Testing a Helicon Double Layer Thruster Immersed in a Space-Simulation Chamber
Date
Authors
West, Michael
Charles, Christine
Boswell, Roderick
Journal Title
Journal ISSN
Volume Title
Publisher
American Institute of Aeronautics and Astronautics
Abstract
The Helicon Double Layer Thruster, a new magnetoplasma thruster that accelerates ions to supersonic velocities using a current-free electric double layer, has been tested successfully for the first time inside a space-simulation vacuum chamber. Using a retarding field energy analyzer, the presence of a current-free double layer and the associated ion beam in argon have been confirmed for operating conditions of 0.297 mgs-1 of argon, 53.3 mPa gas pressure, 100 W of radio-frequency forward power at 13.56 MHz, and a maximum axial magnetic field of 138 G. The inductively coupled plasma and ion beam formed have been characterized axially, and the measured beam velocity is about 8.7 kms-1 for these conditions. The effect of moving the Helicon Double Layer Thruster source tube relative to the magnetic field and radio-frequency antenna is investigated, and the pressure dependence of the double layer is measured from 20 to 275 mPa and compared with a recently developed theoretical model. Ions in the Helicon Double Layer Thruster exhaust are also shown to be nonmagnetized, suggesting that ion detachment has occurred.
Description
Citation
Collections
Source
Journal of Propulsion and Power