Characterization of a Liquid-propellant Pulsed Plasma Thruster Using Various Nozzle Configurations-Reference-Cited by-同舟云学术

Characterization of a Liquid-propellant Pulsed Plasma Thruster Using Various Nozzle Configurations

Published:2019 Issue:4 Volume:62 Page:184-191
ISSN:0549-3811
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:en
Short-container-title:Trans. Japan Soc. Aero. S Sci.

Author:

MIYAGI Kinya¹,KAKAMI Akira²,TACHIBANA Takeshi¹

Affiliation:

1. Department of Mechanical Engineering, Kyushu Institute of Technology

2. Department of Mechanical Design Systems Engineering, University of Miyazaki

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://www.jstage.jst.go.jp/article/tjsass/62/4/62_T-17-101/_pdf

Reference18 articles.

1. 1) Burton, R. L. and Turchi, P. J.: Pulsed Plasma Thruster, J. Propul. Power, 14, 5 (1998), pp. 716–735. doi:10.2514/2.5334

2. 2) BUSEK Co. Inc.: BmP-220 Micro-Pulsed Plasma Thruster, 2016, http://www.busek.com/index_htm_files/70008502F.pdf

3. 3) Ciaralli, S., Coletti, M., and Gabriel, S. B.: Qualification of a Pulsed Plasma Thruster for CubeSat Propulsion (PPTCUP), 34th International Electric Propulsion Conference, IEPC-2015-208, 2015.

4. 4) Masui, H., Cho, M., and Vinh, T. Q.: Design, Development and Testing of Structure and Thermal Subsystem of AOBA-VELOX III, 35th International Electric Propulsion Conference, ISTS2017-f-082, 2017.

5. 5) Enomoto, K., Fujita, R., Ryuho, K., Ono, K., Morikawa, N., Tahara, H., Takada, K., and Wakizono, T.: Development of Coaxial Pulsed Plasma Thruster Systems for Powered Flight Onboard the Osaka Institute of Technology 2nd PROITERES Nano-Satellite, 35th International Electric Propulsion Conference, 2017-b-04, 2017.

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