development of a Small Sounding Hybrid Rocket with a Swirling-Oxidizer-Type Engine, AIAA Paper 2001-3537, 2001.
8) Kitagawa, K., Hachiya, H., Ymamoto, K. and Yuasa, S.: Development and Experimental Launch of a Small Hybrid Rocket with a Swirling-Oxidizer Type Engine, ISTS 2002-g-20, 2002.
9) Beer, J. M. and Chigier, N. A.: Combustion Aerodynamics, Applied Science Pub., London, 1972, p. 109.
10) Lefevre, H.: Atomization and Sprays, Taylor & Francis, Bristol, 1989, pp. 296-298.
11) Sutton, G. P.: Rocket Propulsion Elements, Sixth Edition, John Wiley & Sons, New York, 1996, p. 268.
12) 木村逸？:ロケット工？,養賢堂,東京,1993, pp. 363-378.
10.2514/6.1993-2553 13) Greiner, B. and Frederick, R. A. Jr.: Hybrid Rocket Instability, AIAA Paper 93-2553, 1993.
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