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

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

Podrobná bibliografie
Parent link:MATEC Web of Conferences
Vol. 48 : Space Engineering.— 2016.— [01007, 4 p.]
Hlavní autor: Moshnyakov A. Anton
Korporativní autor: Национальный исследовательский Томский политехнический университет (ТПУ) Институт неразрушающего контроля (ИНК) Кафедра промышленной и медицинской электроники (ПМЭ)
Další autoři: Mikhaylov M. V. Maksim Valentinovich
Shrnutí:Title screen
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
Vydáno: 2016
Edice:Spacecrafts and Devices
Témata:
электронный ресурс
труды учёных ТПУ
блоки
обработка
мощности
эффект Холла
двигатели малой тяги
космические аппараты
On-line přístup:http://dx.doi.org/10.1051/matecconf/20164801007
http://earchive.tpu.ru/handle/11683/33714
Médium: Elektronický zdroj Kapitola
KOHA link:https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=648915

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