| 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 | 39 | 2017 |
| 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 | 27 | 2020 |
| Hybrid rockets as post-boost stages and kick motors L Kamps, S Hirai, H Nagata Aerospace 8 (9), 253, 2021 | 25 | 2021 |
| Comprehensive Data Reduction for N2O/HDPE Hybrid Rocket Motor Performance Evaluation L Kamps, K Sakurai, Y Saito, H Nagata Aerospace 6 (4), 45, 2019 | 24 | 2019 |
| 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 | 20 | 2018 |
| Numerical analysis of nozzle erosion in hybrid rockets and comparison with experiments D Bianchi, MT Migliorino, M Rotondi, L Kamps, H Nagata Journal of Propulsion and Power 38 (3), 389-409, 2022 | 18 | 2022 |
| Numerical and experimental investigation of nozzle thermochemical erosion in hybrid rockets D Bianchi, LT Kamps, F Nasuti, H Nagata 53rd AIAA/SAE/ASEE Joint Propulsion Conference, 4640, 2017 | 14 | 2017 |
| Large-scale CAMUI type hybrid rocket motor scaling, modeling, and test results T Viscor, L Kamps, K Yonekura, H Isochi, H Nagata Aerospace 9 (1), 1, 2021 | 12 | 2021 |
| Fuel regression characteristics of axial-injection end-burning hybrid rocket using nitrous oxide R Okuda, K Komizu, A Tsuji, T Miwa, M Fukada, S Yokobori, K Soeda, ... Journal of propulsion and power 38 (5), 759-770, 2022 | 11 | 2022 |
| Fuel regression characteristics in hybrid rockets using nitrous oxide/high-density polyethylene S Ito, L Kamps, H Nagata Journal of propulsion and power 37 (2), 342-348, 2021 | 11 | 2021 |
| Evaluation of the Thermal Onset of Graphite Nozzle Erosion S Ito, LT Kamps, S Yoshimal, H Nagata AIAA Propulsion and Energy 2020 Forum, 3755, 2020 | 11 | 2020 |
| Development of N2O/HDPE hybrid rocket for microsatellite propulsion L Kamps, P Molas-Roca, E Uchiyama, T Takanashi, H Nagata 70th International Astronautical Congress (IAC-19), Washington DC, United …, 2019 | 11 | 2019 |
| Investigation of Graphite Nozzle Erosion in Hybrid Rockets Using N2O/HDPE LT Kamps, K Sakurai, K Ozawa, H Nagata AIAA Propulsion and Energy 2019 Forum, 4264, 2019 | 10 | 2019 |
| 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 | 8 | 2018 |
| GEO-X (GEOspace x-ray imager) Y Ezoe, R Funase, H Nagata, Y Miyoshi, S Kasahara, H Nakajima, ... Space telescopes and instrumentation 2020: Ultraviolet to gamma ray 11444 …, 2020 | 7 | 2020 |
| One-dimensional modelling of the nozzle cooling with cryogenic oxygen flowing through helical channels in a hybrid rocket G Gallo, L Kamps, S Hirai, C Carmicino, H Nagata Acta Astronautica 210, 176-196, 2023 | 6 | 2023 |
| Numerical analysis of nozzle heating and erosion in hybrid rockets and comparison with experiments D Bianchi, MT Migliorino, M Rotondi, LT Kamps, H Nagata AIAA Propulsion and Energy 2020 Forum, 3767, 2020 | 6 | 2020 |
| Fuel regression characteristics of CAMUI type hybrid rocket using nitrous oxide Y Nobuhara, LT Kamps, H Nagata AIAA Propulsion and Energy 2021 Forum, 3521, 2021 | 5 | 2021 |
| Development of safe, low-cost, re-ignitable rocket ignition system S Hirai, LT Kamps, H Nagata AIAA Propulsion and Energy 2021 Forum, 3509, 2021 | 5 | 2021 |
| GEO-X (GEOspace x-ray imager) Y Ezoe, R Funase, H Nagata, Y Miyoshi, H Nakajima, I Mitsuishi, ... Space Telescopes and Instrumentation 2022: Ultraviolet to Gamma Ray 12181 …, 2022 | 4 | 2022 |
Yuji SaitoTohoku University確認したメール アドレス: tohoku.ac.jp
