Abstract In line with the requirements (table 1.3) a micro-Newton thruster test facility has been developed. The facility consists of a vacuum tank, a highly precise thrust balance, a plasma diagnostics setup and all other necessary hardware to perform EP development, testing and characterisation. As introduced 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.
Micro-Newton Thruster Test Facility
Micro Newton Thruster Development ; 43-103
01.01.2018
61 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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