Development of a Low Power Micro-Ion Engine Using Microwave Discharge

  • Koizumi, Hiroyuki (Institute of Space and Astronautical Science/Japan Aerospace Exploration Agency) ;
  • Kuninaka, Hitoshi (Institute of Space and Astronautical Science/Japan Aerospace Exploration Agency)
  • Published : 2008.03.30

Abstract

In this study, we propose a novel micro-ion engine system. Single plasma source is used for both ion beam source and neutralizing electron source. By changing the electrical connection, either operation can be switched. This micro-ion engine system gives translation motion and attitude control to microspacecraft. The major objective of this study is verification of our concept. Small plasma source of 20 mm diameter was developed. Plasma was sustained by microwave power. Using this plasma source, ion beam extraction and electron emission was successively demonstrated.

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