Annular Hall Thruster with High Anode Efficiency

Cited 0 time in webofscience Cited 0 time in scopus
  • Hit : 147
  • Download : 0
We introduce an annular Hall thruster with a convex magnetic field structure inside a discharge channel by utilizing an internal magnetic circuit rather than a trim coil. The convex magnetic field exhibited a strong component parallel to channel walls except a few millimeters of channel exit. The discharge demonstrated that discharge current was maintained constantly by increasing the anode voltage up to 500 V. Without the magnetic field tailoring, the discharge current increased continuously with the anode voltage, and as a result, a reasonable power efficiency was not obtained. On the other hand, our optimized magnetic field condition exhibited an outstanding operation result: 53.1% anode efficiency, 22 mN thrust, and 2275 s specific impulse at approximately 460 W anode power.
Publisher
American Institute of Aeronautics and Astronautics
Issue Date
2016-07-25
Language
English
Citation

52nd AIAA/SAE/ASEE Joint Propulsion Conference

DOI
10.2514/6.2016-4623
URI
http://hdl.handle.net/10203/274693
Appears in Collection
NE-Conference Papers(학술회의논문)
Files in This Item
There are no files associated with this item.

qr_code

  • mendeley

    citeulike


rss_1.0 rss_2.0 atom_1.0