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Factors Affecting Ion Thruster’s Performance

Authors

  • Yuzhe Liu Email Shandong Experimental High school, Jinan, Shandong
  • Lidong Lin Shandong Experimental High school, Jinan, Shandong
  • Han Dong Shandong Experimental High school, Jinan, Shandong

DOI:

https://doi.org/10.30564/jeisr.v3i2.3678
Received: 2 September 2021 | Published Online: 3 November 2021

Abstract

In this project, we investigated how ion thrusters produce propulsion and how the design of ion thrusters affects the performance of the thruster. In the experiment, we build a high voltage power supply (0- 50 kV) and foil rings to produce ion wind. When considering the design of the thruster, we focus on three variables: the volume of the space, where ions are produced and the electric field intensity. Thus, to investigate the first variable we made foil rings with different radius and change the distance between the ring and positive cathode. To determine the propulsion produced we use a speed sensor to determine the magnitude of the wind produced.

Keywords:

Ion thruster, Ion engine, Ion propulsion

References

[1]Jahn, Robert G. (1968). Physics of Electric Propulsion (1st ed.). McGraw Hill Book Company. ISBN 978-0070322448. Reprint: Jahn, Robert G. (2006). Physics of Electric Propulsion. Dover Publications. ISBN 978-0486450407.

[2]Coulomb (1785b) “Second mémoire sur l’électricité et le magnétisme,” Histoire de l’Académie Royale des Sciences, pages 578-611.

[3]Choueiri, Edgar Y. (2009). “New dawn of electric rocket”. Scientific American. 300 (2): 58–65. Bibcode:2009SciAm.300b..58C. DOI: 10.1038/scientificamerican0209-58. PMID 19186707.

[4]Choueiri, E. Y. “A Critical History of Electric Propulsion: The First 50 Years (1906–1956)”. Retrieved 18 October 2016.

[5] Jahn, Robert G.; Choueiri, Edgar Y. (2003). “Electric Propulsion” (PDF). Encyclopedia of Physical Science and Technology. 5 (3rd ed.). Academic Press. pp. 125-141. ISBN 978-0122274107.

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