Physical and Mathematical Simulation of Electric Polarization of Low-Orbit Spacecraft under the Conditions of Hypersonic Flow by a Stream of Plasma of the Earth's Upper Ionosphere

By Skryabysheva I. Yu.  

Cosmic Research, Vol. 42, Iss. 1, 2004-01 ,pp. : 39-47

MAIK Nauka/Interperiodica

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Planar Problem of an Optimal Transfer of a Low-Thrust Spacecraft from High-Elliptic to Geosynchronous Orbit

By Akhmetshin R. Z.  

Cosmic Research, Vol. 42, Iss. 3, 2004-05 ,pp. : 238-249

MAIK Nauka/Interperiodica

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Cluster flight orbit design method for fractionated spacecraft

By Wang Jihe   Nakasuka Shinichi  

Aircraft Engineering, Vol. 84, Iss. 5, 2012-08 ,pp. : 330-343

Emerald Group Publishing Ltd

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On solving the problems of optimization of trajectories of many-revolution orbit transfers of spacecraft

By Ryzhov S.   Grigoriev I.  

Cosmic Research, Vol. 44, Iss. 3, 2006-05 ,pp. : 258-267

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Optimization of Flight Trajectories of a Spacecraft with Electric Propulsion Using the Gravitational Maneuver

By Fedotov G. G.  

Cosmic Research, Vol. 42, Iss. 4, 2004-07 ,pp. : 389-398

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