Direct thrust measurement of a permanent magnet helicon double layer thruster

By Kazunori Takahashi, T. Lafleur, C. Charles, P. Alexander, R. Boswell, M. Perren, R. Lainé, S. Pottinger, V. Lappas, T. Harle and 1 more. 2011

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Direct thrust measurements of a permanent magnet helicon double layer thruster have been made using a pendulum thrust balance and a high sensitivity laser displacement sensor. At the low pressures used (0.08 Pa) an ion beam is detected downstream of the thruster exit, and a maximum thrust force of about 3 mN is measured for argon with an rf input power of about 700 W. The measured thrust is proportional to the upstream plasma density and is in good agreement with the theoretical thrust based on the maximum upstream electron pressure.

Subfields: Aerospace Engineering, Electrical and Electronic Engineering

View Paper: https://www.semanticscholar.org/paper/54f182caa9e22e0510422ebeebc5107192471af4