Measurement and diagnosis of miniaturized ion thruster plume
Author:
Affiliation:
1. Department of Aerospace Science and Technology, Space Engineering University 1 , Beijing 101416, People’s Republic of China
2. School of Space and Environment, Beihang University 2 , Beijing 100191, People’s Republic of China
Abstract
Funder
National Natural Science Foundation of China
Natural Science Foundation of Beijing Municipality
Publisher
AIP Publishing
Subject
General Physics and Astronomy
Link
https://pubs.aip.org/aip/adv/article-pdf/doi/10.1063/5.0143330/16783396/035036_1_online.pdf
Reference27 articles.
1. Quad channel micro-cathode arc thruster electric propulsion subsystem for the ballistic reinforced satellite (BRICSat-P)
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3. Investigation and experimental simulation of performance deterioration of microwave discharge ion thruster μ10 during space operation;Acta Astronaut.,2020
4. Thrust control algorithms for the GOCE ion propulsion assembly
5. Design and development of the UK-10 ion propulsion system
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