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The effect of easily ionized elements Na and K on the performance of pulsed plasma thruster using water propellant

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Abstract

In view of the low thrust power ratio caused by the high resistance of pulsed plasma thruster using water propellant, the paper argues that the easily ionized elements Na and K with low ionic potentials are added in the water propellant to improve its performance. The measurement of the discharging current and plasma emission spectrographic analysis prove the improvement. The experiments show that the elements Na and K have certain effect on the improvement of the performance of pulsed plasma thruster: In comparison with water propellant, the NaCl and KCl water propellant has a lower total resistance and a higher ratio of thruster power and specific impulse, and the NaCl water propellant has a slightly stronger effect on pulsed plasma thruster than the KCl. The plasma emission spectrographic analysis is in consistent with the experiment of measuring the discharging current: The elements Na and K can intensify the plasma emission spectrographic signal.

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References

  1. Christopher D R, Mark E C, Mattick A T. Pulsed plasma thruster system for microsatellites. J Spac Rock, 2005, 42(1): 161–170

    Article  Google Scholar 

  2. Uezu J J, Iio J P. Study on pulsed plasma thruster configuration to expand impulse bit range. In: 29th International Electric Propulsion Conference, 2005. 234

  3. Spanjers G G, Lotspeich J S. Propellant losses because of particulate emission in a pulsed plasma thruster. J Propul P, 1998, 14(4): 554–559

    Article  Google Scholar 

  4. Markusic T E, Kurt A P, Choueiri E Y, et al. Ablative z-pinch pulsed plasma thruster. J Propul P, 2005, 21(3): 392–405

    Article  Google Scholar 

  5. Hiroyuki K, Kakami A, Furuta Y, et al. Liquid propellant pulsed plasma thruster. In: 28th International Electric Propulsion Conference, 2003. 87

  6. Carsten A S. Investigation of thrust mechanisms in a water fed pulsed plasma thruster. Dissertation of Doctoral Degree. USA: The Ohio State University, 2003. 68–70

    Google Scholar 

  7. Hiroyuki K, Yohei F. A pulsed plasma thruster using water as the propellant. AIAA-2004-3460, 2004

  8. Jahn R G. Physics of Electric Propulsion. New York: McGraw-Hill, 1968. 12–13

    Google Scholar 

  9. Hou D L, Zhao W S, Kang X M. Performance analysis of pulsed plasma thruster. J Propul Tech, 2008, 29(3): 377–380

    Google Scholar 

  10. Liu L L, Deng J X. Design and development of SiC(W, Ti)C gradient ceramic nozzle. Sci China Tech Sci, 2008, 51(1): 77–84

    Article  Google Scholar 

  11. Nob H, Le C K. Closed cycle mhd generator using He/Xe working plasma. AIAA-2002-2144, 2002

  12. Alan M P, Nick P. Salt effects on ion formation in desorption mass spectrometry: an investigation into the role of alkali chlorides on peak suppression in time-of-flight-secondary ion mass spectrometry. Analyt Chem, 2009, 81(3): 1040–1048

    Article  Google Scholar 

  13. Yan J H, Dai S L. Emission spectroscopy diagnosis of the radicals generated in gas-liquid phases gliding arc discharge. Spectr Sp A, 2008, 28(8): 1851–1855

    Google Scholar 

  14. Song W D. Active electrospray ionization for efficient electric thrusters. AIAA-2004-3942, 2004

  15. Wang C C, Subrata R. Microscale plasma actuators for improved thrust density. J Appl Phys, 2009, 17(7): 013310–013317

    Article  Google Scholar 

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Correspondence to Ping Zhu.

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Zhu, P., Hou, L. & Zhang, W. The effect of easily ionized elements Na and K on the performance of pulsed plasma thruster using water propellant. Sci. China Technol. Sci. 53, 2878–2882 (2010). https://doi.org/10.1007/s11431-010-4086-1

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  • DOI: https://doi.org/10.1007/s11431-010-4086-1

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