Titlebook: Micro Newton Thruster Development; Direct Thrust Measur Franz Georg Hey Book 2018 Springer Fachmedien Wiesbaden GmbH 2018 Micro Newton Thru

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https://doi.org/10.1007/978-3-658-21209-4Micro Newton Thruster; Micro-Newton Thrust Measurement; Thrust Noise Characterisation; Electric Propuls

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Electric Propulsion Fundamentals, Furthermore, the acceleration of the propellant particles is not powered by the energy stored in the propellant, but rather by an external power source. This changes the way the parameters of the thruster are calculated.

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Conclusion and Outlook,red 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.

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978-3-658-24865-9Springer Fachmedien Wiesbaden GmbH 2018

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Micro-Newton Thruster Test Facility,ced in chapter 1, section 1.4, the micro-Newton thruster test facility developed can be used for the complete characterisation of AOCS thruster candidates for future scientific space missions such as LISA.

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lance, as well as the downscaling of a High Efficiency Multistage Plasma Thruster to micro-Newton thrust levels. The balance is tailored to fully characterise thruster candidates for the space based gravitational wave detector LISA. Thus, thrust noise measurements in sub-micro-Newton regime can be p

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Book 2018lasma Thruster to micro-Newton thrust levels. The balance is tailored to fully characterise thruster candidates for the space based gravitational wave detector LISA. Thus, thrust noise measurements in sub-micro-Newton regime can be performed in the overall LISA bandwidth. The downscaled thruster can