Affiliation:
1. State Key Laboratory of Electrical Insulation and Power Equipment, Xi'an Jiaotong University, Xi'an 710049, China
2. Surrey Space Centre, University of Surrey, Guilford GU2 7XH, United Kingdom
3. Beijing Institute of Control Engineering, Beijing 100190, China
Abstract
The discharge mode characteristics of cathodes may strongly influence the discharge stability and performance of electrostatic thrusters. In this article, discharge characteristics and mode transition phenomenon of the ring-cusp magnetically confined plasma bridge neutralizer (RCM-PBN) were experimentally studied using argon as the working gas. The dependences of anode current and oscillation amplitude on anode voltage, argon flow rate, heater power, and cathode-to-anode distance were investigated. Plasma properties were measured and plasma plume images were taken under different discharge modes. Two distinct discharge modes were observed during the experiments: high oscillation mode and low oscillation mode. In the high oscillation mode, the plasma plume appears dim, the anode current is low, and the oscillation level is more than 2%. While in the low oscillation mode, a spot-like structure close to the orifice is observed. The plume becomes brighter, the anode current increases, and the oscillation level decreases below 2%. The RCM-PBN was found to transition into the low oscillation mode by increasing anode voltage, flow rate, heater power and by decreasing the cathode-to-anode distance.
Funder
National Natural Science Foundation of China
China Postdoctoral Science Foundation
Beijing Institute of Control Engineering Advanced Space Propulsion Technology Laboratory and Beijing High-efficiency and Green Aerospace Propulsion Engineering Technology Research Center Open Foundati
National Key R&D Program of China
Fundamental Research Funds for the Central Universities
Subject
General Physics and Astronomy
Cited by
2 articles.
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