Optics and Precision Engineering, Volume. 19, Issue 10, 2402(2011)

Work characteristics of low power water propellant pulsed plasma thruster

ZHU Ping1,2、*, HOU Li-ya1, and ZHANG Wei-yi1
Author Affiliations
  • 1[in Chinese]
  • 2[in Chinese]
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    References(14)

    [3] [3] CHRISTOPHER D R, MARK E C, MATTICK A T. Pulsed plasma thruster system for microsatellites[J]. J Spac Rock, 2005, 42(1): 161-170.

    [4] [4] YIN L, ZHOU J, MIAO W B. Design and simulation of the discharge current wave for pulsed plasma thruster[J]. J Propul Tech, 2010, 31(4): 490-495.(in Chinese)

    [5] [5] JUNJI U, JUNPEI I, YUKIYA K, et al.. Study on pulsed plasma thruster configuration to expand impulse bit range[C]. 29th International Electric Propulsion Conference, IEPC,2005: 234.

    [6] [6] SCHONHERR T, KOMURASAKI K. Evaluation of discharge behavior of the pulsed plasma thruster SIMP-LEX[C]. AIAA,2010: 6530.

    [7] [7] SPANJERS G G, LOTSPEICH J S, MCFALL K A, et al.. Propellant losses because of particulate emission in a pulsed plasma thruster[J]. J Propul P,1998,14(4): 554-559.

    [8] [8] MARKUSIC T E, KURT A P, CHOUEIRI E Y, et al.. Ablative z-pinch pulsed plasma thruster[J]. J Propul P, 2005, 21(3): 392-405.

    [9] [9] DE ALESSANDRO R O, BRITO H, GALIAN E S. P4S-1 solid propellant pulsed plasma thruster development phase[C]. AIAA,2009: 5281.

    [10] [10] ARRINGTON L A, HAAG T W, PENCIL E J, et al.. A performance comparison of pulsed plasma thruster electrode configurations[C]. 25th International Electric Propulsion Conference, IEPC,1997: 127.

    [11] [11] KUANG Y Z. Effects of propellant geometry on PPT performance[C]. 17th International Electric Propulsion Conference. IEPC,1984: 685-690.

    [12] [12] HIROYUKI K, KAKAMI A, FURUTA Y, et al.. Liquid propellant pulsed plasma thruster[C]. 28th International Electric Propulsion Conference, IEPC, 2003: 087.

    [13] [13] ZHU P, HOU L Y, ZHANG W Y. The effect of easily ionized elements Na and K on the performance of pulsed plasma thruster using water propellant[J]. Science China Tech. Sci., 2010, 53(10): 2878-2882.

    [14] [14] ZHU P, HOU L Y, ZHANG W Y. The measurement on micro-jet impulse based on laser interferometer[J]. 2009 ASME Fluids Engineering Division Summer Meeting and Exhibition, FEDSM,2009,78030(1): 1707-1714.

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    ZHU Ping, HOU Li-ya, ZHANG Wei-yi. Work characteristics of low power water propellant pulsed plasma thruster[J]. Optics and Precision Engineering, 2011, 19(10): 2402

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    Paper Information

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    Received: Jan. 27, 2011

    Accepted: --

    Published Online: Nov. 9, 2011

    The Author Email: Ping ZHU (hyuanpeng@sohu.com)

    DOI:10.3788/ope.20111910.2402

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