1,000-hours Demonstration of a 6-kW-class Hall Thruster for All-Electric Propulsion Satellite

Author:

FUNAKI Ikkoh12,CHO Shinatora3,SANO Tadahiko2,FUKATSU Tsutomu2,TASHIRO Yosuke4,SHIIKI Taizo4,NAKAMURA Yoichiro4,WATANABE Hiroki5,KUBOTA Kenichi3,MATSUNAGA Yoshiki3,FUCHIGAMI Kenji6

Affiliation:

1. Institute of Space and Astronautical Science, JAXA

2. Space Technology One Directorate, JAXA

3. Research and Development Directorate, JAXA

4. IHI Aerospace

5. Department of Aeronautics and Astronautics, Tokyo Metropolitan University

6. IHI

Publisher

Japan Society for Aeronautical and Space Sciences

Reference46 articles.

1. 1) Goebel, D. M. and Katz, I.: Fundamentals of Electric Propulsion: Ion and Hall Thrusters, JPL Space Science and Technology Series, California, 2008, pp.325-392.

2. 2) Morozov, A. I., and Savelyev, V. V.: Fundamentals of Stationary Plasma Thruster Theory, Review of Plasma Physics, 21 (2000), pp.203-391.

3. 3) Kim, V.: Main Physical Features and Processes Determining the Performance of Stationary Plasma Thrusters, J. Propuls. Power, 14 (1998), pp.736-743.

4. 4) Svitak, A.: Dawn of the All-electric Satellite, Aviation Week, Mar. 16, 2015.

5. 5) Lev, D. R., Emsellem, G. D., and Hallock, A. K.: The Rise of the Electric Age for Satellite Propulsion, New Space, 5 (2017), pp. 4-14.

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