Takashi Sakurai

J-GLOBAL         Last updated: Apr 20, 2019 at 18:29
 
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Name
Takashi Sakurai
Affiliation
Tokyo Metropolitan University

Research Areas

 
 

Published Papers

 
Performance and Regression Rate characteristics of 5-kN SOFT Hybrid Rocket Engine
Sakurai, T., Yuasa, S., Ando, H., Kitagawa, K., Shimada, T.
Journal of Propulsion and Power   33(4) 891-901   Dec 2016   [Refereed]
Development of test facilities for 5-kN-thrust hybrid rocket engines and a swirling-oxidizer-flow-type hybrid rocket engine for technology demonstration
Kitagawa, K., Yuasa, S., Sakurai, T., Hatagaki, S., Shiraishi, N., Ando, H., Yagishita, T., Suzuki, N., Takayama, A., Yui, R., Shimada, T.
International Journal of Energetic Materials and Chemical Propulsion   15(6) 435-451   2016   [Refereed]
Sakurai, T., Yuasa, S., Ono, Y., Honda, T.
Combustion and Flame   160 2497-2506   2013   [Refereed]

Conference Activities & Talks

 
Fuel Regression Behavior of Swirling-Injection End-Burning Hybrid Rocket Engine
Sakurai, T., Oishige, Y., Saito, K.
15th ICFD   7 Nov 2018   
Operating characteristics of gas turbine driven by pulse detonation toward self-sustained operation
Sakurai, T., Takahashi, H., Hirai, Y., Yomo, S.
23rd ISABE   Sep 2017   
Engine Performance of a Swirling-Injection End-Burning Hybrid Rocket Engine using LOX/Paraffin-based Fuel
Saito, K., Oishige, Y., Hayashi, D., Sakurai, T.
30th ISTS   Jun 2017   
Design and Experiment of a LOX Vaporization Nozzle for an A-SOFT Hybrid Rocket Engine
Mizukoshi, T., Takei, T., Sakurai, T.
30th ISTS   Jun 2017   
Fuel Regression Behavior of a Swirling-Injection End-Burning Hybrid Rocket Engine using Paraffin-based Fuels
Oishige, Y., Hayashi, D., Sakurai, T.
52nd AIAA Joint Propulsion Conference, AIAA 2016-4755   Jul 2016