Corrective Propulsion System Based on the SPT-100 for Advanced Meteorological Spacecraft

Аuthors

Chodnenko W. P., Kolosova M. V.^*

Corporation "Space systems monitoring, information management and electromechanical systems" named A.G. Iosif'yan, "Corporation "VNIIEM", 4, Horomny deadlock, building 1, Moscow, 107078, Russia

*e-mail: marina. kolosova@gmail.com

Abstract

The general performance of the spacecraft from the space segment «Meteor MP», and basic requirements for spacecraft corrective propulsion system are presented.

Keywords:

stationary plasma thruster; corrective propulsion system; spacecraft

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