Art

J-GLOBAL ID：202002245725286025   Reference number：20A0871905

Fuel regression behavior of swirling-injection end-burning hybrid rocket engine

旋回噴射端燃焼ハイブリッドロケットエンジンの燃料後退挙動

Author (3)： SAKURAI Takashi (Department of Aeronautics and Astronautics, Tokyo Metropolitan University) ,  OISHIGE Yuya (Graduate School of Aeronautics and Astronautics, Tokyo Metropolitan University) ,  SAITO Kazuyuki (Graduate School of Aeronautics and Astronautics, Tokyo Metropolitan University)
Material： Journal of Fluid Science and Technology (Web)  (J Fluid Sci Technol (Web))
Volume： 14  Issue： 3  Page： JFST0025(J-STAGE)  Publication year： 2019 
JST Material Number： U0022A  ISSN： 1880-5558  Document type： Article
Article type： 原著論文  Country of issue： Japan (JPN)  Language： ENGLISH (EN)

Thesaurus term： *rocket engine ,  fuel ,  paraffin wax ,  mass flow rate ,  particle size(diameter) ,  *unstable combustion ,  melting point ,  heat transfer ,  oxidizing agent ,  ratio ,  actuator
Semi thesaurus term： *hybrid rocket engine ,  Oxygen gas ,  regression velocity ,  酸化剤対燃料比

Author keywords (4)： Swirling-injection ,  End-burning ,  Fuel regression rate ,  Hybrid rocket engine

JST classification (2)： Rocket engines  (PB02050J) ,  Combution equipment in general  (PA03010V)

Reference (18)：

• Batterson, J.W., Majdalani, J., Sidewall Boundary Layers of the Bidirectional Vortex, Journal of Propulsion and Power, Vol.26, No.1 (2010), pp.102-112, https://doi.org/10.2514/1.40442.
• Beer, J.M., and Chigier, N.A., “Swirling Flows,” Combustion Aerodynamics, Applied Science Publishers, London, 1972, pp.100-146.
• Chiaverini, M.J., Review of Solid-Fuel Regression Rate Behavior in Classical and Nonclassical Hybrid Rocket Motors., Ch. 2 of Fundamentals of Hybrid Rocket Combustion and Propulsion, Ed. Chiaverini, M.J. and Kuo, K.K., AIAA Progress in Astronautics and Aeronautics Vol. 218 (2007), pp.101-105.
• Haag, G., Sweeting, M., Richardson, G., An Alternative Geometry Hybrid Rocket for Spacecraft Orbit Transfer Manoeuvers, 51^st International Astronautical Congress (2000), IAF Paper 00-W.2.07.
• Hayashi, D., Sakurai, T., A Fundamental Study of An End-Burning Swirling-Flow Hybrid Rocket Engine Using Low Melting Temperature Fuels, 51st AIAA Joint Propulsion Conference (2015), AIAA 2015-4138.

Terms in the title (7)： 旋回 ,  噴射 ,  燃焼 ,  ハイブリッドロケットエンジン ,  燃料 ,  後退 ,  挙動