Abstract
This paper is focused on the description of simulation codes developed to
design a helicon plasma thruster for a small satellite under development in the research
project Helicon plasma hydrazine combined micro (HPH.com) conducted within the 7th
Framework Program of the EU by a European consortium.
Original language | English |
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Title of host publication | Proceedings of the 31st International Electric Propulsion Conference, IEPC-2009, 20-24 September, 2009, Ann Arbor, Michigan |
Pages | 1-8 |
Publication status | Published - 2009 |