Propulsion and Power Plants
Аuthors
*,Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
*e-mail: vka.mai@mail.ru
Abstract
A model is suggested to compute wall shape changes for discharge chamber channel of a stationary plasma engine. Computed erosion shapes were obtained for the M-100 engine. They correspond satisfactorily to data of full-scale durability tests. An appropriate computer program is able to analyze flows of atomized channel material both inside and outside of the channel. Calculation results show a film sputtering into anode region and these data are confirmed with experiments.
Keywords:
erosion; discharge chamber channel; ionic atomization; sputtering
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