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Inclusion of the economic factor for making a decision in the pre-launch procedure of a launcher. Kosm. nauka tehnol. 2003 ;9(Supplement1):074-077.
. George de Bothezat and his contribution into the world aviation and astronautics. Space Science and Technology. 2022 ;28(1):70-80.
. Rotation characteristics of rigid rotor fastened in resilient mountings with a dynamic instability. Kosm. nauka tehnol. 2002 ;8(Supplement1):058-063.
A method for forming a set of pareto-optimum structural parameters of compound technical systems. Kosm. nauka tehnol. 1996 ;2(1):62–67.
. Methods for determining optimum design parameters of compound technical systems with restrictions impoSED. Kosm. nauka tehnol. 1996 ;2(1):57–61.
. An algorithm for digital correction of the orbital gygocompass of a space vehicle. Kosm. nauka tehnol. 2006 ;12(2-3):012-015.
. The control of essentially non-symmetric runaway block with the engine working uninterruptedly. Kosm. nauka tehnol. 2004 ;10(4):032-038.
. Particularities of control of the International space station «Alpha» at the initial stage of flightI. Kosm. nauka tehnol. 2006 ;12(2-3):003-007.
. Acoustic oscillations in the atmosphere as a possible channel of cosmic influence on the biosphere. Kosm. nauka tehnol. 2002 ;8(Supplement2):420-433.
. Proposals for the ISS: «Photosynthesis-2» Experiment Influence of microgravity on oxygenic photosynthesis. Kosm. nauka tehnol. 2000 ;6(4):096-096.
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