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
262017
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
152018
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
132017
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
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
62014
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
52019
Investigation of Regression Characteristics under Relatively High-Pressure in Axial-Injection End-Burning Hybrid Rockets
Y Saito, M Kimino, A Tsuji, Y Okutani, H Yasukochi, K Soeda, H Nagata
53rd AIAA/SAE/ASEE Joint Propulsion Conference, 4985, 2017
52017
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
52016
Comprehensive Data Reduction for N2O/HDPE Hybrid Rocket Motor Performance Evaluation
L Kamps, K Sakurai, Y Saito, H Nagata
Aerospace 6 (4), 45, 2019
42019
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, 2017
42017
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
42017
Experimental and Analytical Investigation of Effect of Pressure on Regression Rate of Axial-Injection End-Burning Hybrid Rockets
Y Saito, T Yokoi, H Nagata, H Yasukochi, K Soeda, T Totani, M Wakita
52nd AIAA/SAE/ASEE Joint Propulsion Conference, 4752, 2016
42016
Investigation of Graphite Nozzle Erosion in Hybrid Rockets Using O2/C2H4
LT Kamps, S Hirai, K Sakurai, T Viscor, Y Saito, R Guan, H Isochi, ...
2018 Joint Propulsion Conference, 4531, 2018
32018
Investigation of the Throttling Characteristics of Axial-Injection End-Burning Hybrid Rockets
Y Saito, T Yokoi, A Tsuji, K Omura, H Yasukochi, G Soeda, T Totani, ...
Journal of the Japan Society for Aeronautical and Space Sciences 65 (4), 157-167, 2017
32017
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
2*2016
Determinant based Fast Greedy Optimization on Sparse Sensor Selection
Y Saito, K Yamada, T Nonomura, K Asai, D Tsubakino, Y Sasaki
Bulletin of the American Physical Society 64, 2019
12019
Data-driven Vector-measurement-sensor Selection based on Greedy Algorithm for Particle-image-velocimetry Measurement
Y Saito, T Nonomura, K Nankai, K Asai, Y Sasaki, D Tsubakino
arXiv preprint arXiv:1906.00778, 2019
12019
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
12018
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
12018
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, 1-12, 2020
2020
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