Magnetic field configuration effects on a miniature DC ion thruster with an inverted potential structure

Author:

Tanaka Yoshinori,Takao YoshinoriORCID

Funder

JGC-S Scholarship Foundation

Japan Society for the Promotion of Science

Publisher

Elsevier BV

Reference24 articles.

1. Space micropropulsion systems for Cubesats and small satellites: from proximate targets to furthermost frontiers;Levchenko;Appl. Phys. Rev.,2018

2. In-flight operation of the Hayabusa2 ion engine system on its way to rendezvous with asteroid 162173 Ryugu;Nishiyama;Acta Astronaut.,2020

3. Initial flight operations of the miniature propulsion system installed on small space probe: PROCYON;Koizumi;Trans. Jpn. Soc. Aeronaut. Space Sci., Aerosp. Technol. Jpn.,2016

4. Review of formation flying and constellation missions using nanosatellites;Bandyopadhyay;J. Spacecraft Rockets,2016

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

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