In this article problem of low-power SPT development actualite is considered. The main requirements for this thruster class are represented. Some methods of low-power Hall thruster developing and their advantages and disadvantage. The test results and main parameters of new law-power thruster laboratory model SPT-20M are represented. Comparative characteristics of SPT model and law power hollow thrusters developed by leading world specialists is shown.
The low power hollow thruster for orbit correction system for small, mini and micro satellites
01.01.2005
565082 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Hall Thruster for Small, Low Power Satellites
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