Hostname: page-component-848d4c4894-4hhp2 Total loading time: 0 Render date: 2024-06-13T06:41:47.411Z Has data issue: false hasContentIssue false

Theory of the plasma thruster based on the rotating electromagnetic field

Published online by Cambridge University Press:  01 December 2014

Ya. I. Kolesnichenko
Affiliation:
Institute for Nuclear Research, Prospekt Nauky 47, Kyiv 03680, Ukraine
V. V. Lutsenko*
Affiliation:
Institute for Nuclear Research, Prospekt Nauky 47, Kyiv 03680, Ukraine
T. S. Rudenko
Affiliation:
Institute for Nuclear Research, Prospekt Nauky 47, Kyiv 03680, Ukraine
*
Email address for correspondence: lutsenko@kinr.kiev.ua

Abstract

A theory of electrodeless electric propulsion systems (EEPS) based on the use of the solenoid magnetic field and the rotating electromagnetic field produced by antennas is developed, which includes a study of the plasma acceleration by the Radio Frequency (RF) field and the concomitant thrust. It was assumed that the frequency of the RF field exceeds the lower hybrid frequency but is much less than the electron gyrofrequency. Relations for the thrust are obtained and analyzed. It is shown that thrust gain is significant only when the RF-induced drift velocity well exceeds the fluid velocity of the injected plasma. It is revealed that the curvature of the magnetic field lines and the plasma acceleration in the region outside the solenoid are the factors which can considerably increase the thrust. On the other hand, it is found that the axial inhomogeneity of the plasma and some other factors are unfavorable for the thrust. The obtained results can be used for the optimization of particular experiments aimed to create a new thruster for long-time space missions.

Type
Research Article
Copyright
Copyright © Cambridge University Press 2014 

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

REFERENCES

Callaghan, E. E. and Maslen, S. H. 1960 The magnetic field of a finite solenoid. Technical Note D-465, Washington, USA: National Aeronautics and Space Administration, 124.Google Scholar
Matsuoka, T.et al. 2011 Scaling laws of Lissajous acceleration for electrodeless helicon plasma thruster. Plasma Fusion Res. Regular Artic. 6, 2 406 103(1)–2 406 103(4).Google Scholar
Matsuoka, T.et al. 2012 One dimensional modelling of radio frequency electric field penetration into magnetized plasmas. Japan J. Appl. Phys. 51, 096 201(1)096 201(7).CrossRefGoogle Scholar
Motomura, T.et al. 2011 Development of electrodeless electric propulsion systems using high-density helicon plasmas: HEAT Project. General Assembly and Scientific Symposium, 2011 XXXth URSI, IEEE, ISBN 978-1-4244-5117-3, DOI:10.1109/URSIGASS.2011.6051085, 1–4.CrossRefGoogle Scholar
Nakamura, T.et al. 2011 Experimental investigation of plasma acceleration by rotating electric field for electrodness plasma truster. In: Proc. 32nd Int. Electric Propulsion Conf., Wiesbaden, Germany, IEPC-2011-279, 239–249.Google Scholar
Nakamura, T.et al. 2012 Study of helicon plasma Lissajous acceleration for electrodeless electric propulsion. The Japan Society for Aeronautical and Space, 28th International Symposium on SpaceTechnology and Science, Okinawa, 2011-b-08, 1–6.Google Scholar
Shinohara, S.et al. 2013 High-density plasma sources: basics and application to electrodeless electric propulsion. Trans. Fusion Sci. Technol. 63, 164167.CrossRefGoogle Scholar
Toki, K.et al. 2009 Plasma acceleration in a compact helicon source using RF antennae. J. Plasma Fusion Res. Ser. 8, 2530.Google Scholar
Virko, V. F., Virko, Yu.V., Slobodyan, V. M. and Shamrai, K. P. 2010 The effect of magnetic configuration on ion acceleration from a compact helicon source with permanent magnets. Plasma Sources Sci. Technol. 19, 015 004(1)015 004(7).CrossRefGoogle Scholar