Determination of the width of a corridor of re-entry into the atmosphere for the problem of launching a spacecraft into a circumplanetary orbit after braking in the atmosphere |
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Authors: | V A Yaroshevskii |
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Institution: | (1) Zhukovsky Central Institute of Aerohydrodynamics, Zhukovsky, Moscow oblast, 140160, Russia |
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Abstract: | A method of calculating the optimal trajectories of a spacecraft re-entry into the atmosphere is considered under the condition of minimization of a re-orbit burn at the apocenter of the segment of escape from the atmosphere and taking into account a constraint on the maximum overload. |
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