RATO(Rocket-Assisted Take Off) 시스템 적용을 위한 하이브리드 로켓 비단공형 연료 그레인 기초 연소특성 연구

Author:

Kim Su Jin,Ko Su Han,Kim Sul Hee,Kim Gyeong Mo,Lee Seong Geun,Han Ye Chan,Moon Hee Jang

Funder

National Research Foundation of Korea

Publisher

The Korean Society for Aviation and Aeronautics

Subject

General Medicine

Reference13 articles.

1. Bettella, A., Moretto, F., Geremia, E., Bellomo, N., Petronio, D., and Pavarin, D., “Development of 20 kN hybrid rocket booster”, 5th European Conference for Aeronautics and Space Sciences, Munich, Germany, 2013

2. Takashi, T., Saburo, Y., and Kengo, Y., “Effects of swirling oxidizer flow on fuel regression rate of hybrid rockets”, 35th Joint Propulsion Conference and Exhibit, 1999, p.2323. 10.2514/6.1999-2323 PMC1905457

3. Hussain, M. M., Siddiqui, B., and Memon, A. “Design and analysis of rocket assisted takeoff high-speed UAV”, 6th International Conference on Aerospace Science and Engineering, 2019.

4. Yuasa, S., Shimada, O., Imamura, T., Tamura, T., and Yamamoto, T., “A technique for improving the performance of hybrid rocket engines”, 35th IAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 1999, p. 2322. 10.2514/6.1999-2322

5. Larson, D. B., “Formulation and Characterization of praffin-based solid fuels containing novel additives for use in hybrid rocket motors”, Master’s Dissertation, Department of Mechanical and Nuclear Engineering, Pennsylvania University, Philadelphia, P.A., U.S.A., 2012.

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