https://doi.org/10.1140/epjd/e2016-70236-0
Regular Article
An advanced electric propulsion diagnostic (AEPD) platform for in-situ characterization of electric propulsion thrusters and ion beam sources*
1 Leibniz-Institute of Surface
Modification, Permoserstr.
15, 04318
Leipzig,
Germany
2 Aerospazio Tecnologie s.r.l., Via
Provinciale Nord 42a, 53040 Rapolano Terme, Siena, Italy
3 Airbus Defence & Space GmbH,
Im Langen Grund, 74239
Hardthausen-Lampoldshausen,
Germany
4 Christian-Albrechts-Universität zu
Kiel, Leibnizstr.
11-19, 24098
Kiel,
Germany
5 Justus-Liebig-Universität Gießen,
Heinrich-Buff-Ring
16, 35392
Gießen,
Germany
6 ICARE, CNRS,
1C Av. de la Recherche
Scientifique, 45071
Orléans,
France
7 Space Enterprise Partnerships Ltd.,
Bennetts, Eastergate Lane, Chichester, West Sussex
PO20 3SJ,
UK
8 ESA/ESTEC, Keplerlaan 1,
2201 AZ
Noordwijk, The
Netherlands
a
e-mail: Carsten.Bundesmann@iom-leipzig.de
Received:
4
April
2016
Published online:
18
October
2016
Experimental characterization is an essential task in development, qualification and optimization process of electric propulsion thrusters or ion beam sources for material processing, because it can verify that the thruster or ion beam source fulfills the requested mission or application requirements, and it can provide parameters for thruster and plasma modeling. Moreover, there is a need for standardizing electric propulsion thruster diagnostics in order to make characterization results of different thrusters and also from measurements performed in different vacuum facilities reliable and comparable. Therefore, we have developed an advanced electric propulsion diagnostic (AEPD) platform, which allows a comprehensive in-situ characterization of electric propulsion thrusters (or ion beam sources) and could serve as a standard on-ground tool in the future. The AEPD platform uses a five-axis positioning system and provides the option to use diagnostic tools for beam characterization (Faraday probe, retarding potential analyzer, ExB probe, active thermal probe), for optical inspection (telemicroscope, triangular laser head), and for thermal characterization (pyrometer, thermocamera). Here we describe the capabilities of the diagnostic platform and provide first experimental results of the characterization of a gridded ion thruster RIT-μX.
© EDP Sciences, Società Italiana di Fisica, Springer-Verlag 2016