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J-GLOBAL ID:202102272134262094   Reference number:21A0057423

Demonstration Study of Pulse Detonation Engine System for Sounding Rocket S-520-31

観測ロケットS-520-31号機搭載用パルスデトネーションエンジンのシステム実証研究
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Volume: 64th  Page: ROMBUNNO.2K09  Publication year: 2020 
JST Material Number: S0277B  ISSN: 1884-1945  Document type: Proceedings
Article type: 原著論文  Country of issue: Japan (JPN)  Language: JAPANESE (JA)
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Rocket engines 
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Reference (9):
  • Piotr W.:Detonative propulsion, Proceedings of the Combustion Institute Vol. 34, Issue 1, pp. 125-158, 2013.
  • 遠藤琢磨:デトネーションの熱流体力学 1,2011.
  • Matsuoka, K., Takagi, S., Kasahara, J., Matsuo, A. and Funaki, I.:Validation of pulse-detonation operation in low-ambient-pressure environment, Journal of Propulsion and Power, Vol. 34, No. 1, pp. 116-124, 2018.
  • Takagi, S., Hosono, K., Matsuoka, K., Kasahara, J., Matsuo, A., Funaki, I.:Experimental performance evaluation of 3N-class pulse detonation thruster using liquid purge method, AIAA Paper 2016-0122, 2016.
  • Ninomiya, K.:Handbook of Spacecraft Dynamics and Control from Basic Theories to Application, Baifukan, Tokyo, pp.507-508, 2007.
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