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

Details 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 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

May 2006

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2006cosre..44..236y&link_type=abstract

Cosmic Research, Volume 44, Issue 3, pp.236-244

Physics

45.10.Db

Scientific paper

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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