Development of a MEMS based colloid thruster with sandwich structure

Jijun Xiong, Zhaoying Zhou, Dong Sun, Xiongying Ye

    Research output: Journal Publications and ReviewsRGC 21 - Publication in refereed journalpeer-review

    Abstract

    Design of a propulsion system with mini-size, high specific impulse and extremely low impulse bit is highly demanded by micro and nano spacecrafts. In this paper, a MEMS based micro colloid thruster has been developed by bulk silicon processing. The dimensions of the new thruster have been reduced considerably, which allows the micro thrusters to use a working voltage of 1-3 kV instead of 5-10 kV traditionally. The emitter of the thruster is designed to enable fine thrust control in the micro Newton range. A cantilever-based test facility is further developed to test the micro colloid thruster. Experimental results show that a thrust in the order of micro Newton can be produced by a single emitter, with a working threshold voltage as low as 1400 V. © 2004 Elsevier B.V. All rights reserved.
    Original languageEnglish
    Pages (from-to)168-172
    JournalSensors and Actuators, A: Physical
    Volume117
    Issue number1
    DOIs
    Publication statusPublished - 3 Jan 2005

    Research Keywords

    • Colloid thruster
    • MEMS
    • Micro propulsion
    • Micro thruster

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