Discharge mode transition in a Krypton-fed 1 A-class LaB6 cathode for low-power Hall thrusters for small satellites-Reference-Cited by-同舟云学术

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Discharge mode transition in a Krypton-fed 1 A-class LaB6 cathode for low-power Hall thrusters for small satellites

Published:2020-02-14 Issue:6 Volume:127 Page:064501
ISSN:0021-8979
Container-title:Journal of Applied Physics
language:en
Short-container-title:Journal of Applied Physics

Author:

Potrivitu G.-C.¹^ORCID,Xu L.¹²,Huang S.¹,Rohaizat M. W. A. B.¹^ORCID,Xu S.¹^ORCID

Affiliation:

1. Plasma Sources and Applications Centre/Space Propulsion Centre, National Institute of Education, Nanyang Technological University, Singapore 637616

2. Center for Space Propulsion and Gravitational Universe (SPaGU), Hang Zhou Institute for Advanced Studies, University of Chinese Academy of Sciences, Hang Zhou 310024, China

Funder

OSTIn-SRP/EDB; NRF; MOE Singapore AcRF

Publisher

AIP Publishing

Subject

General Physics and Astronomy

Link

http://aip.scitation.org/doi/pdf/10.1063/1.5142019

Reference25 articles.

1. The technological and commercial expansion of electric propulsion

2. Space micropropulsion systems for Cubesats and small satellites: From proximate targets to furthermost frontiers

3. Mars Colonization: Beyond Getting There

4. Explore space using swarms of tiny satellites

5. Electric propulsion for satellites and spacecraft: established technologies and novel approaches

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1. Densification, microstructure, mechanical, and thermionic properties of spark plasma sintered LaB₆–HfB₂ composite;International Journal of Applied Ceramic Technology;2024-07-15

2. Investigation of anode diameter and keeper geometry influence on open-end emitter heaterless hollow cathode discharge;Vacuum;2024-07

3. Development of a modular hollow cathode for ground testing of plasma thrusters;Vacuum;2024-01

4. LaB6 hollow cathode with a novel graphite heater;Vacuum;2023-10

5. Experimental Characterization of a Hollow Cathode with Iridium–Cerium Alloy;Journal of Propulsion and Power;2023-09

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