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Development of a novel power processing unit for Hall thrusters

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Описание материала

We have been developing a new concept PPU, which has the advantages of smaller size and lighter weight than conventional one. The thrust performance of magnetic layer type Hall thruster developed at Kyushu University with this new PPU was investigated and it showed a good performance compared to conventional power supplies. The thrust to power ratio is improved to 58 mN/kW at discharge voltage of 150 V and anode xenon mass flow rate of 1.0 mg/s.

Характеристики

Дата проведения

October 6 – 10, 2013

Название конференции

33nd International Electric Propulsion Conference

место проведения

George Washington University in Washington, D.C., USA

Качество

excellent

Раздел

Аэрокосмическая техника

Язык

English

Типы файлов

pdf

Автор(ы)

Osuga H., Tamida T., Yamamoto N.

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