Physics, mathematics, and technology

2012 Issue №4

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The check of electromagnetic compability of the propulsion system with the electrodynamic simulator of the thrust module

Pages
90-94

Abstract

The noise nature of discharge current oscillations of the stationary plasma thruster has been revealed. The maximal level of generated low-frequency conducted interferences in all the modes of the electro-dynamic thrust module simulator operation has been determined.

Reference

1. Яковлев Е. А. Испытания космических электроракетных двигательных установок. М., 1981.
2. Лесневский В. А., Румянцев А. В., Соколов В. В. Имитатор электродинамических характеристик тягового модуля // Вестник Российского государственного университета им. И. Канта. 2010. Вып. 10.