Development of thrust stand for low impulse measurement from microthrusters H Koizumi, K Komurasaki, Y Arakawa Review of scientific instruments 75 (10), 3185-3190, 2004 | 139 | 2004 |
Plasma generation using high-power millimeter-wave beam and its application for thrust generation Y Oda, K Komurasaki, K Takahashi, A Kasugai, K Sakamoto Journal of Applied Physics 100 (11), 2006 | 123 | 2006 |
Discharge current oscillation in Hall thrusters N Yamamoto, K Komurasaki, Y Arakawa Journal of propulsion and power 21 (5), 870-876, 2005 | 115 | 2005 |
Two-dimensional numerical model of plasma flow in a Hall thruster K Komurasaki, Y Arakawa Journal of Propulsion and Power 11 (6), 1317-1323, 1995 | 112 | 1995 |
Analysis of atmosphere-breathing electric propulsion T Schönherr, K Komurasaki, F Romano, B Massuti-Ballester, G Herdrich IEEE Transactions on Plasma Science 43 (1), 287-294, 2014 | 95 | 2014 |
Propulsive impulse measurement of a microwave-boosted vehicle in the atmosphere T Nakagawa, Y Mihara, K Komurasaki, K Takahashi, K Sakamoto, T Imai Journal of spacecraft and rockets 41 (1), 151-153, 2004 | 89 | 2004 |
Plasma acceleration processes in an ablative pulsed plasma thruster H Koizumi, R Noji, K Komurasaki, Y Arakawa Physics of plasmas 14 (3), 2007 | 87 | 2007 |
Initial flight operations of the miniature propulsion system installed on small space probe: PROCYON H Koizumi, H Kawahara, K Yaginuma, J Asakawa, Y Nakagawa, ... Transactions of the Japan Society for Aeronautical and Space Sciences …, 2016 | 83 | 2016 |
Energy transfer from a laser pulse to a blast wave in reduced-pressure air atmospheres K Mori, K Komurasaki, Y Arakawa Journal of Applied Physics 95 (11), 5979-5983, 2004 | 80 | 2004 |
Kinetic particle simulation of discharge and wall erosion of a Hall thruster S Cho, K Komurasaki, Y Arakawa Physics of Plasmas 20 (6), 2013 | 73 | 2013 |
Engineering model of the miniature ion propulsion system for the nano-satellite: HODOYOSHI-4 H Koizumi, K Komurasaki, J Aoyama, K Yamaguchi Transactions of the Japan Society for Aeronautical and Space Sciences …, 2014 | 66 | 2014 |
Thrust performance of microwave rocket under repetitive-pulse operation Y Oda, T Shibata, K Komurasaki, K Takahashi, A Kasugai, K Sakamoto Journal of Propulsion and Power 25 (1), 118-122, 2009 | 64 | 2009 |
Influence of the focusing f number on the heating regime transition in laser absorption waves K Mori, K Komurasaki, Y Arakawa Journal of applied Physics 92 (10), 5663-5667, 2002 | 64 | 2002 |
Numerical analysis of azimuthal rotating spokes in a crossed-field discharge plasma R Kawashima, K Hara, K Komurasaki Plasma Sources Science and Technology 27 (3), 035010, 2018 | 60 | 2018 |
Characteristics of plasma properties in an ablative pulsed plasma thruster T Schönherr, F Nees, Y Arakawa, K Komurasaki, G Herdrich Physics of Plasmas 20 (3), 2013 | 60 | 2013 |
Performance characterization of a miniature microwave discharge ion thruster operated with water Y Nakagawa, H Koizumi, H Kawahara, K Komurasaki Acta Astronautica 157, 294-299, 2019 | 59 | 2019 |
Three-dimensional particle-in-cell simulation of a miniature plasma source for a microwave discharge ion thruster Y Takao, H Koizumi, K Komurasaki, K Eriguchi, K Ono Plasma sources science and technology 23 (6), 064004, 2014 | 59 | 2014 |
Pulsed Plasma Thrusters: a worldwide review and long yearned classification P Molina-Cabrera, G Herdrich, M Lau, S Fausolas, T Schoenherr, ... Proceedings of 32nd International Electric Propulsion Conference, 2011 | 55 | 2011 |
Fundamental ground experiment of a water resistojet propulsion system: AQUARIUS installed on a 6U CubeSat: EQUULEUS J Asakawa, H Koizumi, K Nishii, N Takeda, M Murohara, R Funase, ... Transactions of the Japan Society for Aeronautical and Space Sciences …, 2018 | 54 | 2018 |
Design and performance of liquid propellant pulsed plasma thruster A Kakami, H Koizumi, K Komurasaki, Y Arakawa Vacuum 73 (3-4), 419-425, 2004 | 53 | 2004 |