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Aleksashkin S. N. Bobylev A. V. Vlasenko O. V. Pichkhadze K. M. Terterashvili A. V. Yaroshevsky V. A. 《Cosmic Research》2003,41(3):280-284
The possibility of using an inflatable braking device for controlled descent in the Martian atmosphere of large-capacity cargoes is analyzed. The most complicated version of the trajectory control problem is considered, namely, the injection of a spacecraft at hyperbolic velocity into a parking orbit after braking in the atmosphere. 相似文献
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