2018 | OriginalPaper | Chapter
Conclusion and Outlook
Author : Franz Georg Hey
Published in: Micro Newton Thruster Development
Publisher: Springer Fachmedien Wiesbaden
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In this thesis the development, design and characterisation of a micro-Newton thruster test facility was presented. The facility consists of the required vacuum infrastructure, a highly precise and highly stable micro-Newton thrust balance and a set of plasma diagnostics. Measurement results of real thruster tests that has been performed with the facility has been shown and analysed.