Yuji Saito
Yuji Saito
確認したメール アドレス: aero.mech.tohoku.ac.jp - ホームページ
タイトル
引用先
引用先
Verification firings of end-burning type hybrid rockets
H Nagata, H Teraki, Y Saito, R Kanai, H Yasukochi, M Wakita, T Totani
Journal of propulsion and power 33 (6), 1473-1477, 2017
302017
Fuel regression characteristics of a novel axial-injection end-burning hybrid rocket
Y Saito, T Yokoi, H Yasukochi, K Soeda, T Totani, M Wakita, H Nagata
Journal of Propulsion and Power 34 (1), 247-259, 2018
25*2018
Method for determining nozzle-throat-erosion history in hybrid rockets
L Kamps, Y Saito, R Kawabata, M Wakita, T Totani, Y Takahashi, ...
Journal of propulsion and power 33 (6), 1369-1377, 2017
162017
Mission to Earth–Moon Lagrange point by a 6U CubeSat: EQUULEUS
R Funase, S Ikari, K Miyoshi, Y Kawabata, S Nakajima, S Nomura, ...
IEEE Aerospace and Electronic Systems Magazine 35 (3), 30-44, 2020
142020
High pressure fuel regression characteristics of axial-injection end-burning hybrid rockets
Y Saito, M Kimino, A Tsuji, Y Okutani, K Soeda, H Nagata
Journal of Propulsion and Power 35 (2), 328-341, 2019
11*2019
Investigation of Throttling Response Characteristics of Axial-Injection End-Burning Hybrid Rockets
Y Saito, M Kimino, A TSUJI, K Omura, H Yasukochi, K Soeda, T Totani, ...
Transactions of the Japan Society for Aeronautical and Space Sciences …, 2018
82018
端面燃焼式ハイブリッドロケットの推力制御特性に関する研究
齋藤勇士, 横井俊希, 津地歩, 尾村和信, 安河内裕之, 添田建太郎, ...
日本航空宇宙学会論文集 65 (4), 157-167, 2017
7*2017
Evaluations of Data Reduction Methods for Hybrid Rockets
H Nagata, Y Saito, T Ishiyama, Y Inaba, M Wakita, T Totani
Proceedings of the 65th International Astronautical Congress, Toronto, ON …, 2014
72014
Investigation of Graphite Nozzle Erosion in Hybrid Rockets Using Oxygen/High-Density Polyethylene
L Kamps, S Hirai, K Sakurai, T Viscor, Y Saito, R Guan, H Isochi, N Adachi, ...
Journal of Propulsion and Power 36 (3), 423-434, 2020
6*2020
Comprehensive Data Reduction for N2O/HDPE Hybrid Rocket Motor Performance Evaluation
L Kamps, K Sakurai, Y Saito, H Nagata
Aerospace 6 (4), 45, 2019
62019
Estimation of Hybrid Rocket Nozzle Throat Erosion History
Y SAITO, T UEMATSU, H ISOCHI, M WAKITA, T TOTANI, H NAGATA
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES …, 2016
62016
Determinant-based Fast Greedy Sensor Selection Algorithm
Y Saito, T Nonomura, K Yamada, K Asai, Y Sasaki, D Tsubakino
arXiv preprint arXiv:1911.08757, 2019
42019
The Accuracy of Reconstruction Techniques for Determining Hybrid Rocket Fuel Regression Rate
Y Saito, LT Kamps, K Komizu, D Bianchi, F Nasuti, H Nagata
2018 Joint Propulsion Conference, 4923, 2018
42018
Investigation of axial-injection end-burning hybrid rocket motor regression
Y Saito, T Yokoi, L Neumann, H Yasukochi, K Soeda, T Totani, M Wakita, ...
Advances in Aircraft and Spacecraft Science 4 (3), 281-296, 2017
42017
Data-driven Vector-measurement-sensor Selection based on Greedy Algorithm
Y Saito, T Nonomura, K Nankai, K Yamada, K Asai, Y Tsubakino, ...
IEEE Sensors Letters 4, 2020
32020
Fast Greedy Optimization of Sensor Selection in Measurement with Correlated Noise
K Yamada, Y Saito, K Nankai, T Nonomura, K Asai, D Tsubakino
arXiv preprint arXiv:1912.01776, 2019
22019
Feasibility study on sparse processing particle image velocimetry
N Kanda, K Nankai, Y Saito, T Nonomura, K Asai
APS, Q11. 008, 2019
22019
Investigation of Regression Rate under High-Pressure in Axial-Injection End-Burning Hybrid Rockets
Y Okutani, Y Saito, M Kimino, A Tuji, K Soeda, H Nagata
2018 Joint Propulsion Conference, 4529, 2018
22018
Verification of the Throttling characteristics of Axial-Injection End-Burning type Hybrid Rockets
Y Saito, T Yokoi, H Yasukochi, K Soeda, T Totani, M Wakita, H Nagata
67th International Astronautical Congress, Guadalajara, Mexico, 2016
22016
Experimental Investigation of the Continuous Transition of Flame-Spreading near the Blow-Off Limit
K Komizu, Y Saito, A Tsuji, H Nagata
Journal of Combustion 2020, 2020
12020
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