Low-Power Ion Thrusters. State of Development at Research Institute of Applied Mechanics and Electrodynamics, MAI

Author:

Akhmetzhanov R V,Bogatyi A V,Kashirin D A,Obukhov V A,Popov G A,Svotina V V,Khartov S A

Abstract

Abstract This article describes the activities carried out by RIAME MAI in the field of low-power ion thrusters in 2010-2020. The results of study of a laboratory model of low power RIT using a different shape of GDC are presented. The results of work on creating an experimental model of such RIT with elements of the propulsion system are shown. The article also presents the research on the process of erosion of the accelerating electrode of the RIT - a critical element of the thruster design from the point of view of the lifetime.

Publisher

IOP Publishing

Subject

General Medicine

Reference17 articles.

1. Hollow Cathode and Low-Thrust Extraction Grid Analysis for a Miniature Ion Thruster;Wirz,2008

2. Small carry-on impactor of Hayabusa 2 mission;Takanao;Acta Astronautica,2013

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