Abstract
To clause the problem of a choice of design characteristics low-orbit space vehicle, incorporating Electric Rocket Propulsion System (ERPS) for correction of parameters of an orbit is considered. The mathematical models describing interrelation of factors of an environment, design parameters of onboard systems (including ERPS) and design characteristics low-orbit space vehicle as a whole are considered.
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Schedule a callMore From: VESTNIK of Samara University. Aerospace and Mechanical Engineering
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