Influence of Azimuthally Nonuniform Propellant Flow Rate on Thrust Vector and Discharge Current Oscillation in a Hall Thruster
Authors:
- Yasuhiro FukushimaYFYasuhiro Fukushima
- Shigeru YokotaSYShigeru Yokota
- Kimiya KomurasakiKKKimiya Komurasaki
- Yoshihiro ArakawaYAYoshihiro Arakawa
- 1 January 2009
- journal article
- Published by Japan Society for Aeronautical and Space Sciences in TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, SPACE TECHNOLOGY JAPAN
- Vol. 7 (ists26) , Pb_41-Pb_45