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Efficiency Estimation of Electrothermal Thrusters Use in the Control System of the Technological Spacecraft Motion
Authors:G P Anshakov  A I Belousov  A V Sedel’nikov  A S Gorozhankina
Institution:1.Samara University,Samara,Russia
Abstract:The influence of various control systems of the orbital motion of a technological spacecraft on the level of microacceleration of its internal environment is simulated. Conclusions are drawn about the effectiveness of control systems with different actuators for realization of certain gravitationally sensitive processes onboard a spacecraft.
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