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Comparative analysis of micro-cathode arc thruster performance

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Описание материала

Propulsion systems based on electrically activated small thrusters that utilize chemically-inert solid propellants are beneficial for micro-satellite applications. Microthrusters are able to deliver small impulse bits and characterized by simplicity, scalability, low cost, low weight and high reliability. This paper analyzes performance of micro-cathode thruster in comparison with other commercially available thruster technologies operating at the same power range.

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)

Keidar M., Shashurin A., Zhuang T.

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