Critical conditions of condensation of metal working medium of electric propulsion on spacecraft surfaces

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MAIK Nauka/Interperiodica

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

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

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Optimization of transfer trajectories to the Apophis asteroid for spacecraft with high and low thrust

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Cosmic Research, Vol. 52, Iss. 2, 2014-03 ,pp. : 106-117

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On a possibility of delivery of samples of primordial matter from asteroids of the main belt by a spacecraft with electric propulsion

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Cosmic Research, Vol. 45, Iss. 3, 2007-06 ,pp. : 210-219

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The use of solutions to problems of spacecraft trajectory optimization in impulse formulation when solving the problems of optimal control of trajectories of a spacecraft with limited thrust engine: I

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Cosmic Research, Vol. 45, Iss. 4, 2007-08 ,pp. : 339-347

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