Effect of spacecraft surface conductivity on voltage of microwave neutralizer in gridded ion thrusters-Reference-Cited by-同舟云学术

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Effect of spacecraft surface conductivity on voltage of microwave neutralizer in gridded ion thrusters

Published:2023-11 Issue: Volume:212 Page:130-138
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Nono Ayumu^ORCID,Morishita Takato^ORCID,Hosoda Satoshi,Tsukizaki Ryudo,Nishiyama Kazutaka^ORCID

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference24 articles.

1. A critical history of electric propulsion: the first 50 Years (1906-1956);Choueiri;J. Propul. Power,2004

2. Powered flight of electron cyclotron resonance ion engines on Hayabusa explorer;Kuninaka;J. Propul. Power,2007

3. Electric propulsion for satellites and spacecraft: established technologies and novel approaches;Mazouffre;Plasma Sources Sci. Technol.,2016

4. The technological and commercial expansion of electric propulsion;Lev;Acta Astronaut.,2019

5. Fundamentals of Electric Propulsion: Ion and Hall Thrusters;Goebel,2008

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