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Kohei Ozawa
Kohei Ozawa
University of Tokyo
Aerospace engineering
Rocket engine
Engineering
Combustion
Physics
7
Papers
27
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Hybrid Rocket Firing Experiments at Various Axial–Tangential Oxidizer-Flow-Rate Ratios
2019
Journal of Propulsion and Power
Kohei Ozawa
Koki Kitagawa
Shigeru Aso
Toru Shimada
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Citations (9)
Effects of O/F Shifts on Flight Performances of Vertically Launched Hybrid Sounding Rockets
2017
Kohei Ozawa
Toru Shimada
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Citations (6)
Static burning tests on a bread board model of altering-intenisty swirling-oxidizer-flow-type hybrid rocket engine
2016
Kohei Ozawa
Tomoaki Usuki
Genki Mishima
Koki Kitagawa
Masato Yamashita
Masato Mizuchi
Koki Katakami
Yudai Maji
Shigeru Aso
Yasuhiro Tani
Yutaka Wada
Toru Shimada
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Citations (3)
Linear Combustion Stability Analysis of Uni-directional Vortex Injection Hybrid Rocket Engines
2014
Kohei Ozawa
Toru Shimada
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Citations (1)
A Theoretical Study of Combustion Stability in Vortex Injection Hybrid Rocket Engine
2014
Transactions of The Japan Society for Aeronautical and Space Sciences, Space Technology Japan
Kohei Ozawa
Toru Shimada
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