Creation of Algorithms for Correction of Low-altitude Orbit Parameters for a Space Vehicle with Electrical Rocket Propulsion System
Vadim Salmin, Vladimir Volotsuev, Ivan Tkachenko
Influence of design parameters of an electrical rocket propulsion system (ERPS) and algorithms of correction of low-altitude orbits for terms of useful functioning of a space vehicle is investigated. The method of a selection optimum ERPS and cyclogrammes of orbit correction low-altitude space vehicle is offered. Guaranteeing estimations of a propellant consumption on long intervals of time for various types ERPS on the basis of fixed plasma engines are received.