Skip to main content
Log in

Electric Propulsion Thrusters: Laboratory Investigation of Jets by Probe Methods

  • Aero- and Gas-Dynamics of Flight Vehicles and Their Engines
  • Published:
Russian Aeronautics Aims and scope Submit manuscript

Abstract

Features of probe measurements of plasma jet parameters of the electric propulsion thrusters under laboratory conditions are studied. Effect of the pressure of the residual gas in the vacuum chamber onto plasma jet formation and spread are investigated.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Similar content being viewed by others

References

  1. Gorshkov, O.A., Muravlev, V.A., and Shagaida, A.A., Khollovskie i ionnye plazmennye dvigateli dlya kosmicheskikh apparatov (Hall and Ion Plasma Thrusters for the Spacecraft), Koroteev, A.S., Ed., Moscow: Mashinostroenie, 2008.

    Google Scholar 

  2. Kim, V.P., Nadiradze, A.B., Popov, G.A., Khodnenko, V.P., and Shishkin, G.G., Problems Dealing with Electric Propulsion Thrusters’ Usage at Spacecraft, in Model’ kosmosa (Space Model), Novikov, L.S., Ed., Moscow: KDU, 2007, vol. 2: Space Effect onto Spacecraft Materials and Equipment, pp. 615–659.

    Google Scholar 

  3. Nazarenko, I.P., Gavryushin, V.M., and Evdokimov, K.V., High-Energy Electron Beam Relaxation in a Stationary Plasma Thruster, Izv.Vuz. Av. Tekhnika, 2017, vol. 60, no. 4, pp. 120–125 [Russian Aeronautics (Engl. Transl.), vol. 60, no. 4, pp. 609–615].

    Google Scholar 

  4. Korsun, A.G., Tverdokhlebova, E.M., and Gabdullin, F.F., The Distinction Between the EP Plume Expansion in Space and in Vacuum Chamber, Proc. 29th Int. Electric Propulsion Conf., Princeton Univ., 2005, IEPC-2005-073, URL: http://www.erps.spacegrant.org//IEPC%20Archives.html.

    Google Scholar 

  5. Biagioni, L., Kim, V., Nicolini, D., et al., Basic Issues in Electric Propulsion Testing and the Need for International Standards, Proc. 28th Int. Electric Propulsion Conf., Toulouse, 2003, IEPC-2003-230, URL: http://www.erps.spacegrant.org//IEPC%20Archives.html.

    Google Scholar 

  6. Andrenucci, M., Berti, M., Biagioni, L., et al., The New EP Test Facilities at Centrospazio and Alta, Proc. 28th Int. Electric Propulsion Conf., Toulouse, 2003, IEPC-2003-229, URL: http://www.erps.spacegrant.org//IEPC%20Archives.html.

    Google Scholar 

  7. Pridannikov, S.Yu., Performances of Stationary Plasma Thrusters under Long-Term Operation, Cand. Sc. (Tech.) Dissertation, Kaliningrad, 2004.

    Google Scholar 

  8. Miller, J.S., Pullins, S.H., Levandier, D.J., et al., Xenon Charge Exchange Cross Sections for Electrostatic Thruster Models, J. Appl. Phys., 2002, vol. 91, no. 3, pp. 984–991.

    Article  Google Scholar 

  9. Bugrova, A.I. and Morozov, A.I., Influence of Vacuum Conditions on the SPT Operation, Proc. 24th Int. Electric Propulsion Conf., Moscow, 1995, IEPC-1995-046, URL: http://www.erps.spacegrant.org//IEPC%20Archives.html.

    Google Scholar 

  10. Hofer, R.R., Peterson, P.Y., and Gallimore, A.D., Characterizing Vacuum Facility Backpressure Effects on the Performance of Hall Thrusters, Proc. 27th Int. Electric Propulsion Conf., Pasadena, CA, 2001, IEPC-01-045, URL: http://www.erps.spacegrant.org//IEPC%20Archives.html.

    Google Scholar 

  11. Azziz, Y., Experimental and Theoretical Characterization of a Hall Thruster Plume, Aeronautics and Astronautics, PhD Dissertation, USA, Massachusetts Institute of Technology, 2007.

    Google Scholar 

  12. Spektor, R., Tighe, W.G., Stoltz, P.H., and Beckwith, K.R.C., Facility Effects on Hall Thruster Performance Through Cathode Coupling, Proc. 34rd Int. Electric Propulsion Conf., Kobe, 2015, IEPC-2015-309, URL: http://www.erps.spacegrant.org//IEPC%20Archives.html.

    Google Scholar 

  13. Li Jie, Yu Daren, Ning Zhongxi, and Li Yong, Effects of Hydrogen Partial Pressure within the Vacuum Facility on Plume Focusing of a Hall Thruster, Proc. 32nd Int. Electric Propulsion Conf., Wiesbaden, 2011, IEPC-2011-098, URL: http://www.erps.spacegrant.org//IEPC%20Archives.html.

    Google Scholar 

  14. Wensheng Huang, Hani Kamhawi, and Haag, T., Effect of Background Pressure on the Performance and Plume of the HiVHAc Hall Thruster, Proc. 33rd Int. Electric Propulsion Conf., Washington: The George Washington University, 2013, IEPC-2013-058, URL: http://www.erps.spacegrant.org//IEPC%20Archives.html.

    Google Scholar 

  15. Kozlov, O.V., Elektricheskii zond v plazme (Electric Probe in Plasma), Moscow: Atomizdat, 1969.

    Google Scholar 

  16. Tonks, L. and Langmuir, I., A General Theory of the Plasma of an Arc, Physical Review, 1929, vol. 34, no. 6. p. 876–922.

    Google Scholar 

  17. Shastry, R., Hofer, R.R., Reid, B.M., and Gallimore, A.D., Method for Analyzing ExB Probe Spectra from Hall Thruster Plumes, Proc. 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conf. & Exhibition, Hartford, CT, 2008, AIAA 2008–4647.

    Google Scholar 

  18. Huddlestone, R.H., Plasma Diagnostic Techniques, Academic Press, 1965.

    Google Scholar 

  19. Khartov, S.A., Nadiradze, A.B., Yakubov, A.M., and Zikeeva, Yu.V., Some Remarks about Published Data Concerning the SPT-100Jet Parameters Distribution, Proc. 25th Int. Electric Propulsion Conf., Cleveland, 1997, IEPC-97-152, URL: http://www.erps.spacegrant.org//IEPC%20Archives.html.

    Google Scholar 

  20. Pereslavtsev, A.A. and Khartov, S.A., Plasma Parameters Investigation in the Near Cathode Zone of the SPT Discharge, Proc. 29th Int. Electric Propulsion Conf., Princeton Univ., 2005, IEPC-2005-061, URL: http://www.erps.spacegrant.org//IEPC%20Archives.html.

    Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to A. B. Nadiradze.

Additional information

Original Russian Text © V.V. Kozhevnikov, A.B. Nadiradze, I.P. Nazarenko, Yu.L. Frolova, S.A. Khartov, 2018, published in Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2018, No. 4, pp. 150–153.

About this article

Check for updates. Verify currency and authenticity via CrossMark

Cite this article

Kozhevnikov, V.V., Nadiradze, A.B., Nazarenko, I.P. et al. Electric Propulsion Thrusters: Laboratory Investigation of Jets by Probe Methods. Russ. Aeronaut. 61, 677–681 (2018). https://doi.org/10.3103/S106879981804027X

Download citation

  • Received:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.3103/S106879981804027X

Keywords

Navigation