Power processing unit for hall-effect thrusters on "Meteor-M №3 spacecraf"

The development results of power processing unit (PPU-M) for hall-effect thrusters on «Meteor-M №3» spacecraft are considered. The structure, weight, dimensions and main technical characteristics of the system in the paper are presented. The work peculiarity of the system is unstable input voltage o...

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Bibliographic Details
Published inMATEC Web of Conferences Vol. 48; p. 1007
Main Authors Moshnyakov, Anton, Mikhaylov, Maxim
Format Journal Article Conference Proceeding
LanguageEnglish
Published Les Ulis EDP Sciences 2016
Subjects
Analogs
Circuit design
Comparative analysis
Data buses
Hall effect
Spacecraft
Thrusters
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Summary:The development results of power processing unit (PPU-M) for hall-effect thrusters on «Meteor-M №3» spacecraft are considered. The structure, weight, dimensions and main technical characteristics of the system in the paper are presented. The work peculiarity of the system is unstable input voltage of both power bus and control bus that increases the ripple voltages and currents at the input and the output and causes the additional requirements to the circuit design. A comparative analysis of the system characteristics and European analogs was carried out, and then a conclusion on the basis of available data that the characteristics of the system are not inferior to European analogs was made.
ISSN:2261-236X
2274-7214
2261-236X
DOI:10.1051/matecconf/20164801007